System and method for operating a steam turbine with a control system having a turbine simulator

Abstract

A steam turbine is provided with an automatic digital computer control and a backup analog control which function in load and speed control loops during the positioning of the turbine inlet valves for speed and load control. An operator panel is provided with a test switch for transferring the turbine operation to backup control and for connecting the automatic control to a turbine simulator stored in the computer when it is desired to use the on-line computer for training, checkout or maintenance without disturbing the power generation process.

Parent Case Text

This is a continuation, of application Ser. No. 247,852 filed Apr. 26, 1972, now abandoned.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS

1. Ser. No. 722,779, entitled "Improved System and Method for Operating a Steam Turbine and an Electric Power Generating Plant" filed by Theodore C. Giras and Manfred Birnbaum on Apr. 4, 1968 now abandoned, assigned to the present assignee, and continued as Ser. No. 124,933 on Mar. 16, 1971, and Ser. No. 319,115, on Dec. 29, 1972.

2. Ser. No. 408,962, entitled "System and Method for Starting, Synchronizing and Operating a Steam Turbine with Digital Computer Control" filed as a continuation of Ser. No. 247,877 which had been filed by Theodore C. Girass and Robert Uram on Apr. 26, 1972 and assigned to the present assignee.

BACKGROUND OF THE INVENTION

The present invention relates to electric power plant turbines and more particularly to steam turbine control systems and the operation of such systems with turbine simulators.

In the operation of an electric power generating plant, it is often desirable to have at the plant site a turbine or turbine generator simulation capability for turbine operator training and control system maintenance purposes. Briefly, a turbine simulator dynamically provides the functioning needed to generate turbine or turbine generator feedback signals to the turbine control system in response to control signal outputs from the control system. A plant situs simulation capability is to be distinguished for conventionally available power plant or turbine simulators usable at locations remote from the plant for purposes other than turbine operator training or control system maintenance, i.e. such as for testing purposes during original manufacture. The latter simulators may be provided in the form of software models executable in digital computers at the remote location. In some instances, portable or resident analog or digital computer simulators are provided at the plant location in the form of equipment items distinct from the turbine control equipment. In the usual case, the in-plant simulator is usable during periods of off-line turbine status for control system checkout prior to on-line operation.

It is generally desirable to provide a turbine or turbine generator simulator which is usable off-line and during on-line turbine operation for control system checkout and maintenance and/or for turbine operator training. The need for on-line simulation capability increases with increasing control system complexity. In any case, simulation for turbine operator training or control system maintenance purposes relative to the installed and operational turbine should be implementable without interruption of electric power generation because of turbine shutdown costs and possible power generation revenue losses. The present invention is directed to this objective.

The description of prior art herein is made on good faith and no representation is made that any prior art considered is the best pertaining prior art nor that the interpretation placed on it is unrebuttable.

SUMMARY OF THE INVENTION

A turbine for an electric power plant includes inlet valves or other means for controlling the energization level of of the turbine, and a control system for the turbine includes an automatic control and a backup control. Means are provided for automatically controlling the valves or other means to satisfy a turbine speed or load reference. The automatic control system further includes means for responding to predetermined control outputs from the automatic control system and for generating turbine response simulations for application to predetermined inputs for the automatic control system when the turbine control system is placed in a simulation mode by the operation of an operator switch. Means are provided for transferring the turbine operation from automatic to backup control on selection of the simulation mode.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a schematic diagram on an electric power plant including a large steam turbine and a fossile fuel fired drum type boiler and control devices which are all operable in accordance with the principles of the invention;

FIG. 2 shows a schematic diagram on a programmed digital computer control system operable with a steam turbine and its associated devices shown in FIG. 1 in accordance with the principles of the invention;

FIGS. 3A, 3B and 3C shows a schematic diagram of a hybrid interface between a manual backup system and the digital computer connected with the servo system controlling the valve actuators;

FIG. 4 shows a simplified block diagram of the digital Electro Hydraulic Control System in accordance with the principle of the invention;

FIG. 5 shows a block diagram of a control program used in accordance with the principles of the invention;

FIG. 6 shows a block diagram of the programs and subroutines of the digital Electro Hydraulic and the automatic turbine startup and monitoring program in accordance with the principles of the invention;

FIG. 7 shows a block diagram of proportional-plus-reset controller program which is operable in accordance with the principles of the invention;

FIG. 8 shows a flow chart of the proportional-plus-reset subroutine (PRESET) which is operable in accordance with the principles of the invention;

FIG. 9 shows a block diagram of a proportional controller function with dead band which is operable in accordance with the principles of the invention;

FIG. 10 shows a flow chart of a speed loop (SPDLOOP) subroutine which is operable in accordance with the principles of the invention;

FIG. 11 shows a view of a part of an operator's control panel which is operable in accordance with the principles of the invention;

FIG. 12 shows a view of a part of the operator's control panel which is operable in accordance with the principles of the invention;

FIG. 13 shows a view of a portion of the operator's control panel which is operable in accordance with the principles of the invention;

FIG. 14 is a block diagram of the logic program which is operable in accordance with the principles of the invention;

FIG. 15 is a flow chart of a maintenance test logic program which is operable in accordance with the principles of the invention;

FIG. 16 is a flow chart of a transfer to manual operation subroutine which is operable in accordance with the principles of the invention;

FIG. 17 is a block diagram of a load control system which is operable in accordance with the principles of the invention;

FIG. 18 is a block diagram of a megawatt feedback loop subroutine which is operable in accordance with the principles of the invention;

FIG. 19 is a block diagram of an impulse pressure loop with megawatt loop in service which is operable in accordance with the principles of the invention;

FIG. 20 is a block diagram showing a panel task interaction function which is operable in accordance with the principles of the invention;

FIG. 21 is a block diagram of a panel program which is operable in accordance with the principles of the invention;

FIG. 22 is a block diagram showing a control task interface which is operable in accordance with the principles of the invention;

FIG. 23 is a block diagram showing a control program which is operable in accordance with the principles of the invention;

FIG. 24 shows a block diagram of an operating mode selection function which is operable in accordance with the principles of the invention;

FIGS. 25A and 25B show a flow chart of a select operating mode function which is operable in accordance with the principles of the invention;

FIG. 26 shows a symbolic diagram of the use of a speed/load reference function which is operable in accordance with the principles of the invention;

FIG. 27 is a block diagram showing a speed control function which is operable in accordance with the principles of the invention;

FIG. 28 shows a block diagram of the load control system which is operable in accordance with the principles of the invention;

FIG. 29 includes a flow chart of the load control system which is operable in accordance with the principles of the invention;

FIG. 30 shows a block diagram of the throttle valve control function which is operable in accordance with the principles of the invention;

FIG. 31 shows a mixed block diagram of a governor control function program which is operable in accordance with the principles of the invention;

FIG. 32 shows a block diagram of the Digital Electro Hydraulic System which is operable in accordance with the principles of the invention.

DESCRIPTION OF THE PREFERRED EMBODIMENT

A. POWER PLANT

More specifically, there is shown in FIG. 1 a large single reheat steam turbine constructed in a well known manner and operated and controlled in an electric power plant 12 in accordance with the principles of the invention. As will become more evident through this description, other types of steam turbines can also be controlled in accordance with the principles of the invention and particularly in accordance with the broader aspects of the invention. The generalized electric power plant shown in FIG. 1 and the more general aspects of the computer control system to be described in connection with FIG. 2 are like those disclosed in the aforementioned Giras and Birnbaum patent application Ser. No. 319,115. As already indicated, the present application is directed to general improvements in turbine operation and controlled as well as more specific improvements related to digital computer operation and control of turbines.

The turbine 10 is provided with a single output shaft 14 which drives a conventional large alternating current generator 16 to produce three-phase electric power (or any other phase electric power) as measured by a conventional power detector 18 which measures the rate of flow of electric energy. Typically, the generator 16 is connected through one or more breakers 17 per phase to a large electric power network and when so connected causes the turbo-generator arrangement to operate at synchronous speed under steady state conditions. Under transient electric load change conditions, system frequency may be affected and conforming turbo-generator speed changes would result. At synchronism, power contribution of the generator 16 to the network is normally determined by the turbine steam flow which in this instance is supplied to the turbine 10 at substantially constant throttle pressure.

In this case, the turbine 10 is of the multistage axial flow type and includes a high pressure section 20, an intermediate pressure section 22, and a lower pressure section 24. Each of these turbine sections may include a plurality of expansion stages provided by stationary vanes and an interacting bladed rotor connected to the shaft 14. In other applications, turbines operating in accordance with the present invention may have other forms with more or fewer sections tandemly connected to one shaft or compoundly coupled to more than one shaft.

The constant throttle pressure steam for driving the turbine 10 is developed by a steam generating system 26 which is provided in the form of a conventional drum type boiler operated by fossil fuel such as pulverized coal or natural gas. From a generalized standpoint, the present invention can also be applied to steam turbines associated with other types of steam generating systems such as nuclear reactor or once through boiler systems.

The turbine 10 in this instance is of the plural inlet front end type, and steam flow is accordingly directed to the turbine steam chest (not specifically indicated) through four throttle inlet valves TV1-TV4. Generally, the plural inlet type and other front end turbine types such as the single ended type or the end bar lift type may involve different numbers and/or arrangements of valves.

Steam is directed from the admission steam chest to the first high pressure section expansion stage through eight governor inlet valves GV1-GV8 which are arranged to supply steam to inlets arcuately spaced about the turbine high pressure casing to constitute a somewhat typical governor valving arrangement for large fossil fuel turbines. Nuclear turbines might on the other hand typically utilize only four governor valves.

During start-up, the governor valves GV1-GV8 are typically all fully opened and steam flow control is provided by a full arc throttle valve operation. At some point in the start-up process, transfer is made from full arc throttle valve control to full arc governor valve control because of throttling energy losses and/or throttling control capability. Upon transfer the throttle valves TV1-TV4 are fully opened, and the governor valves GV1-GV8 are normally operated in the single valve mode. Subsequently, the governor valves may be individually operated in a predetermined sequence usually directed to achieving thermal balance on the rotor and reduced rotor blade stressing while producing the desired turbine speed and/or load operating level. For example, in a typical governor valve control mode, governor valves GV5-GV8 may be initially closed as the governor valves GV1-GV4 are jointly operated from time to time to define positions producing the desired corresponding total steam flows. After the governor valves GV1-GV4 have reached the end of their control region, i.e., upon being fully opened, or at some overlap point prior to reaching their fully opened position, the remaining governor valves GV5-GV8 are sequentially placed in operation in numerical order to produce continued steam flow control at higher steam flow levels. This governor valve sequence of operation is based on the assumption that the governor valve controlled inlets are arcuately spaced about the 360.degree. periphery of the turbine high pressure casing and that they are numbered consecutively around the periphery so that the inlets corresponding to the governor valves GV1 and GV8 are arcuately adjacent to each other.

After the steam has crossed past the first stage impulse blading to the first stage reaction blading of the high pressure section, it is directed to a reheater system 28 which is associated with a boiler or steam generating system 26. In practice, the reheater system 28 may typically include a pair of parallel connected reheaters coupled to the boiler 26 in heat transfer relation as indicated by the reference character 29 and associated with opposite sides of the turbine casing.

With a raised enthalpy level, the reheated steam flows from the reheater system 28 through the intermediate pressure turbine section 22 and the low pressure turbine section 24. From the latter, the vitiated steam is exhausted to a condenser 32 from which water flow is directed (not indicated) back to the boiler 26.

Respective hydraulically operated throttle valve actuators indicated by the reference character 42 are provided for the four throttle valves TV1-TV4. Similarly, respective hydraulically operated governor valve acuators indicated by the reference character 44 are provided for the eight governor valves GV1-GV8. Hydraulically operated acuators indicated by the reference characters 46 and 48 are provided for the reheat stop and interceptor valves SV and IV. A computer monitored high pressure fluid supply 50 provides the controlling fluid for actuator operation of the valves TV1-TV4, GV1-GV8, SV and IV. A computer supervised lubricating oil system (not shown) is separately provided for turbine plant lubricating requirements.

The respective actuators 42, 44, 46 and 48 are of conventional construction, and the inlet valve actuators 42 and 44 are operated by respective stabilizing position controls indicated by the reference characters 50 and 52. If desired, the interceptor valve actuators 48 can also be operated by a position control 56 although such control is not employed in the present detailed embodiment of the invention. Each position control includes a conventional analog controller (not shown in FIG. 1) which drives a suitably known actuator servo valve (not indicated) in the well known manner. The reheat stop valve actuators 46 are fully open unless the conventional trip system or other operating means causes them to close and stops the reheat steam flow.

Since the turbine power is proportional to steam flow under the assumed control condition of substantially constant throttle pressure, steam valve positions are controlled to produce control over stream flow as an intermediate variable and over turbine speed and/or load as an end control variable or variables. Actuator operation provides the steam valve positioning, and respective valve position detectors PDT1-PDT4, PDG1-PDG8 and PDI are provided to generate respective valve position feedback signals for developing position error signals to be applied to the respective position controls 50, 52 and 56. One or more contact sensors CSS provides status data for the stop valving SV. The position detectors are provided in suitable conventional form, for example, they make conventional use of linear variable differential transformer operation in generating negative position feedback signals for algebraic summing with respect to position setpoint signals SP in developing the respective input error signals. Position controlled operation of the interceptor valving IV would typically be provided only under a reheat steam flow cutback requirement.

A speed detector 58 is provided for determining the turbine shaft speed for speed control and for frequency participation control purposes. The speed detector 58 can for example be in the form of a reluctance pickup (not shown) magnetically coupled to a notched wheel (not shown) on the turbo-generator shaft 14. In the detailed embodiment subsequently described herein, a plurality of sensors are employed for speed detection. Analog and/or pulse signals produced by the speed detector 58, the electric power detector 18, the pressure detectors 38 and 40, the valve position detectors PDT1-PDT4, PDG1-PDG8 and PDI, the status contact or contacts CSS, and other sensors (not shown) and status contacts (not shown) are employed in programmed computer operation of the turbine 10 for various purposes including controlling turbine performance on an on-line real time basis and further including monitoring, sequencing, supervising, alarming, displaying and logging.

B. DEH - COMPUTER CONTROL SYSTEM

As generally illustrated in FIG. 2, a Digital Electro-Hydraulic control system (DEH) 1100 includes a programmed digital computer 210 to operate the turbine 10 and the plant 12 with improved performance and operating characteristics. The computer 210 can include conventional hardware including a central processor 212 and a memory 214. The digital computer 210 and its associated input/output interfacing equipment is a suitable digital computer system such as that sold by Westinghouse Electric Corporation under the trade name of T2000. In cases when the steam generating system 26 as well as the turbine 10 are placed under computer control, use can be made of one or more P2000 computers or alternatively a larger computer system such as that sold by Xerox Data Systems and known as the Sigma 5. Separate computers, such as P2000 computers, can be employed for the respective steam generation and turbine control functions in the controlled plant unit and interaction is achieved by interconnecting the separate computers together through data links or other means.

The digital computer used in the DEH control system 1100 is a P2000 computer which is designed for real time process control applications. The P2000 typically uses a 16 bit word length with 2's complement, a single address and fixed word length operated in a parallel mode. All the basic DEH system functions are performed with a 16,000 word (16K), 3 microsecond magnetic core memory. The integral magnetic core memory can be expanded to 65,000 words (65K).

The equipment interfacing with the computer 210 includes a contact interrupt system 124 which scans contacts representing the status of various plant and equipment conditions in plant wiring 1126. The status contacts might typically be contacts of mercury wetted relays (not shown) which operate by energization circuits (not shown) capable of sensing the predetermined conditions associated with the various system devices. Data from status contacts is used in interlock logic functioning and control for other programs, protection analog system functioning, programmed monitoring and logging and demand logging, etc.

Operator's panel buttons 1130 transmit digital information to the computer 2010. The operator's panel buttons 1130 can set a load reference, a pulse pressure, megawatt output, speed, etc.

In addition, interfacing with plant instrumentation 1118 is provided by an analog input system 1116. The analog input system 1116 samples analog signals at a predetermined rate from predetermined input channels and coverts the signals sampled to digital values for entry into the computer 210. The analog signals sensed in the plant instrumentation 1118 represent parameters including the impulse chamber pressure, the megawatt power, the valve positions of the throttle valves TV1 through TV4 and the governor valves GV1 through GV8 and the interceptor Valve IV, throttle pressure, steam flow, various steam temperatures, miscellaneous equipment operating temperature, generator hydrogen cooling pressure and temperature, etc. A detailed list of all parameters is provided in the appendix 1. Such parameters include process parameters which are sensed or controlled in the process (turbine or plant) and other variables which are defined for use in the programmed computer operation. Interfacing from external systems such as an automatic dispatch system is controlled through the operator's panel buttons 1130.

A conventional programmer's console and tape reader 218 is provided for various purposes including program entry into the central processor 212 and the memory 214 thereof. A logging typewriter 1146 is provided for logging printouts of various monitored parameters as well as alarms generated (ATS) which includes program system blocks 1140, 1142, 1144 (FIG. 6) in the DEH control system 1100. A trend recorder 1147 continuously records predetermined parameters of the system. An interrupt system 124 is provided for controlling the input and output transfer of information between the digital computer 210 and the input/output equipment. The digital computer 210 acts on interrupt from the interrupt system 124 in accordance with an executive program. Interrupt signals from the interrupt system 124 stop the digital computer 210 by interrupting a program in operation. The interrupt signals are serviced immediately.

Output interfacing is provided by contacts 1128 for the computer 210. The contacts 1128 operate status display lamps, and they operate in conjunction with a conventional analog/output system and a valve position control output system comprising a throttle valve control system 22o and a governor valve control system 222. A manual control system, is coupled to the valve position control output system 220 and is operable therewith to provide manual turbine control during computer shut-down. The throttle and governor valve control system 220 and 222 correspond to the valve position controls 50 and 52 and the actuators 42 and 44 in FIG. 1. Generally, the manual control system is similar to those disclosed in prior U.S. Pat. No. 3,552,872 by T. Giras et al and U.S. Pat. No. 3,741,246 by A. Braytenbah, both assigned to the present assignee.

Digital output data from the computer 210 is first converted to analog signals in the analog output system 224 and then transmitted to the valve control system 220 and 222. Analog signals are also applied to auxiliary devices and systems, not shown, and interceptor valve systems not shown.

C. SUBSYSTEMS EXTERNAL TO THE DEH COMPUTER

Making reference now to FIGS. 3A-3C, a hardwired digital/analog system forms a part of the DEH control system 1100 (FIG. 2). Structurally, it embraces elements which are included in the blocks 50, 52, 42 and 44 of FIG. 1 as well as additional elements. A hybrid interface 510 is included as a part of the hardwired system. The hybrid interface 510 is connected to actuator system servoamplifiers 414 for the various steam valves which in turn are connected to a manual controller 516, an overspeed protection controller, not shown, and redundant DC power supplies, not shown.

A controller shown in FIG. 3A is employed for throttle valve TV1-TV4 control in the TV control system 50 of FIG. 1. The governor valves GV1-GV8 are controlled in an analogous fashion by the GV control system 52.

While the steam turbine is controlled by the digital computer 210, the hardwired system 511 tracks single valve analog outputs 520 from the digital computer 210. A comparator 518 compares a signal from a digital-to-analog converter 522 of the manual system with the signal 520 from the digital computer 210. A signal from the comparator 518 controls a logic system 524 such that the logic system 524 runs an up-down counter 526 to the point where the output of the converter 522 is equal to the output signal 520 from the digital computer 210. Should the hardwired system 511 fail to track the signal 520 from the digital computer 210 a monitor light will flash on the operator's panel.

When the DEH control system reverts to the control of the backup manual controller 516 as a result of an operator selection or due to a contingency condition, such as loss of power on the automatic digital computer 210, or a stoppage of a function in the digital computer 210, or a loss of a speed channel in the wide range speed control all as described in greater detail infra, the input of the valve actuation system 322 is switched by switches 528 from the automatic controllers in the blocks 50, 52 (FIG. 1) or 220, 222 (FIG. 2) to the control of the manual controller 516. Bumpless transfer is thereby accomplished between the digital computer 210 and the manual controller 516.

Similarly, tracking is provided in the computer 210 for switching bumplessly from manual to automatic turbine control. As previously indicated, the presently disclosed hybrid structural arrangement of software and hardware elements is the preferred arrangement for the provision of improved turbine and plant operation and control with backup capability. However, other hybrid arrangements can be implemented within the field of application of the invention.

D. DEH PROGRAM SYSTEM

DEH Program System Organization, DEH Control Loops And Control Task Program

With reference now to FIG. 4, an overall generalized control system of this invention is shown in block diagram form. The digital electrohydraulic (DEH) control system 1100 operates valve actuators 1012 for the turbine 10. The digital electrohydraulic control system 1100 comprises a digital computer 1014, corresponding to the digital computer 210 in FIG. 2, and it is interconnected with a hardwired analog backup control system 1016. The digital computer 1014 and the backup control system 1016 are connected to an electronic servo system 1018 corresponding to blocks 220 and 222, in FIG. 2. The digital computer control system 1014 and the analog backup system 1016 track each other during turbine operations in the event it becomes necessary or desirable to make a bumpless transfer of control from a digital computer controlled automatic mode of operation to a manual analog backup mode or from the manual mode to the digital automatic mode.

In order to provide plant and turbine monitor and control functions and to provide operator interface functions, the DEH computer 1014 is programmed with a system of task and task support programs. The program system is organized efficiently and economically to achieve the end operating functions. Control functions are achieved by control loops which structurally include both hardware and software elements, with the software elements being included in the computer program system. Elements of the program system are considered herein to a level of detail sufficient to reach an understanding of the invention. More functional detail on various programs is presented in Appendix 2. Further, a detailed listing of a DEH system program substantially conforming to the description presented herein is presented in Appendix 3 in symbolic and machine language. Most of the listing is compiled by a P2000 compiler from instructions written in Fortran IV. A detailed dictionary of system parameters is presented in Appendix 1, and a detailed computer input/output signal list is presented in Appendix 4. Appendix 5 mainly provides additional hardware information related to the hardwired system previously considered as part of the DEH control system.

As previously discussed, a primary function of the digital electrohydraulic (DEH) system 1100 is to automatically position the turbine throttle valves TV1 through TV4 and the governor valves GV1 through GV8 at all times to maintain turbine speed and/or load. A special periodically executed program designated the CONTROL task is utilized by the P2000 computer along with other programs to be described in greater detail subsequently herein.

With reference now to FIG. 5, a functional control loop diagram in its preferred form includes the CONTROL task or program 1020 which is executed in the computer 1010. Inputs representing demand and rate provide the desired turbine operating setpoints. The demand is typically either the target speed in specified revolutions per minute of the turbine systems during startup or shutdown operations or the target load in megawatts of electrical output to be produced by the generating system 16 during load operations. The demand enters the block diagram configuration of FIG. 5 at the input 1050 of a compare block 1052.

The rate input either in specified RPM per minute or specified megawatts per minute, depending upon which input is to be used in the demand function, is applied to an integrator block 1054. The rate inputs in RPM and megawatts of loading per minute are established to limit the buildup of stresses in the rotor of the turbine-generator 10. An error output of the compare block 1052 is applied to the integrator block 1054. In generating the error output the demand value is compared with a reference corresponding to the present turbine operating setpoint in the compare block 1052. The reference value is representative of the setpont RPM applied to the turbine system or the setpoint generator megawatts output, depending upon whether the turbine generating system is in the speed mode of operation or the load mode of operation. The error output is applied to the integrator 1054 so that a negative error drives the integrator 1054 in one sense and a positive error drives it in the opposite sense. The polarity error normally drives the integrator 1054 until the reference and the demand are equal or if desired until they bear some other predetermined relationship with each other. The rate input to the integrator 1054 varies the rate of integration, i.e. the rate at which the reference or the turbine operating setpoint moves toward the entered demand.

Demand and rate input signals can be entered by a human operator from a keyboard. Inputs for rate and demand can also be generated or selected by automatic synchronizing equipment, by automatic dispatching system equipment external to the computer, by another computer automatic turbine startup program or by a boiler control system. The inputs for demand and rate in automatic synchronizing and boiler control modes are preferably discrete pulses. However, time control pulse widths or continuous analog input signals may also be utilized. In the automatic startup mode, the turbine acceleration is controlled as a function of detected turbine operating conditions including rotor thermal stress. Similarly, loading rate can be controlled as a function of detected turbine operating conditions.

The output from the integrator 1054 is applied to a breaker decision block 1060. The breaker decision block 1060 checks the state of the main generator circuit breaker 17 and whether speed control or load control is to be used. The breaker block 1060 them makes a decision as to the use of the reference value. The decision made by the breaker block 1060 is placed at the earliest possible point in the control task 1020 thereby reducing computational time and subsequently the duty cycle required by the control task 1020. If the main generator circuit breaker 17 is open whereby the turbine system is in wide range speed control the reference is applied to the compare block 1062 and compared with the actual turbine generator speed in a feedback type control loop. A speed error value from the compare block 1062 is fed to a proportional plus reset controller block 1068, to be described in greater detail later herein. The proportional plus reset controller 1068 provides an integrating function in the control task 1060 which reduces the speed error signal to zero. In the prior art, speed control systems limited to proportional controllers are unable to reduce a speed error signal to zero. During manual operation an offset in the required setpoint in no longer required in order to maintain the turbine speed at a predetermined value. Great accuracy and precision of turbine speed whereby the turbine speed is held within one RPM over tens of minutes is also accomplished. The accuracy of speed is so high that the turbine 10 can be manually synchronized to the power line without an external synchronizer typically required. An output from the proportional plus reset controller block 1068 is then processed for external actuation and positioning of the appropriate throttle and/or governor valves.

If the main generator circuit breaker 17 is closed, the CONTROL task 1020 advances from the breaker block 1060 to a summer 1072 where the REFERENCE acts as a feedforward setpoint in a combined feedforward-feedback load control system. If the main generator circuit breaker 17 is closed, the turbine generator system 10 is being loaded by the electrical network connected thereto.

In the control task 1020 of the DEH system 1100 utilizes the summer 1072 to compare the reference value with the output of speed loop 1310 in order to keep the speed correction independent of load. A multiplier function has a sensitivity to varying load which is objectionable in the speed loop 1310.

During the load mode of operation the DEMAND represents the specified loading in MW of the generator 16 which is to be held at a predetermined value by the DEH system 1100. However, the actual load will be modified by any deviations in system frequency in accordance with a predetermined regulation value. To provide for frequency participation, a rated speed value in box 1074 is compared in box 1078 with a "two signal" speed value represented by box 1076. The two signal speed system provides high turbine operating reliability to be described infra herein. An output from the compare function 1078 is fed through a function 1080 which is similar to a proportional controller which converts the speed error value in accordance with the regulation value. The speed error from the proportional controller 1080 is combined with the feedforward megawatt reference, i.e., the speed error and the megawatt reference are summed in summation function or box 1072 to generate a combined speed compensated reference signal.

The speed compensated load reference is compared with actual megawatts in a compare box or function 1082. The resultant error is then run through a proportional plus reset controller represented by program box 1084 to generate a feedback megawatt trim.

The feedforward speed compensated reference is trimmed by the megawatt feedback error multiplicatively to correct load mismatch, i.e. they are multiplied together in the feedforward turbine reference path by multiplication function 1086. Multiplication is utilized as a safety feature such that if one signal e.g. MW should fail a large value would not result which could cause an overspeed condition but instead the DEH system 1100 would switch to a manual mode. The resulting speed compensated and megawatt trimmed reference serves as an impulse pressure setpoint in an impulse pressure controller and it is compared with a feedback impulse chamber pressure representation from input 1088. The difference between the feedforward reference and the impulse pressure is developed by a comparator function 1090, and the error output therefrom functions in a feedback impulse pressure control loop. Thus, the impulse pressure error is applied to a proportional plus reset controller function 1092.

During load control the megawatt loop comprising in part blocks 1082 and 1084 may be switched out of service leaving the speed loop 1310 and an impulse pressure loop operative in the DEH system 1100.

Impulse pressure responds very quickly to changes of load and steam flow and therefore provides a signal with minimum lag which smooths the output response of the turbine generator 10 because the lag dynamics and subsequent transient response is minimized. The impulse pressure input may be switched in and out from the compare function 1090. An alternative embodiment embracing feedforward control with impulse feedback trim is applicable.

Between block 1092 and the governor valves GV1-GV8 a value characterization function for the purpose of linerizing the response of the valve is interposed. The value characterization function described in detail in Appendix III infra herein is utilized in both automatic modes and manual modes of operation of the DEH system 1100. The output of the proportional plus reset controller function 1092 is then ultimately coupled to the governor valves GV1-GV8 through electrohydraulic position control loops implemented by equipment considered elsewhere herein. The proportional plus reset controller output 1092 causes positioning of the governor valves GV1-GV8 in load control to achieve the desired megawatt demand while compensation is made for speed, megawatt and impulse pressure deviations from desired setpoints.

Making reference to FIG. 6, the control program 1020 is shown with interconnections to other programs in the program system employed in the Digital Electro Hydraulic (DEH) system 1100. The periodically executed program 1020 receives data from a logic task 1110 where mode and other decisions which affect the control program are made, a panel task 1112 where operator inputs may be determined to affect the control program, an auxiliary synchronizer program 1114 and an analog scan program 1116 which processes input process data. The analog scan task 1116 receives data from plant instrumentation 1118 external to the computer as considered elsehwere herein, in the form of pressures, temperatures, speeds, etc. and converts such data to proper form for use by other programs. Generally, the auxiliary synchronizer program 1114 measures time for certain important events and it periodically bids or runs the control and other programs. An extremely accurate clock function 1120 operates through a monitor program 1122 to run the auxiliary synchronizer program 1114.

The monitor program or executive package 1122 also provides for controlling certain input/output operations of the computer and, more generally, it schedules the use of the computer to the various programs in accordance with assigned priorities. For more detail on the P2000 computer system and its executive package, reference is made to Appendix 4. In the appendix description, the executive package is described as including analog scan and contact closure input routines, whereas these routines are considered as programs external to the executive package in this part of the disclosure.

The logic task 1110 is fed from outputs of a contact interrupt or sequence of events program 1124 which monitors contact variables in the power plant 1126. The contact parameters include those which represent breaker state, turbine auto stop, tripped/latched state interrogation data states, etc. Bids from the interrupt program 1124 are registered with and queued for execution by the executive program 1111. The control program 1110 also receives data from the panel task 1112 and transmits data to status lamps and output contacts 1128. The panel task 1112 receives data instruction based on supervision signals from the operator panel buttons 1130 and transmits data to panel lamps 1132 and to the control program 1020. The auxiliary synchronizer program 1114 synchronizes through the executive program 1111 the bidding of the control program 1020, the analog scan program 1116, a visual display task 1134 and a flash task 1136. The visual display task transmits data to display windows 1138.

The control program 1020 receives numerical quantities representing process variables from the analog scan program 1116. As already generally considered, the control program 1020 utilizes the values of the various feedback variables including turbine speed, impulse pressure and megawatt output to calculate the position of the throttle valves TV1-TV4 and governor valves GV1-GV8 in the turbine system 10, thereby controlling the megawatt load and the speed of the turbine 10.

To interface the control and logic programs efficiently, the sequence of events program 1124 normally provides for the logic task 1110 contact status updating on demand rather than periodically. The logic task 1110 computes all logical states according to predetermined conditions and transmits this data to the control program 1020 where this information is utilized in determining the positioning control action for the throttle valves TV1-TV4, and the governor valves GV1-GV8. The logic task 1110 also controls the state of various lamps and relay type contact outputs in a predetermined manner.

Another important part of the DEH system is the OPERATOR'S PANEL program. The operator communicates through the panel with the DEH control programs by means of various buttons which have assigned functions. When any button is pressed, a special interrupt is generated; this interrupt triggers a PANEL INTERRUPT program which decodes the button pressed, and then bids the PANEL task. The PANEL program processes the button and takes the proper action, which usually means manipulating some panel lamps, as well as passing on the button information to both the LOGIC and the CONTROL tasks.

The Operator's Panel also has two sets of display windows which allow display of all turbine program parameters, variables, and constants. A visual display task presents this information in the windows at the request of the operator through various dedicated display buttons and a numerical keyboard. The visual display values are periodically updated in the windows as the quantity changes.

Certain important turbine operating conditions are communicated to the DEH operator by way of flashing lamps on the panel. Therefore a special FLASH program is part of the DEH system. Its function is to monitor and detect such contingency conditions, and flash the appropriate lamp to alert the operator to the state.

E. DEH PROGRAMS OR TASKS

1. PRESET SUBROUTINE

Making reference now to FIG. 7, a functional diagram of the proportional plus reset controller task program 1068 of FIG. 5 is shown in greater detail. The proportional plus reset controller subroutine 1068 is called by the control program 1020 of FIG. 5 when the DEH turbine control system 1100 is in the speed mode of control and also when the DEH turbine control system 1100 is in the load mode of control with the megawatt and impulse pressure feedback loops in service. As already indicated utilizing a proportional plus reset function during speed control provides very accurate control of the angular velocity of the turbine system.

The proportional plus reset controler 1068 provides an output which is composed of the sum of two parts. One part of the output is proportional to an input and the other part is an integral of the input. Therefore, instantaneous response is available as well as the capability of zero input error. A setpoint or dynamic reference from a demand source is applied to an input 1210 of a difference function 1212. The difference function 1212 compares the input and the actual controlled process value. An output from the difference function 1212 is fed to a proportional gain function 1216 and to an input of an integrator or integrating function 1218 having a rest time TR. An output from the integrator 1218 is high and low limited by the program as represented by the reset windup prevention function 1220 in order to avoid excessive integrator outputs which could occur with a reset windup.

Proportional and integral outputs from the gain function 1216 and the windup limited integrator 1218 are summed in a summing function 1222. The total output from the summing function 1222 is high and low limited by another function 1224 and fed to a process function 1226 thereby limiting the total output to a useful output range.

Making reference now to FIG. 8, a pictorial representation of a flow chart for the proportional plus reset controller program is shown. In the preferred embodiment the Preset program is designed such that a call from the control program 1030 provides a list of variables necessary to evaluate the controller 1068 output. The structure of the subroutine is indicated by the Fortran statement given below.

SUBROUTINE PRESET (ERR, ERRX, G, TR, HL, XLL, RES, PRES)

The variables in the above equation are defined as follows:

English Language FORTRAN Variables Equivalents ______________________________________ ERR -- The current input ERRX -- The last input G -- The controller proportional gain TR -- The controller reset time HL -- The controller high limit XLL -- The controller low limit RES -- The controller integral output PRES -- The controller total output. ______________________________________

Again making reference to FIG. 8, where standard FORTRAN notation is used, the Preset subroutine 1068 first evaluates the integral part of the controller output according to equation: ##EQU1## The subroutine 1068 next saves the current input ERR in storage location ERRX 1250 for the following call to the subroutine 1068. The controller integral output RES 1252 is then checked against the high limit 1254 and the low limit 1256 to prevent reset/windup. The proportional part of the output is computed and added to the integral part of the output integrator 1218 to form the total output PRES 1258. PRES 1258 is checked against high limit 1260 and low limit 1262 after which the proportional plus reset controller subroutine 1068 returns to the control task 1020.

As previously considered, the proportional plus reset controller subroutine 1068 is used by the control task program 1020 during three different phases of operation of the turbine system. During startup of the turbine system 10, the proportional plus reset controller subroutine program 1068 is used as a speed controller in order to regulate and hold the speed of the turbine 10 at a predetermined value or at a predetermined acceleration rate. Because of the integral function of the proportional plus reset controller subroutine program 1068 the speed of the turbine system 10 can be held to within 1 rpm. Also, in order for an operator to keep the speed of the turbine system 10 at a predetermined value, an error offset input signal typical of a purely proportional system is not required. Therefore, the reference and the controlled variable, both turbine speed in this case, will be equal. The proportional plus reset controller subroutine program 1068 is also used in the megawatt controller feedback loop and the impulse chamber pressure controller feedback loop.

During turbine startup, the quantity REFDMD is the internal speed reference while WS is the actual turbine speed. GS1 and T1 are the proportional gain and reset time, HLS and O. are the high and low limits, RESSPD is the integral part of the output, SPDSP is the total output, and RESSPDX is the last value of the input.

In the megawatt controller during megawatt loop operation, REF1 is the megawatt set point, MW is the megawatt feedback, and GR2 is a ranging gain to convert from engineering units to per-unit form. GL2 and T2 are the proportional gain and the reset time, while HEL and LEL are high and low limits. RESMW is the integral output, Y is the total output, and RESMWX is the last input.

With impulse pressure loop operation, PISP is the set point for the impulse pressure controller, PI is the feedback and GL3 and T3 are the proportional gain and the reset time. GR4 and 0. are the high and low limits, RESPI is the integral output, VSP is the total output, and RESPIX is the last input.

RESET INTEGRATOR ALGORITHM

To perform the mathematical function of integration in a digital computer it is desirable to use numerical techniques to approximate the exact value of the integral. In the preferred embodiment, the algorithm uses the trapezoidal rule for integration and it is simple in format, requires little computer storage and is executed very rapidly. The algorithm uses one value of input past history to achieve a high degree of accuracy.

The following algorithm is used in the computer: ##EQU2## Definitions of the terms in this equation follow: (N) -- The current instant of real tme

(N-1) -- The last instant of real time.

Dt -- the sampling interval, or the time duration between evaluations of the integration algorithm. In the DEH Control System this is normally 1 sec.

Tr -- the controller reset time in sec.

X(n) -- the current value of the input.

X(n-1) -- the last value of the input.

Y(n) -- the current value of the output.

Y(n-1) -- the last value of the output.

To use the integrator algorithm, the DEH control system is organized so that the parameters DT and TR, the input variables X(N) and X(N-1), and the output variables Y(N) and Y(N-1) are in known areas of COMMON storage. The CONTROL task computes the current value of X(N) and calls the PRESET subroutine. The PRESET subroutine evaluates the current value of Y(N) according to the integrator algorithm and stores the value for use by all other parts of the DEH system.

2. SPEED LOOP SUBROUTINE

Making reference now to FIG. 9, a speed loop program 1310 which functionally is part of the arrangement shown in FIG. 5 is shown in greater detail. The speed loop (SPDLOOP) program 1310 normally computes data required in the functioning of the speed feedback loop in the load control comprising as shown in FIG. 5 the rated speed reference 1074, the actual turbine speed 1076, the compare function 1078, the proportional controller 1080 and the summing function 1072. During the load control, the speed feedback loop adjusts the load reference (and thus the governor valves) to correct for any turbine speed deviation from rated speed. The speed feedback loop uses a proportional controller to accomplish this function. The speed loop subroutine 1310 is called upon to perform speed control loop functions by the control program 1020. In FIG. 9, the functioning of the proportional controller 1080 is shown in detail. The error output from the compare function 1078 is fed through a deadband function 1312. A proportionality constant (GR1) 1314 and a high limit function (HLF) 1316 are included in the computation.

The speed loop (SPDLOOP) subroutine is called by the Control Task during the load control mode and when switching occurs between actual speed signals. Subroutine form reduces the requirement for memory storage space thereby reducing the computer expense required for operation of the DEH system 1100.

The deadband function 1312 provides for bypassing small noise variations in the speed error generated by the compare function 1078 so as to prevent turbine speed changes which would otherwise occur. Systems without a deadband continuously respond to small variations which are random in nature resulting in undue stress in the turbine 10 and unnecessary, time and duty cycle consuming operation of the control system. A continuous hunting about the rated speed due to the gain of the system would occur without the deadband 1312. The speed regulation gain GR1 at 1314 is set to yield rated megawatt output power speed correction for a predetermined turbine speed error. The high limit function HLS at 1316 provides for a maximum speed correction factor.

The turbine speed 1076 is derived from three transducers. The turbine digital speed transducer arrangement is that disclosed in greater element and system implementation detail in the aforementioned Reuther Application Ser. No. 412,513. Briefly, in the preferred embodiment for determining the speed of the turbine, the system comprises three independent speed signals. These speed signals consist of a very accurate digital signal generated by special electronic circuitry from a magnetic pickup, an accurate analog signal generated by a second independent magnetic pickup, and a supervisory analog instrument signal from a third independent pickup. The DEH system compares these signals and through logical decisions selects the proper signal to use for speed control or speed compensated load control. This selection process switches the signal used by the DEH control system 1100 from the digital channel signal to the accurate analog channel signal or vice versa under predetermined dynamic conditions. In order to hold the governor valves at a fixed position during this speed signal switching the control program 1020 uses the speed loop subroutine 1310 and performs a computation to maintain a bumpless speed signal transfer.

Making reference to FIG. 10, the speed loop (SPDLOOP) subroutine flow chart 1310 is shown in greater detaiil. Two FORTRAN statements signify the operations of the speed loop subroutine program flow chart 1310. These statements are:

Call spdloop

ref1 = refdmd + x

variables in the flow chart 1310 are defined as follows:

FORTRAN VARIABLES ENGLISH LANGUAGE EQUIVALENT ______________________________________ REFMD Load reference WR The turbine rated speed REFl Corrected load reference WS The actual turbine speed TEMP Temporary storage location variable SPDB The speed deadband GRl The speed regulation gain (normally set to yield rated megawatt speed correction for a 180 rpm speed error) X Speed correction factor HLF The high limit function. ______________________________________

AUXILIARY SYNCHRONIZER PROGRAM

3. OPERATOR'S PANEL

Referring now to FIGS. 11, 12 and 13, the control panel 1130 for the digital electrohydraulic system 1100 is shown in detail. Specified functions have control panel buttons which flash in order to attract the attention of an operator. The FLASH task has two functions: it flashes appropriate lights to alert the operator to various important conditions in the DEH system, and it sets contact outputs to pass these same conditions to the Analog Backup and Boiler Control Systems The FLASH task is on priority level 5 and is bid by the AUX SYNC task every 1/2 sec.

The concept behind the FLASH task is that flashing will attract the operator's attention much more quickly than simply maintaining a steady on condition. Most of the flashing lights indicate contingency conditions; a few indicate such things as invalid keyboard entries or that the DEH system is ready to go on automatic control. The flashing frequency is set at 1/2 sec on and 1/2 sec off as long as the condition exists. At the termination of the flashing condition, the corresponding lights and contacts are turned off.

A total of nine conditions are continually monitored for flashing by the FLASH task. These are listed below with a brief description of each.

______________________________________ 1. Reference Low The turbine load reference is - Limit being limited by the low load limit. 2. Reference High The turbine load reference is Limit being limited by the high load limit. 3. Valve Position The turbine governor valve output Limit is being limited by the valve position limit. 4. Throttle Pressure The turbine load reference is Limit being run back because throttle pressure is below set point. No light is flashed in this case but a contact output is set during the throttle pressure limiting. 5. DEH Ready for The DEH control system has tracked Automatic the manual backup system and is ready to go on automatic control. 6. Valve Status While on automatic control, the Contingency DEH system has detected a valve LVDT position not in agreement with its corresponding analog output. 7. Governor Valve A governor valve LVDT position Contingency is not in agreement with its analog output. 8. Throttle Valve A throttle valve LVDT position Contingency is not in agreement with its analog output. 9. Invalid Request An invalid keyboard entry has been made. ______________________________________

In order to determine whether to flash a light or to suppress flashing, the FLASH task maintains two arrays in core memory. One of these is called LIMIT and contains the current value of the nine limiting or flashing conditions listed above, as they are set by various other DEH programs. The second array is called OLDLIMIT and is an image of the immediate past value of the LIMIT array. These two arrays are examined every 1/2 sec by the FLASH task according to the following table of combinations:

FLASH TASK LAMP COMBINATIONS ______________________________________ LIMIT OLDLIMIT Action ______________________________________ 0 0 Do Nothing 0 1 Turn Light Off 1 0 Turn Light On 1 1 Turn Light Off ______________________________________

After the proper action is taken by the FLASH task, the OLDLIMIT array is then updated to agree with the current limit array for the next pass through the task 1/2 sec later.

A third array called CCOFLAG is also maintained by the FLASH task in order to set contact outputs when a limiting condition exists. The contact outputs are not set and reset regularly (as are the flashing lights) but rather the contacts are set and remain on as long as the flashing condition exists. When the flashing condition ceases the contacts are reset. A table of combinations illustrating this action follows:

FLASH TASK CONTACT COMBINATIONS ______________________________________ LIMIT CCOFLAG Action ______________________________________ 0 0 Do Nothing 0 1 Reset Contact 1 0 Set Contact 1 1 Do Nothing ______________________________________

It should be noted that only the first five flash conditions listed above have contact outputs associated with them; the remaining four simply flash Operator's Panel lights.

The control of the operation of the DEH control system 1100 is greatly facilitated for the operator by the novel layout of the operator's panel 1130, the flashing and warning capabilities thereof, and the interface provided with the turbine control and monitor functions through the pushbutton switches. In addition, simulated turbine operation is provided by the DEH system for operator training or other purposes through the operation of the appropriate panel switches during turbine down time. Further, it is noteworthy that manual and automatic operator controls are at the same panel location for good operator interface under all operating conditions.

4. LOGIC TASK

The LOGIC task determines the operational status of the DEH turbine control system from information provided by the plant, the operator, and other DEH programs. A contact input from the plant wiring triggers the sequence of events or interrupt program which calls upon the plant contact closure input subroutine which in turn requests that the logic program be executed by the setting of a flag called RUNLOGIC in the logic program. The logic program is also run by the panel interrupt program which calls upon the panel task program to run the logic program in response to panel button operations. The control task program in performing its various computations and decisions will sometimes request the logic program to run in order to update conditions in the control system. FIG. 14 shows a block diagram of the logic program 1110.

The mechanism for actual execution of the LOGIC program is provided by the AUX SYNC task, which runs every 1/10 sec and carries out the scheduled and demand bidding of various tasks in the DEH system. AUX SYNC checks the state of the RUNLOGIC flag and, if it is set, bids the LOGIC task immediately. Thus, the maximum response time for LOGIC requests is 1/10 sec; on the average the response will be much faster than this.

In order to allow immediate rerunning of the LOGIC task should system conditions require, the LOGIC program first resets RUNLOGIC. Thus any other program may then set RUNLOGIC and request a bid which will be carried out by the AUX SYNC program withiin 1/10 sec. There are two major results of the LOGIC task: the computation of all logic states necessary for proper operation of the DEH system, and the processing of all status and monitor lamp contact outputs to inform the plant control system and operating personnel of the state of the DEH system.

The logic program 1110 controls a series of tests which determine the readiness and operability of the DEH system 1100. One of these tests is that for the overspeed protection controller which is part of the analog backup portion of the hardwired system 1016 shown in FIG. 4. Generally, the logic program 1110 is structured from a plurality of subroutines which provide the varying logic functions for other programs in the DEH program system, and the various logic subroutines are all sequentially executed each time the logic program is run.

LOGIC CONTACT CLOSURE OUTPUT SUBROUTINE

The logic task 1110 includes a subroutine called a logic contact closure output subroutine therein. The logic contact closure output subroutine updates all the digital outputs to the status lamps and contacts for transmission thereto. The logic program 1110 handles a great number of contact outputs thereby keeping the output logic states of the DEH computer current. Thus, the logic contact closure output subroutine 1910 reduces the total storage requirements otherwise required for the logic program 1110.

In addition, certain logical variables, which are normally set by the PANEL task, must be aligned by the LOGIC task with conditions as they exist instant by instant in the power plant. To do these functions in-line for each contact output in the LOGIC task would take considerable core storage to accommodate the individual situations.

MAINTENANCE TEST

In order to take advantage of the full flexibility, adjustability and dynamic response of the DEH system 1100 a maintenance test system 1810 is provided, a logic flow chart of which is shown in FIG. 15. The maintenance test program 1810 allows an operator to change, adjust or tune a large number of operational parameters and constants of the DEH system 1100. The contents of the DEH system 1100 can therefore be modified without extensive adjustment or reprogramming. An operator is able to optimize the DEH system 1100 from the control panel 1130 as shown in FIGS. 11 and 12 which allows for an essentially infinite variability in the choice of constants. Great flexibility and control is therefore available to an operator.

In addition, the maintenance test program 1810 of FIG. 15 allows an operator to use a simulation mode for operator training purposes.

COMPUTER SET MANUAL LOGIC

When the DEH system is in automatic control, it is possible for certain conditions to occur which require transfer to manual operator control. One of these is the case in which the maintenance test switch is moved to the test position. Even though a wired connection places the control in manual operation, the DEH LOGIC program sets a contact output requesting transfer to manual as a backup. The second situation occurs when the turbine is on automatic speed control and all speed input signals fail, as determined by the speed selection program in the CONTROL task. This speed channel failure will also require transfer to manual operation by a contact output from this LOGIC task.

FIG. 16 shows a flow chart of a transfer to manual operation subroutine.

STM is the logical variable to switch to turbine manual control, and is set by the maintenance test contact input (OPRT) or the speed channel failure variable (SPFT) while on speed control (i.e. the main breaker (BR) is not set). A call to the LCCO subroutine is then made.

MEGAWATT FEEDBACK LOGIC

Megawatt feedback is one of the two major loops used on turbine load control to maintain the governor valves at the correct position. The other feedback is impulse pressure; between these two loops it is possible to adapt the computer outputs to account for valve non-linearities and to assure that the megawatt setting in the reference window is actually being supplied by the turbine/generator.

The megawatt feedback logic places the megawatt loop in service on request from an operator's panel pushbutton, providing all permissive conditions are satisfied, and removes the loop from service from the operator's panel pushbutton or when any condition exists which requires removing the megawatt feedback. Placing the loop in service or removing it is done bumplessly, so that the governor valves remain at the same position. In addition, the REFERENCE and DEMAND values are automatically adjusted to agree with the new state of the DEH control system.

Referring to FIG. 18, a block diagram of the megawatt feedback loop is shown in greater detail than in FIG. 5. It should be noted that the speed compensated reference 1087, at the input of multiplication function 1086, is multiplied by the megawatt compensation 1089. The multiplication of the signals instead of a differencing provides an additional safety feature since the loss of either of the signals 1087 or 1089 will produce a zero output rather than a runaway condition.

IMPULSE PRESSURE FEEDBACK LOGIC

Impulse pressure feedback is the other of the two major loops used in the turbine load control to maintain the governor valves at the correct position. The impulse pressure feedback logic places the impulse pressure feedback loop in service on request from an operator's panel pushbutton, providing all permissive conditions are satisfied, and removes the loop from service on request from the operator or when any condition exists which requires removing impulse pressure feedback. Placing the loop in service or removing it is done automatically and bumplessly, so that the governor valves remain at the same position.

The impulse pressure feedback logic is shown in greater detail in FIG. 19. With a digital computer, bumpless transfer is achieved without the use of elaborate external circuitry because of the digital computational nature of the machine. A value can be computed instantaneously and inserted in the integrator 1218 of the proportional plus reset controller subroutine 1068 as shown in FIG. 7. In the preferred embodiment of the Digital Electro-Hydraulic control system 1100, the proportional plus reset controller 1168 is utilized by the following functions: the megawatt feedback loop 1091, the impulse pressure feedback loop 1816 and the speed feedback loop made up of the rated speed reference 1074, the compare function 1076 and the actual turbine speed function 1076.

5. PANEL TASK

The DEH Operator's Panel is the focal point of turbine operation; it has been designed to make use of the latest digital techniques to provide maximum operational capability. The Operator's Panel provides the primary method of communicating information and control action between the operator and the DEH Control System. This is accomplished through a group of pushbuttons and a keyboard (which together initiate a number of diverse actions), and two digital displays (which provide the operator with visual indication of internal DEH system numerical values.)

When pressed, any of the buttons on the Operator's Panel provide momentary action during which a normally-open contact is connected to an electronic diode matrix. Operation of a button energizes a common computer interrupt for the Operator's Panel and applies voltage to a unique combination of 6 contact inputs assigned as a pushbutton decoder. The diode matrix may be used to identify up to 60 pushbuttons. When a button is pressed, the associated interrupt is read within 64.mu. sec, and the corresponding contact inputs scanned and stored in computer memory as a bit pattern for further processing.

Each of the buttons on the panel are backlighted. When a button is pressed and appropriate logical conditions exist, the lamp is turned on to acknowledge to the operator that the action he initiated has been carried out. Should the proper logical conditions not be set, the lamp is not turned on. This informs the operator that the action he requested cannot be carried out.

A few of the buttons are of the digital push-push type which when pushed once initiate an action, and when pushed again suppress that action. Some of these buttons also contain a split lens which indicates one action in the upper half of the lamp and another (usually opposite) action in the lower lens. In addition, certain button backlights are flashed under particular operating circumstances and conditions.

The buttons and keys on the Operator's Panel may be grouped in broad functional groups according to the type of action associated with each set of buttons. A brief description of these groups follows:

1. CONTROL SYSTEM SWITCHING -- These buttons alter the configuration of the DEH Control System by switching in or out certain control functions. Examples are throttle pressure control and impulse pressure control.

2. DISPLAY/CHANGE DEH SYSTEM PARAMETERS -- These buttons allow the operator to visually display and change important parameters which affect the operation of the DEH system. Examples are the speed and load demand, high and low load limits, speed and load rate settings, and control system tuning parameters.

3. OPERATING MODE SELECTION -- This group of buttons provides the operator with the ability to select the turbine operating mode. Examples are permitting an Automatic Synchronizer or an Automatic Dispatch System to set the turbine reference, or selecting local operator automatic control of the turbine (which includes hold/go action).

4. VALVE STATUS/TESTING/LIMITING -- This group of buttons allows valve status information display, throttle/governor valve testing, and valve position limit adjustment.

5. AUTOMATIC TURBINE STARTUP -- This group of buttons is used in conjunction with a special DEH program which continuously monitors important turbine variables, and which also may start up and accelerate the turbine during wide-range speed control.

6. MANUAL OPERATION -- These buttons allow the operator to manually control the position of the turbine valves from the Operator's Panel. The DEH PANEL task has no direct connection with this group of buttons.

7. KEYBOARD ACTIVITY -- These buttons and keys allow numerical data to be input to the DEH system. Such information may include requests for numerical values via the display windows, or may adjust system parameters for optimum performance.

The panel task 1112 responds to the buttons pressed on the operator's panel 1130 by an operator of the DEH control system 1100. The control panel 1130 is shown in FIGS. 11 and 12. Referring now to FIG. 20, the interactions of the panel task 1112 are shown in greater detail. Pushbuttons 1110 are decoded in a diode decoding network 1912 which generates contact inputs to activate the panel interrupt program 1156. The panel interrupt program scans the contact inputs and bids the panel task 1112 whereby the pressed button is decoded and either the panel task 1112 carries out the desired action or the logic task 1110 is bid or the visual display task 1134 is called to carry out the desired command.

6. CONTROL PROGRAM

Automatic control of turbine speed and load requires a complex, interacting feedback control system capable of compensating for dynamic conditions in the power system, the boiler and the turbine-generator. Impulse chamber pressure and shaft speed from the turbine, megawatts from the generator, and throttle pressure from the boiler are used in the controlled operation of the turbine.

In addition to the primary control features discussed above, the DEH system also contains provisions for high and low load limits, valve position limit, and throttle pressure limit; each of these can be adjusted from the Operator's Panel. A number of auxiliary functions are also available which improve the overall turbine performance and the capabilities of the DEH system. Brief descriptions of these follow:

1. Valve position limit adjustment from the Operator's Panel.

2. Valve testing from the Operator's Panel.

3. Speed signal selection from alternate independent sources.

4. Automatic instantaneous, and bumpless operating-mode selection from the Operator's Panel.

5. A continuous valve position monitor and contingency-alert function for the operator during automatic control.

6. A digital simulation and training feature which allows use of the Operator's Panel and most of the DEH system at any time on manual control, without affecting the turbine output or valve position. This powerful aid is used for operator and engineer training, simulation studies, control system tuning or adjustment, and for demonstration purposes.

In order to achieve these objectives, the CONTROL task is provided with analog inputs representing the various important quantities to be controlled, and also is supplied with contact inputs and system logical states.

The control program 1012 and related programs are shown in greater detail in FIG. 22. In the computer program system, the control program 1012 is interconnected with the analog scan program 1116, the auxiliary sync program 1114, the sequence of events interrupt program 1124 and the logic task 1110. FIG. 23 shows a block diagram of the control program 1012. The control program 1012 accepts data from the analog scan program 1116, the sequence of events interrupt program 1124 and is controlled in certain respects by the logic program 1110 and the auxiliary synchronizing program 1114. The control program 1012, upon receiving appropriate inputs, computes the throttle valve TV1-TV4 and the governor valve GV1-GV8 outputs needed to satisfy speed or load demand.

The control program 1012 of the DEH control system 1100 functions, in the preferred embodiment, under three modes of DEH system control. The modes are manual, where the valves GV1-GV8 and the TV1-TV4 are positioned manually through the hardwired control system and the DEH control computer tracks in preparation for an automatic mode of control. The second mode of control is the operator automatic mode, where the valves GV1-DV8 and TV1-TV4 are positioned automatically by the DEH computer in response to a demand signal entered from the keyboard 1130, of FIG. 12. The third mode of control is remote automatic mode, where the valves GV1-GV8 and TV1-TV4 are positioned automatically as in the operator automatic mode but use the automatic turbine startup program 1141 or an automatic synchronizer or an automatic dispatch system for setting the demand value.

SELECT OPERATING MODE FUNCTION

Input demand values of speed, load, rate of change of speed, and rate of change of load are fed to the DEH control system 1100 from various sources and transferred bumplessly from one source to another. Each of these sources has its own independent mode of operation and provides a demand or rate signal to the control program 1020. The control task 1020 responds to the input demand signals and generates outputs which ultimately move the throttle valves TV1 through TV4 and/or the governor valves GV1 through GV8.

with the breaker 17 open and the turbine 10 in speed control, the following modes of operation may be selected:

1. Automatic synchronizer mode -- pulse type contact input for adjusting the turbine speed reference and speed demand and moving the turbine 10 to synchronizing speed and phase.

2. Automatic turbine startup program mode -- provides turbine speed demand and rate.

3. Operator automatic mode -- speed, demand and rate of change of speed entered from the keyboard 1860 on the operator's panel 1130 shown in FIG 12.

4. Maintenance test mode -- speed demand and rate of change of speed are entered by an operator from the keyboard 1860 on the operator's control panel 1130 of FIG. 12 while the DEH system 1100 is being used as a simulator or trainer.

5. Manual tracking mode -- the speed demand and rate of change of speed are internally computed by the DEH system 1100 and set to track the manual analog back-up system 1016 as shown in FIG. 4 in preparation for a bumpless transfer to the operator automatic mode of control.

With the breaker 17 closed and the turbine 10 in the level mode control, the following modes of operation may be selected:

1. Throttle pressure limiting mode -- a contingent mode in which the turbine load reference is run back or decreased at a predetermined rate to a predetermined minimum value as long as a predetermined condition exists.

2. Run-back mode -- a contingency mode in which the load reference is run back or decreased at a predetermined rate as long as a predetermined condition exists.

3. Automatic dispatch system mode -- pulse type contact inputs are supplied from an automatic dispatch system to adjust turbine load reference and demand when the automatic dispatch system button 1870 on the operator's panel 1130 is depressed.

4. Operator automatic mode -- the load demand and the load rate are entered from the keyboard 1830 on the control panel 1130 in FIG. 12.

5. Maintenance test mode -- load demand and load rate are entered from the keyboard 1860 of the control panel 1130 in FIG. 12 while the DEH system 1100 is being used as a simulator or trainer.

6. Manual tracking mode -- the load demand and rate are internally computed by the DEH system 1100 and set to track the manual analog back-up system 1016 preparatory to a bumpless transfer to the operator automatic mode of control.

The select operating mode function responds immediately to turbine demand and rate inputs from the appropriate source as described above. This program determines which operating mode is currently in control by performing various logical and numerical decisions, and then retrieves from selected storage locations the correct values for demand and rate. These are then passed on to the succeeding DEH control programs for further processing and ultimate positioning of the valves. The select operating mode function also accommodates switching between operating modes, accepting new inputs and adapting the DEH system ot the new state in a bumpless transfer of control.

Various contact inputs are required for raise and lower pulses, manual operation, maintenance test, and so forth; these are handled by the SEQUENCE OF EVENTS interrupt program and the PLANTCCI subroutine, which performs a contact input scan. In addition, certain panel pushbuttons affect the operating mode selection; these are handled by the PANEL INTERRUPT program and the PANEL task, which decode and claissify the pushbuttons pressed. The LOGIC task then checks all permissive conditions and current control system status, and computes the appropriate logical states for interpretation by the CONTROL task and the SELECT OPERATING MODE program.

Referring now to FIg. 24, a block diagram is shown illustrating the select operating mode function 2050. Contact inputs from plant wiring 1126 activate the sequence of events interrupt program 1124 which calls the plant contact input subroutine 1150, to scan the plant wiring 1126 for contact inputs. Mode pushbuttons such as automatic turbine startup 1141, automatic dispatch system 1170 and automatic synchronizer 1871 activate the panel interrupt program 1156 which calls the panel program 1112 for classification and which in turn calls upon the logic program 1110 to compute the logic states involved. The logic program 1110 calls the control program 1020 to select the operating mode in that program.

In FIGS. 25A and 25B a flow chart of the select operating mode logic is shown. As one example of mode selection referring to a path 2023, after a statement 7000, provisions are made for a bumpless transfer from an automatic or test mode to an operator mode. The bumpless transfer is accomplished by comparing the computer outputs and the operator mode output signals for the governor valve GV1-GV4 positions. The DEH system 1110 inhibits any transfer until the error between the transferring output and the output transferred is within a predetermined deadband (DBTRKS). Bumpless transfer is accomplished by the DEH control system 1100 by comparing output from one mode of control of the governor valves GV and the throttle valves TV and the same output from another output mode controlling the same parameters. The flow chart of FIGS. 25A and 25B shows mode selection for a complete operating system. In a hardwired or analog control system, the analog parameter output, to be transferred to must continuously track the parameter output to be transferred from. This tracking method is expensive and cumbersome since it has to be done continuously and requires complex hardware. However, in a digital system, such as the DEH control system 1100, the equating of the two parameter outputs need be performed only on transfer. Therefore, great economy of operation is achieved.

SPEED/LOAD REFERENCE FUNCTION

In the DEH turbine controller, the speed/load reference is the central and most important variable in the entire control system. The reference serves as the junction or meeting place between the turbine speed or load demand, selected from any of the various operating modes discussed in the last section, and the Speed or Load Control System, which directs the reference through appropriate control system strategy to the turbine throttle and governor valves to supply the requested demand. FIG. 26 is a diagram which indicates the central importance of the reference in the DEH control system.

The speed/load reference function increments the internal turbine reference at the selected rate to meet the selected demand. This function is most useful when the turbine is on Operator Automatic, on the AUTOMATIC TURBINE STARTUP program, or in the Simulator/Trainer modes. This is because each of these control modes requests unique rates of change of the reference, while the remaining control modes, such as the Automatic Synchronizer and the Automatic Dispatch System, move the reference in pulses or short bursts which are carried out in one step. The Runback and Throttle Pressure contingency modes use some of the features of the reference function, but they bypass much of the subtle reference logic in their hurry to unload the turbine.

For these modes which request movement of the reference at a unique rate, the reference function must provide the controlled motion. Not only must the rate be ramped exactly, but the logic must be such that, at the correct time, the reference must be made exactly equal to the demand, with no overshoot or undershoot. In addition, the reference logic must be sensitive to the GO and HOLD states, and must start or stop movement instantly if requested to do so. Finally, the reference system must turn off the GO and HOLD lamps, if conditions dictate, by passing on to the LOGIC task the proper status information to accomplish this important visual indication feature.

The decision breaker function 1060, of FIG. 5, is identical to the speed/load reference function 1060, of FIG. 26. A software speed control subsystem 2092 of FIG. 26, corresponds to the compare function 1062, the speed reference 1066 and the proportional plus reset controller function 1068, of FIG. 5. The software load control substystem 1094, of FIG. 26, corresponds to the rated speed reference 1074, the turbine speed 1076, the compare function 1078, the proportional controller 1080, the summing function 1972, the compare function 1082, the proportional plus reset controller function 1084, the multiplication function 1086, the compare function 1090, the impulse pressure transducer 1088 and the proportional plus reset controller 1092, of FIG. 5. The speed/load reference 1060 is controlled by, depending upon the mode, and automatic synchronizer 1080, the automatic turbine starter program 1141, and operator automatic mode 1082, a manual tracking mode 2084, a simulator/trainer 2086, an automatic dispatch system 2088, or a run-back contingency load 2090. Each of these modes increments the speed/load reference function 1060 at a selected rate to meet a selected demand.

SPEED CONTROL FUNCTION

The speed control function positions the throttle and governor valves to achieve the existing speed reference with optimum dynamic and steady state response. This is accomplished by using individual proportional-plus-reset controllers for throttle and governor valve speed control, as shown in FIG. 27. The speed error between the turbine speed reference and actual speed drives the appropriate controller, which then reacts by positioning the proper valves to reduce the speed error to zero. The speed controller outputs are low-limit checked against zero and high-limit checked against the quantity HLS, which is a keyboard-entered constant set at 4200 rpm. This prevents the controllers from reaching a reset-windup condition which may inadvertently occur in odd circumstances. The speed controller output is then suitably ranged from 0 to 100 percent and sent downstream as the quantity SPD in the CONTROL task to the THROTTLE and GOVERNOR VALVE programs.

LOAD CONTROL FUNCTION

The load control function positions the governor valves to achieve the existing load reference with optimum dymanic and steady state response. This is accomplished with a feedforward-feedback control system strategy designed to stabilize interactions between the major turbine-generator variables: impulse chamber pressure, megawatts, shaft speed and valve position. FIGS. 28 and 29 show the control system which satisfies these objectives.

The main feedforward path is represented by the turbine load reference value (REFDMD), which is computed by the operating mode selection function described earlier. The feed forward variable (REFDMD) is compensated with two feedback trim factors to account for frequency (speed) participation and megawatt mismatch. The speed compensation is provided by a proportional feedback loop in which the droop regulation gain (GR1) is adjusted to yield rated megawatts correction for a 180 rpm speed error. This speed feedback factor (X) is then summed with the turbine load reference (REFDMD) to produce the speed-corrected load reference (REF1).

A special feature which has been incorporated in the speed feedback loop is a software speed-deadband; this non-linear function filters out high-frequency low-amplitude noise on the speed input signal, thus keeping the load control system from responding to such meaningless information. The width of the speed deadband may be adjusted from the keyboard by setting the appropriate value into the constant SPDB. Another special feature of the speed deadband is the method of implementing this function in comparison with most standard control systems. The common way to incorporate the speed deadband in previous systems is to allow speed errors greater than the width of the deadband to enter the control system completely. This has been found to shock many systems into oscillatory conditions which may have undesirable effects. In the DEH Control System the speed error, when it is larger than the deadband, is smoothly entered into the speed compensation factor by a linear relationship. Thus the shock effect of a sudden speed error is removed completely.

The megawatt feedback loop provides a trim correction signal which is applied to the speed-compensated load reference (REF1) in a product form to yield the speed-and-megawatt corrected load reference (REF2). An additional highly desirable feature of megawatt feedback in the DEH system is that with it the reference and demand display windows on the Operator's Panel are calibrated in actual megawatts when the loop is in service. A proportional-plus-reset controller is used to reduce megawatt error to zero, with the loop providing a feed back factor (Y) which floats around unity (1.0 ) in performing its corrective action. As usual, high and low limits are provided to prevent reset windup and to bound the range of megawatt compensation.

The load reference (REF2), now corrected for speed and megawatt errors, becomes the set point for the impulse pressure cascade feedback loop or the direct demand for valve position, depending on whether the impulse pressure loop is in or out of service. REF2 is multiplied by a ranging gain (GR3) to convert to impulse pressure set point (PISP) in psi. If the loop is in service, then a proportional-plus-reset controller is implemented to drive the impulse pressure error to zero; as always, high and low limits restrict the range of variation of the controller to eliminate the possibility of reset windup. The final governor valve set point (VSP), whether it is generated by the feedback loop or directly from the load reference (REF2), is then converted into a percent valve demand (GVSP) by suitable ranging and is sent downstream in the control task to the THROTTLE and GOVERNOR VALVE programs.

The load control function block diagram shown in FIGS. 28 and 29 is an expansion of the load control, shown in FIG. 5, incorporating the speed loop subroutine and proportional control of function diagram of FIG. 9.

THROTTLE VALVE CONTROL FUNCTION

The throttle valve control function (FIG. 30) computes the correct value of the throttle valve analog output at all times. When the DEH system is on automatic control, this analog output actually positions the throttle valves; when the DEH system is on manual control, this analog output tracks the backup system preparatory to transfer to automatic control.

To accomplish its objective, the throttle valve control function must interrogate various turbine logical and numerical states, and proceed to act on the outcome of these decisions. There are five distinct situations which must be detected by these logical and numerical interrogations. A brief description of these follow; refer to Figure for the method of performing these tests and the major actions taken.

1. The turbine is unlatched and in neither throttle nor governor valve control. During this time the throttle valves are held closed by the throttle valve control function.

2. The turbine is latched and in positive throttle valve control while the DEH system is in wide-range speed control. During this time the throttle valve control function accepts the output of the speed controller (SPD) and positions the throttle valves accordingly.

3. The DEH system is in a transition period, transferring from throttle to governor valves during wide-range speed control. For this interval of time, the throttle valves are still in positive control and the throttle valve control function continues to accept the speed controller output (SPD) and positions the throttle valves accordingly.

4. The DEH system remains in the transition period of transferring from throttle to governor valve control, but now the governor valves are in positive control. During this time the throttle valve control function drives the throttle valves to the wide-open position with a throttle valve bias integrator (TVBIAS), which has a constant input (BTVO) incrementing the integrator. 5. The transition period is over and the transfer from throttle to governor valve control is complete; the turbine is now on either wide-range speed control or on load control after having been synchronized with the power system. During this time the throttle valve control function keeps the throttle valves wide open.

GOVERNOR VALVE CONTROL FUNCTION

The governor valve control function (FIG. 31) computes the correct value for the governor valve analog output at all times. When the DEH system is on automatic control, this analog output actually positions the governor valves; when the DEH system is on manual control, this analog output tracks the backup system preparatory to transfer to automatic control.

To accomplish its objective, the governor valve control function must interrogate various turbine logical states and proceed to act on the outcome of these decisions. There are five distinct situations which must be detected by these logical interrogations. A brief description of these follows; refer to Figure for the method performing these tests and the major action taken.

1. The turbine is unlatched and in neither throttle nor governor control. During this time the governor valves are held closed by the governor valve control function.

2. The turbine is latched and in positive throttle valve control while the DEH system is in wide-range speed control. During this time the governor valve control function drives the governor valves wide open with a governor valve bias integrator (GVBIAS).

3. the DEH system is in a transition period, transferring from throttle valve to governor valve control during wide-range speed operation. For this interval of time, the governor valve control function drives the governor valves to the closed position with the governor valve bias integrator (GVBIAS). The governor valve control function then waits for a decrease in turbine speed and for the Analog Backup System to track the computer outputs.

4. The DEH system remains in the transition period but now the governor valves are in positive control during widerange speed operation. During this time the governor valve control function accepts the output of the speed controller (SPD) and positions the governor valves accordingly.

5. The main generator circuit breaker is closed and the DEH system is in load control. During this time the governor valve control function accepts the output of the load control system GVSP) and positions the governor valves accordingly.

TURBINE OPERATION SIMULATION

In order to allow operators to become proficient in the operation of the DEH system 1100 without risking damage to a multimillion dollar turbine-generator system 10 a simulation subroutine 2110, in FIG. 27, is provided during speed control. A similar subroutine 2111 (FIG. 28) is provided for simulation of the turbine-generator system dynamics during load control.

LOGIC TASK

The LOGIC task is assigned priority level 9 and is bid by the AUX SYNC program on demand by other tasks in the DEH system.

Its size is 1092 words, its data pool size is 147 words, and its header is 9 words for a required storage of 1248 locations. LOGIC is linked as a separate task and loaded into the computer through the tape reader. The core area assigned to LOGIC is (1970 to 1E5F).sub.16 ; this is 4FO.sub.16 (1264.sub.10) locations, which allows a few spares. The LOGIC task is organized as a series of small subprograms which are executed sequentially and which address themselves to particular aspects of the total DEH Control System logical operation. The subprograms are in some cases quite simple, as when monitor lights are turned on or off, and in other cases they are quite complex, as when it is necessary to account for many permissive conditions to allow feedback loops to be put into service.

MAINTENANCE TEST

The MAINTENANCE TEST system is activated by a two-position key-lock switch on the Operator's Panel. The function of this switch is to allow tuning or adjusting of certain constants in the DEH Control System, or to allow operation of the DEH system in a simulation mode for training purposes. When such tests are to be performed, the maintenance test key is moved to the right position; this immediately switches the turbine to manual control by a wired connection and sets a contact input to the DEH system. The LOGIC task then reacts in three ways: first, a contact output is set which turns on a monitor lamp above and to the right of the maintenance test switch; second, another contact output is set which requests transfer to manual as a backup to the wired connection; and third, the manual-tracking portion of the DEH Control System is disabled.

When the maintenance test action is completed and the test switch returned to the off position, the LOGIC task resets the two contact outputs to turn off the maintenance test lamp and to release the request for manual control. In addition, this part of the program enables the manual-tracking system be resetting the turbine REFERENCE and DEMAND to zero and allowing the normal control programs to run.

OPERATION AUTOMATIC LOGIC

the state of manual or automatic operation of the DEH system is actually determined by circuitry in the analog backup system, and the DEH programs simply respond to these states. When the DEH system is in manual control, the analog backup system ignores the computer output signals and positions the valves according to its up/down counter circuitry. Conversely, when the DEH system is in automatic control, the analog backup system uses the computer outputs to position the valves and adjusts its up/down counter to track the computer outputs.

When transfer is made to manual, either by pushbutton or computer request, the analog backup system opens contacts carrying the computer outputs to the valves and simultaneously closes contacts carrying backup system outputs to the valves. In addition, a contact input is sent to the DEH system LOGIC task indicating manual operation. When transfer is made to automatic control by pressing the OPERATOR AUTOMATIC pushbutton, and assuming that the computer system is tracked and ready for automatic, the analog backup system opens contacts carrying its own signals to the valves and simultaneously closes contacts carrying the computer outputs to the valves. The operator automatic logic thus merely updates internal computer variables to the state of manual or automatic control as determined by the backup system.

In updating the DEH system programs to the existing control state, the internal operator automatic variable (OA) is set to the logical inverse of the manual contact input represented by TM. Then a decision is made to determine if the system has just been switched to automatic by comparing OA and its last value (OAX). If automatic has just occurred, ready tracking flags are reset; if not, no action is taken. In either case, the last value (OAX) is set to the current automatic state (OA) for use in the next bid of the LOGIC task.

GO LOGIC

When the DEH system is on operator automatic control, the turbine speed/load (DEMAND) is entered from the keyboard. The operator then may allow the turbine reference to adjust to the demand by pressing the GO pushbutton. When the operator does this, the GO lamp is turned on and logical states are set to begin moving the reference in the CONTROL task. When the reference equals the demand, the GO lamp is turned off. The GO logic detects the various conditions affecting the GO state and sets the status and lamp accordingly.

The GO pushbutton (GOPB), which is updated by the PANEL task, is the set signal for the GO flip-flop. The reset or clear signal, which will override the set signal, can occur from a number of different conditions as follows: the HOLD pushbutton (HOLDPB) as updated by the PANEL task, a computed hold condition (HOLDCP) as set by the CONTROL or LOGIC tasks, the DEH system not being in operator automatic control (OA) or in the maintenance test condition (OPRT) (during which the system may be used as a simulator/trainer), or the condition in which the reference has reached the demand and the CONTROL task sets the GOHOLDOF state to clear the GO lamp.

HOLD LOGIC

When the DEH system is an operator automatic control, the turbine speed/load (DEMAND) is entered from the keyboard. The operator may then inhibit the turbine reference from adjusting to the demand by pressing the HOLD pushbutton. When the operator does this, the HOLD lamp is turned on and logical states are set to prohibit the reference from moving in the CONTROL task. The HOLD logic detects the various conditions affecting the HOLD state and sets the status and lamp accordingly.

The HOLD pushbutton state (HOLDPB), which is set by the PANEL task, or the hold state (HOLDCP) computed by the CONTROL or LOGIC tasks, acts as the set signal for the HOLD flip-flop. The reset or clear signal, which will override the set signal, can occur from a number of different conditions as follows: the DEH system not being on operator automatic control (OA) or in the maintenance test condition (OPRT) (during which the system may be used as a simulator/trainer), the GO flip-flop being set and thus overriding the HOLD state, or the condition in which the reference has reached the demand and the CONTROL task sets the GOHOLDOF state to clear the HOLD lamp. The HOLD logic program then resets the computed hold state (HOLDCP) and the GOHOLDOF state, so that they may be used in future decisions by the CONTROL and LOGIC tasks.

GOVERNOR CONTROL LOGIC

Control of turbine steam flow with the governor valves is required during speed and load control. Normally governor control is initiated when the turbine has been accelerated to near synchronous speed, after which the unit is brought up to synchronous speed, synchronized and then loaded with the governor valves as the normal mode of operation.

The governor control logic detects turbine latch and unlatching conditions, transfer from throttle valve to governor valve control, and manual operation of the governor valves. When any of these conditions occur, the governor logic must align the DEH system to the appropriate governor control state.

The governor control flip-flop (GC) may be set by a number of conditions, the most common of which occurs on automatic control when the operator presses the transfer TV/GV pushbutton (TRPB). Assuming that the governor valves are at their maximum open position as indicated by GVMAX and that the automatic turbine startup mode (ATS) is not selected, then the govenor flip-flop will be set. An alternate path for setting this flip-flop occurs if the automatic turbine startup program (ATS) requests transfer via the logical variable ATSTRPB. In addition, when the throttle valves reach about 90 percent position, a contact input (THI) is activated by the analog backup system, and this contact sets the GC flip-flop. This last case occurs when the turbine is a manual control. Finally, the governor control flip-flop is reset when the turbine latch contact input (ASL) is released.

Following the GC flip-flop, a decision is made to determine if the system has just switched to governor control by comparing GC with its last state (GCX). If transfer has just occurred, the turbine speed (WS) at this instant is saved as WSTRANS, the speed at throttle/governor valve transfer. This value is used in the CONTROL task for a special valve position control logic decision. The last operation in the governor control program is to call the LCCO subroutine to update the GC lamp.

THROTTLE VALVE CONTROL LOGIC

Control of turbine steam flow with the throttle valves is required when the turbine is initially rolled and during speed control up to the point of transfer to governor valve control. After this the throttle valves are kept wide open during normal operation. The throttle control logic detects turbine latch and unlatching conditions, transfer from throttle to governor valve control, and manual operation of the throttle valves. When any of these conditions occur the throttle logic must then align the DEH system to the appropriate throttle control state.

The throttle control state (TC) is simply the logical inverse of the governor control state (GC) when the turbine is latched. However, the throttle control lamp flip-flop (TCLITE) may be set by either TC or by manual operation (TM) while the throttle valves are below 90 percent open as indicated by the contact input (THI) not being set. The TCLITE flip-flop is reset by the contact input (THI) indicating throttle valves wide open or by the turbine latch contact input (ASL) not set.

The throttle control logic also indicates that the transfer from throttle to governor valve state (TRTVGV) is underway when governor control (GC) exists but the throttle valves are not yet wide open. In addition, the transfer complete state (TRCOM) is set when the throttle valves are wide open on governor control as indicated by THI. Finally, the program sets various contact outputs to pass this information on to the plant and operating personnel by calling the LCCO subroutine.

MEGAWATT FEEDBACK LOGIC

To place the loop in service bumplessly, it is necessary to maintain constant governor valve position while inserting the megawatt proportional-plus-reset controller in the control system computations. This means that the integrator in this controller must be instantly set to the proper value, the reference must be reset to that value which will yield no change in governor valve position, and proper account must be taken of the speed feedback effect at the instant of putting the loop in service. A derivation of the equations necessary to guarantee these conditions follows.

REF2 is effectively the governor valve set point which must remain fixed in placing the loop in service, REFDMD is the turbine reference, X is the speed feedback effect and REF1 is the speed modified reference. When the loop is placed in service, the proper values of Y, the megawatt feedback factor, and RESMW, the megawatt integrator, must be computed, and REFDMD then readjusted to produce exactly the same value for REF2 to yield bumpless transfer. The necessary and sufficient condition for bumpless transfer then is that REF2 before and after the switching must be identical, as shown in EQUATION (1).

REF2.sub.IN = REF2.sub.OUT (1)

the value of REF2 before the switch is retained in computer memory, whereas the expression for REF2 after the loop is in may be determined result follows.

REF2.sub.IN = Y * REF1.sub.IN (2)

immediately after the switch, the value of REF1 must equal the existing analog input representing megawatts (MW), so that the integrator sees a zero error. Thus, an equation for this condition is:

REF1.sub. IN = MW (3)

substituting Equations (1) and (3) into (2) and solving for the required value of the megawatt factor (Y) and therefore the megawatt integrator output (RESMW) yields the following result: ##EQU3##

Finally, to guarantee that the transfer will be bumpless the new value of REFDMD must be computed as follows.

REF1.sub.IN = REFDMD.sub.IN + X (5)

substituting Equation (3) into (5) and solving for REFDMD completes the required derivation.

REFDMD.sub.IN = MW - X (6)

the steps in the computation may be summarized: compute the new value of Y and RESMW from Equation (4), compute the new value of REFDMD from Equation (6), set the megawatt integrator last input (RESMWX) to zero, and place the loop in service.

To remove the megawatt loop from service bumplessly, a similar set of computations must be followed. The necessary and sufficient condition for bumpless transfer is to retain a constant value for REF2 as follows.

REF2.sub.OUT = REF2.sub.IN

The value of REF2 before the switch is retained in computer memory, whereas the expression for REF2 after the switch may be determined as given below.

REF2.sub.OUT = REF1.sub.OUT

Immediately after the switch, the value of REF1 must equal the value of REF2 before the switch, since the megawatt loop is now out of service.

REF1.sub.OUT =REF2.sub.IN (7)

finally, to guarantee the bumpless transfer, the new value of the reference REFDMD must be computed to satisfy Equation (7).

REF1.sub.OUT =REFDMD.sub.OUT + X (8)

substituting Equation (7) into (8) and solving for REFDMD yields the final result.

REFDMD.sub.OUT = REF2.sub.IN - X (9)

thus to take the megawatt loop out of service, the reference is reset to the value given in Equation (9) and the monitor lamp indication is reset.

The megawatt pushbutton, represented by MWIPB and updated by the PANEL program, sets the megawatt flip-flop (MWI), while this flip-flop may be reset by a number of conditions as follows: the main breaker (BR) open; a megawatt transducer failure (MWTF), which is a contact input set by the analog backup system; a valve position limit condition as indicated by VPLIM; an analog input failure (AIFAILMW) of the megawatt feedback signal as set by the ANALOG SCAN program; or the analog-to-digital converter out of service (VIDAROS). After evaluation of the megawatt flip-flop, decisions are made to determine if the megawatt loop has just been put into service or just taken out of service, assuming that the main breaker (BR) is closed. If the loop has just been put in, as indicated by the leading edge of the MWI pulse, then the bumpless transfer computations listed in Equations (4) and (6) are executed. If the loop has just come out of service, as indicated by the trailing edge of the MWI pulse, then the bumpless transfer computation listed in Equation (9) is executed. In both cases a call to the LCCO subroutine is made to place the megawatt lamp and two status contact outputs for the megawatt loop in the proper state.

IMPULSE PRESSURE FEEDBACK LOGIC

To place the impulse pressure loop in service bumplessly, it is necessary to maintain the governor valves constant while inserting the impulse pressure proportional-plus-reset controller in the control system computations. This means that the integrator in the controller must be instantly positioned at the proper value. Depending on whether the megawatt feedback loop is in service at this time, one of the following two sets of derivations will be appropriate.

GR3 is a ranging constant which converts the megawatt reference value (REF2) to an impulse pressure set point (PISP) while IPI is the impulse pressure flip-flop. The analog input (PI) is the actual impulse pressure at the instant of placing the loop in service, RESPI is the impulse pressure integrator, and VSP is the governor valve set point. When the loop is put in service, both the integrator values (RESMW and RESPI) must be instantly recomputed to hold the governor valve set point (VSP) constant. Thus to remain bumpless, the following expression must hold.

VSP.sub.IN = VSP.sub.OUT

The value of VSP before the switch is retained in computer memory, whereas after the loop is in service, the value of VSP will be given by the integrator (RESPI). Therefore this integrator output must be instantly set to the value of VSP.

RESPI = VSP.sub.OUT (10)

the additional requirement is that the impulse pressure set point (PISP) be identical to the existing impulse pressure analog input at the instant of switching so that the integrator sees a zero error. This is satisfied as follows.

PISP.sub.IN = PI (11)

the computed value for PISP now may be written to determine what changes must be made to the megawatt integrator.

PISP = GR3 * REF2.sub.IN (12)

the value of REF 2 in turn may be determined in terms of REF1, which does not change when the impulse pressure is switched in since REF1 is upstream of the megawatt loop.

REF2.sub.IN = Y * REF1 (13)

substituting Equations (11) and (12) into (13), and remembering that the megawatt correction factor (Y) and the megawatt integrator output (RESMW) are equal, the new value which must be given to RESMW may be solved for as follows: ##EQU4## The steps in the computation to place impulse pressure feedback into service when the megawatt loop is already in service may be summarized: compute the new value of the impulse integrator from Equation (10), set the last value of the impulse integrator input (RESPIX) to zero, compute the new value of the megawatt integrator from Equation (14), and place the loop in service.

To remove the impulse pressure feedback from service bumplessly, a similar set of computations must be followed. The necessary and sufficient condition is to hold the value of VSP constant as follows:

VSP.sub.OUT = VSP.sub.IN (15)

the value of VSP before the switch will be retained in computer memory, whereas the value of VSP after the switch can be determined when the loop is out.

VSP.sub.OUT = PISP (16)

the set point (PISP) can in turn be computed as follows:

PISP = GR3 * REF2 (17)

finally, REF2 may be determined from REF1 which does not change since it is upstream of the megawatt integrator.

REF2 = Y * REF1 (18)

substituting Equations (15), (16) and (17) into (18), and remembering that the megawatt correction factor (Y) and the megawatt integrator (RESMW) are equal, the new value which must be given to RESMW may be solved for as follows: ##EQU5## The steps in the computation to remove the impulse pressure feedback from service when the megawatt loop is in service are to compute the new value of the megawatt integrator from Equation (19) and then place the loop out of service.

The above set of computations hold for switching the impulse pressure loop while the megawatt loop is in service. The situation is significantly different when the megawatt loop is out of service, since then the reference must be reset to maintain a bumpless transfer. To put the impulse pressure loop in service bumplessly, it is necessary, as always, to keep the governor valve set point constant.

VSP.sub.IN = VSP.sub.OUT

Again, the value of VSP before the switch will be in computer memory. The remaining equations describing the system after the switch may be derived with results as follows:

Respi = vsp.sub.out

pisp = pi

pisp = gr3 * ref2

ref2 = ref1

ref1 = refdmd + x (20)

solving this set of equations for the new value of REFDMD yields the required condition. ##EQU6## Thus, to summarize, when placing impulse pressure feedback in service with the megawatt loop out of service, it is necessary to set the impulse integrator (RESPI) to the value given in Equation (20), reset the last input to this integrator (RESPIX) to zero, compute the new reference REFDMD from Equation (21), and place the loop in service.

The last case to cover is that of removing the impulse pressure loop when megawatt feedback is out of service. Once more the governor valves must remain constant to assure bumpless transfer, as indicated below.

VSP.sub.OUT = VSP.sub.IN

As always, the value of VSP prior to the switch will be in computer memory. The set of equations describing the computations may be written as follows:

VSP.sub.OUT = PSIP

PISP = GR3 * REF2

REF2 = REF1

REF1 = REFDMD + X

Solving this set of equations for the new value of REFDMD yields the required condition. ##EQU7## Thus, REFDMD is computed according to Equation (22), the impulse pressure loop is removed, and the transfer proceeds bumplessly.

The impulse pressure pushbutton, represented by IPIPD and update by the PANEL program, sets the impulse pressure flip-flop (IPI), while a number of conditions may reset the flip-flop as follows: the main breaker (BR) open; a valve position limiting condition as indicated by VPLIM; an analog input failure (AIFAILPI) for the impulse pressure feedback signal as set by the ANALOG SCAN task; the analog-to-digital converter out of service (VIDAROS); or a contact input (SIO) to set impulse pressure out of service when in the automatic dispatch system (ADS) mode. After evaluation of the impulse pressure flip-flop (IPI), decisions are made to determine if the loop has just been put into service or just taken out of service assuming that the main breaker (BR) is closed. If the loop has just come in, as indicated by "the leading edge of the IPI pulse," then the bumpless transfer computations discussed and derived above are evaluated. If the loop has just come out, as indicated by "the trailing edge of the IPI pulse," then again appropriate bumpless transfer conditions are evaluated as discussed above. An additional decision is made on MWI as to whether or not the megawatt feedback loop is in service. As derived above, the form of the bumpless transfer computations depends on the state of the megawatt loop. After all expressions are evaluated, calls are made to the LCCO subroutine to place the impulse pressure lamp and two status contact outputs in the proper state.

SPEED FEEDBACK LOGIC

The speed feedback loop is critically important when the turbine is on automatic speed control, and is of somewhat less importance on load control. Without speed feedback on automatic speed control, the DEH system must reject to manual operation, while on automatic load control the DEH system merely removes the speed feedback loop from service. The operator may place the speed loop back in service after it has been rejected by pressing the speed loop pushbutton, providing the speed inputs have in the meantime been corrected and are again valid.

Once the speed feedback loop is in service, the operator cannot take it out of service, since standard turbine control practice requires speed in service at all times if the input signals are valid. Thus when the loop is in service, pressing the pushbutton is ignored. The only mechanism for taking the loop out of service is by automatic action of the DEH system programs when a speed transducer failure occurs. The speed feedback logic program responds to those conditions which will activate or deactivate the speed loop, whether the conditions be an operator pushbutton request or automatic rejection by the transducer failure.

PANEL TASK

The PANEL Task is assigned priority level C.sub.16 (12.sub.10) and is bid by the PANEL INTERRUPT program when a button is pressed.

FIG. 21 shows a block diagram of the major functions performed by the PANEL task. These include executing each of the button group functions discussed above, as well as additional decisions, checks, and bookkeeping necessary to properly perform the action requested by the operator.

BUTTON DECODE

The BUTTON DECODE program examines the button identification (IPB) provided by the PANEL INTERRUPT program, and transfers to the proper location in the PANEL task to carry out the action required by this button. The program also does some bookkeeping checks necessary to keep the panel lamps in the correct state. A total of 54 buttons can be decoded in the current version of the DEH PANEL task.

The identification of the last button (IPBX), which had been pressed and which has associated with it a visual display mode lamp, is stored in a temporary integer location (JJ) for later use in turning off the last lamp. Then the current button identification (IPB) is checked to determine if it represents the ENTER pushbutton; if so, a special logical variable ENTERPB is reset for later use should the ENTER button be pressed two or more consecutive times. This has been found to be a rather common operator error and is flashed as an invalid request. The program then simply executes a FORTRAN computed GO TO statement and transfers to the appropriate portion of the PANEL task.

CONTROL SYSTEM SWITCHING

There are six buttons on the Operator's Panel which may switch control states of the DEH system. A brief description of each follows:

1. TRANSFER TV/GV - This button initiates a transfer from throttle valve to governor valve control during wide-range speed operation. The pushbutton has a split lens. When control is on the throttle valves, the upper half of the lens is backlighted. When the button is pressed, to transfer control, the entire lens is backlighted. At the completion of the transfer, only the bottom half of the lens remains on. Once the DEH system is on governor control, it stays in this mode until the turbine is tripped and relatched. At this time, it is again in throttle valve control.

2. IMPULSE PRESSURE FEEDBACK IN/OUT - This is a pushpush button with split lens. It places the impulse pressure feedback loop in or out of service, with appropriate backlighting of the button lens.

3. MEGAWATT FEEDBACK IN/OUT - This is a push-push button with split lens. It places the megawatt feedback loop in or out of service, with appropriate backlighting of the button lens.

4. SPEED FEEDBACK IN/OUT - This split lens button places the speed feedback loop in service in the DEH system. Normally the speed loop is always in service; however, when the DEH CONTROL task detects a speed channel failure condition in which all speed input signals are unreliable, the speed feedback loop is disabled and the speed channel monitor lamps turned on. When the speed inputs become reliable, the monitor lamps are turned off, thus indicating to the operator that he may place the speed feedback loop back in service. As long as the speed signals are reliable, the operator cannot take the speed loop out of service.

5. THROTTLE PRESSURE CONTROL IN/OUT - This is a push-push button with split lens which places the throttle pressure controller in or out of service, with appropriate backlighting of the lens.

6. CONTROLLER RESET - The button restores the DEH system to an active operating state after the computer has been stopped due to a power failure or hardware/software maintenance.

The logical variable TRPB is set when the TRANSFER TV/GV button is pressed. The impulse pressure, megawatt, and throttle pressure logical states (IPIPB, MWIPB and TRCPB respectively) are set to the logical inverse of their previous state when the corresponding buttons are pressed. This is the mechanism which provides the push-push nature of these buttons. The logical variable SPIPB is set when the speed feedback button is pressed. Finally, each of these buttons initiate a bid for the LOGIC task by setting the RUNLOGIC variable prior to exit from the PANEL task.

The CONTROLLER RESET button is handled somewhat differently. The state CRESETPB is set by the STOP/INITIALIZE task, which does cleanup and initialization after a computer stop condition. Then CRESETPB is checked; if it is not set, the computer has been running, and thus the button pressed is ignored. If CRESETPB is set, this means the computer had been stopped; CRESETPB is reset and the lamp behind the button is turned off. In addition, the PANEL task effectively presses the speed feedback button by setting the logical state SPIPB. This is done so that the DEH system restarts after a power failure or other computer stop condition with the speed feedback loop in service. The LOGIC task is requested to run by setting the RUNLOGIC state. The REFERENCE display button is also effectively pressed so that the display windows always start out in the same mode after a stop condition on the computer.

OPERATING MODE SELECTION

There are five buttons which may be used to select the turbine operating mode. When any of these are pressed, they initiate major operating changes in the DEH Control System, assuming the proper conditions exist for the mode selected. A brief description of these buttons follows:

1. OPERATOR AUTOMATIC (OPER AUTO) - This button places the turbine in automatic control with the operator providing all demand, rate, and set point information from the keyboard. If the turbine had been previously in manual control, the OPER AUTO lamp must be flashing to indicate that the DEH system is ready to accept automatic control; otherwise pressing the OPER AUTO button is ignored. If the turbine had been in one of the remote control modes listed below, then pressing the OPER AUTO button rejects the remote and returns automatic control to the operator.

2. AUXILIARY SYNCHRONIZER (AUTO SYNC) - This button allows automatic synchronizing equipment to synchronize the turbine generator with the power system by indexing the speed demand and reference with raise/lower pulses, in the form of contact inputs.

3. AUTOMATIC DISPATCHING SYSTEM (ADS) - This button allows automatic dispatching equipment to operate the turbine generator by setting the load demand and reference. A number of dispatching options are available, including raise/lower pulses, raise/lower pulse-width modulation, and analog input values to set the reference.

4. AUTOMATIC TURBINE STARTUP (TURBINE AUTO START) - This button allows a special computer program to automatically start up and accelerate the turbine during wide-range speed control. The program may reside in the DEH computer on it may exist in another computer in the plant or at a remote location.

5. COMPUTER DATA LINK (COMP DATA LINK) - This optional button allows another computer, either in the plant or at a remote location, to provide all demand, rate, and set point information to the DEH system.

The OPER AUTO button resets the remove mode button states (ASPB, ADSPB and AUTOSTAR) for Automatic Synchronizer, the Automatic Dispatch System, and the AUTOMATIC TURBINE STARTUP program, respectively. Since the operator automatic state (OA) is merely the logical inverse of the turbine manual state (TM), the PANEL task cannot actually set OA, but can only request the LOGIC task to run, by setting the RUNLOGIC variable. The LOGIC program then determines whether or not operator automatic is accepted by the manual backup system.

The remote buttons set their corresponding pushbutton states after which RUNLOGIC is set. As in the case of operator automatic, the LOGIC task then determines if the requested mode will be accepted.

The data link button is handled somewhat differently; this is a push-push button whose state (DLINK) is given the logical inverse of its previous value at statement 14. The new state is then interrogated in order to determine whether to turn the button backlight on or off, after which the program exists.

AUTOMATIC TURBINE STARTUP

Five buttons are associated with the automatic turbine startup feature of the DEH system. A brief description of these buttons follows:

1. AUTOMATIC TURBINE STARTUP (TURBINE AUTO START) - This button allows a special computer program to automatically start up and accelerate the turbine during wide-range speed control.

2. TURBINE SUPERVISION OFF - This is a push-push button which controls the printout of messages from the turbine supervisory programs. Normally, the messages are always printed; the operator may suppress printing by pressing this button, which then backlights. Should the messages be desired later, then the button may be pressed again; the lamp is turned off and the supervisory messages are printed on the typewriter.

3. OVERRIDE ALARM - This button overrides certain alarm stops which the AUTOMATIC TURBINE STARTUP program may detect. When this happens, the program waits for operator action before proceeding with the acceleration. If the operator decides to continue the startup, he presses the OVERRIDE ALARM button.

4. OVERRIDE SENSOR HOLD - This button overrides certain analog input sensor stops, which the AUTOMATIC TURBINE STARTUP program may detect. When this happens, the program waits for operator action before proceeding with the acceleration. If the operator decides to continue the startup, he presses this button.

5. RETURN SENSOR TO SCAN - This button returns certain analog inputs to scan after their sensor has been repaired. Should a sensor fail, the AUTOMATIC TURBINE STARTUP removes the corresponding input from scan; when the sensor is detected valid again, this button is backlighted to notify the operator. He then presses the button to return the input to its normal scan.

MANUAL BUTTONS

Six buttons on the Operator's Panel are associated with manual operation of the turbine. Even though the DEH PANEL program does not interface directly with these buttons, a brief description of their function is given for completeness. In general, these buttons allow the operator to control the position of the turbine throttle the governor valves directly from the panel.

1. TURBINE MANUAL - This button places the turbine under manual control of the operator, with the transition from automatic being achieved essentially bumplessly.

2. TV LOWER - This button lowers, or decreases, the throttle valves at a fixed rate as long as the button is held down.

3. TV RAISE - This button raises, or increases, the throttle valves at a fixed rate as long as the button is held down.

4. GV LOWER - This button lowers, or decreases, the governor valves at a fixed rate as long as the button is held down.

5. GV RAISE - This button raises, or increases, the governor valves at a fixed rate as long as the button is held down.

6. FAST ACTION - This button opens or closes the throttle and governor valves, at a fast rate, in manual control. The FAST ACTION must be held down at the same time as any of the TV or GV RAISE/LOWER buttons described above to achieve the fast action effect.

CONTROL TASK

Select Operating Mode Function

The SELECT OPERATING MODE program must distinguish between speed and load control by examining the state of the main generator circuit breaker. For wide-range speed control, the program flow chart is shown in FIG. 25A. The automatic synchronizer state (AS) is first interrogated; if it is the operating mode, the auto sync increase and decrease states (ASINC and ASDEC) are examined. These states are flip-flops which are controlled by the LOGIC task when the auto sync raise or lower contact inputs are set. The program carefully checks to see if both the increase and decrease states are set; if so, no action is taken. Otherwise a temporary location (TEMP) is set to +1 rpm or -1 rpm for each pass through the program during which the appropriate contact input is set. The turbine speed reference and demand are then incremented properly, the ASINC and ASDEC states are reset for the next time, and the program passes to the next stage of the CONTROL task.

If the automatic synchronizer is not the operating mode, then the Automatic Turbine Startup (ATS) state is interrogated at statement 4000 (FIG. 23A). If it is the operating mode, as determined by the LOGIC task, the turbine speed demand and rate are selected from this program via computer locations TASDMD and TASRATE. The rate is then checked against an absolute high limit (OARATMAX), which is a keyboard entered constant usually set at 800 rpm after which the program passes on to the next stage of the CONTROL task.

If the AUTOMATIC TURBINE STARTUP program is not the operating mode, the Operator Automatic (OA) state, and the Maintenance Test (OPRT) state are interrogated at statement 6000 (FIG. 25A). If either of these states are set, the turbine speed demand and rate are selected from the keyboard and the program proceeds to the next stage of the CONTROL task. Note that an Operator Automatic the keyboard values control the turbine, while in Maintenance Test the keyboard values simulate a turbine.

If neither Operator Automatic nor Maintenance Test is the operating mode, then the turbine is in Manual control and the SELECT OPERATING MODE program goes into the manual tracking mode at statement 7000. If the contact input (THI) is set, this means the throttle valves are wide open and the turbine is in speed governor control. Then the error between manual and computer governor valve outputs (IGVMAN and IGVAO) is multiplied by a gain factor (GR10) and saved in a temporary location. If the contact input (THI) is not set, then the turbine is in speed throttle control and the error between manual and computer throttle valve outputs (ITVMAN and ITVAO) is multiplied by a gain factor (GR5) and saved in a temporary location.

In either case, assuming the speed loop (SPI) is in service, the valve output error is checked against a speed tracking deadband (DBTRKS, which is a keyboard entered constant usually set at 1 percent) and the reference is checked against actual speed (WS) through a reference tracking deadband (DBTRKREF, which is also a keyboard entered constant usually set at 50 rpm). If both conditions are met, the READY state ia set to indicate the DEH system is ready to assume automatic control. The READY state is detected by the FLASH task, which then flashes the OPER AUTO light to let the operator know that he may transfer to automatic control.

Finally, the gained valve position error in the temporary location (TEMP) is uused to increment the reference (REFDMD), which is then checked against an absolute high speed limit (HLS). This is a keyboard entered constant which is normally set at 4200 rpm. The program than transfers to statement 15500 for some final bookkeeping checks.

When the SELECT OPERATING MODE program determines that the main generator circuit breaker is closed, thus indicating the turbine is on load control, transfer is made to statement 10000 which is shown in FIG. 25B. The Throttle Pressure Control (TPC) state is interrogated; if it is in service, then the actual throttle pressure (PO) is compared against a set point (POSP), which is a keyboard entered constant usually set at about 1600 psia. If the throttle pressure (PO) is above the set point (POSP), no further action is taken. But if PO is below POSP, then the governor valve position (GVSP) as called for by the computer is checked against a minimum governor valve set point (GVSPMIN). This is a keyboard entered constant usually set at about 25 percent. if GVSP is less than GVSPMIN, no further action is taken; but if GVSP is greater than GVSPMIN, then the throttle pressure limiting state (TPLIM) is set and the reference load rate is set to runback the reference at the rate TPCRATE, which is a keyboard entered constant usually set at 200 percent per minute. The program then transfers to statement 11500 for further bookkeeping computation.

If no throttle pressure contingency exists, the RUNBACK contact input (RB) is interrogated; if it is set, the load reference is runback at the rate (RBRATE, which is a keyboard entered constant set at about 100 percent per minute. Then at statement 11500 some bookkeeping details are taken care of. Thus if the Automatic Dispatch System (ADS) state has been in control when either a throttle pressure limit or runback condition occurred, this mode is rejected by resetting the automatic dispatch system pushbutton state (ADSPB) and setting the RUNLOGIC flag. Within 1/10 sec the AUX SYNC task bids the LOGIC task, which then realigns all states to the correct position. A second bookkeeping check is made at statement 11700 where the HOLD state is checked. If HOLD is reset, then it is set so that the operator has an indication of why the reference has been runback.

If no runback contingency exists, then the Automatic Dispatch System (ADS) state is interrogated at statement 1200. If it is the operating mode, the ADS increase and decrease states (ADSINC and ADSDEC) are examined. These are flip-flops which are controlled by the LOGIC task when the ADS increase and decrease contact inputs are set. The program carefully checks to see if both the increase and decrease contacts are set; if so no action is taken. Otherwise a temporary location (TEMP) is set to the ADS raise or lower pulse count (IADSUP or IADSDOWN). The AUX SYNC task keeps track of these pulse counts according to the conditions set up by the LOGIC task. However, a maximum ADS pulse-width is imposed on both the raise and lower pulses in the SELECT OPERATING MODE program by comparing their counts (IADSUP and IADSDOWN) with a limit (ADSMAXT), which is a keyboard entered constant usually set to 10 counts of 1/10 sec each (thus yielding a maximum pulse-width of 1 sec). After the pulse-width limiting action, at statement 12400 the turbine load reference and demand are incremented by an amount proportional to the pulse-width; the proportionality factor (ADSRATE) is a keyboard entered constant usually set somewhere between 1 and 10 MW per sec of pulse-width. Finally, at statement 12600, various ADS counters and states are reset prior to moving on to the next stage of the CONTROL task.

If the ADS state is not set, then the select operating mode program checks the Operator Automatic (OA) state and the Maintenance Test (OPRT) state at statement 14000. If either of these states are set, then the turbine demand and rate are accepted from the keyboard and the program proceeds to the next stage of the CONTROL task. Note that in Operator Automatic the keyboard values control the turbine, while in Maintenance Test the keyboard values simulate a turbine.

If neither Operator Automatic nor Maintenance Test is the operating mode, then the turbine is in Manual control and the SELECT OPERATING MODE program goes into the Manual Load Tracking mode at statement 1500. The error between the manual and computer governor valve outputs (IGVMAN and IGVAO) is stored in a temporary location (TEMP) and compared against a load tracking deadband (DBTRKL), which is a keyboard entered constant usually set at about 1 percent. If the outputs agree within DBTRKL, then the READY state is set to indicate the DEH system is ready to assume automatic control. The READY state is detected by the FLASH task, which then flashes the OPER AUTO light to let the operator knwn that he may transfer to automatic control.

The valve output error is then gain multiplied by GR9 and added to the current reference (REFDMD), which is high-limit-checked against MWMAX, a keyboard entered constant usually set to about 120 percent of rated megawatts. REFDMD is also low-limit-checked against zero, thus assuring that the tracking scheme will not windup in either direction. Finally, a last check is made to determine if a voltage exists on the test analog output lines; if so, the READY state is reset so that transfer to automatic control is inhibited until this voltage is removed. This may be done by pressing the OPEN valve test pushbutton until the lights behind the OPEN and CLOSE pushbutton go out.

SPEED/LOAD REFERENCE FUNCTION

The GO state is checked; if GO is off, the HOLD state is checked. If HOLD is on and the demand and reference value (REFDMD) are equal, then the logical states (GOHOLDOF and RUNLOGIC) are set. This results in the LOGIC task being bid within 1/10 sec by the AUX SYNC task, which recognizes the RUNLOGIC state. The LOGIC task then turns off the HOLD flip-flop and lamp as requested by the GOHOLDOF state.

If the GO state is set back however, then this is the signal to allow the reference to move toward the demand. The magnitude of the difference between the reference and the demand is computed and stored in a temporary location. Then the magnitude of the incremental step size taken each second by the selected rate, as discussed above, is saved in another temporary location. These two temporary quantities are then compared and if the demand/reference difference in TEMP is greater than the incremental step size in TEMP1, this means the reference must continue to move closer to the demand. However, the governor valve position limiting state (VPLIM) is checked; if it is set and the demand is above the reference, then no movement is allowed in the reference. This is because the valve position limit function is operating and refuses to allow any increase in reference because this will attempt to increase the governor valve position beyond the limit.

If there is no valve position limiting action, then the reference is incremented by the incremental rate step size and the program transfers for final exit.

Eventually the reference will approach within the allotted boundary of the demand. Then the reference program immediately sets the reference equal to the demand. Finally, the state of the breaker (BR) is interrogated; if it is set, the program transfers for the Load Control System computations, while transfer is made for the Speed Control System computations if the breaker state (BR) is reset.

SPEED CONTROL FUNCTION

To provide the simulation and training feature, FIG. 27 shows an additional program path which will internally generate a simulated speed signal (SIMWS) in the Maintenance Test mode of operation. This is accomplished by feeding back the speed controller output (SPDSP) through a first order lag transfer function which approximates the turbine inertia response. This simulated speed then replaces the actual speed in developing a speed error during the Simulation/Training mode of operation.

All speed control system parameters, such as gains, reset times and limits, are keyboard entered constnts which are available for tuning or adjustment during the Maintenance Test mode. These changes require transfer of the turbine control to manual operation.

Logical checks are made to determine whether the speed computations should be evaluated. Thus, if the speed inputs failed and are unreliable, then the speed loop (SPI) is taken out of service, and there is no speed information by which to control the turbine. In addition, if the overspeed speed protection circuit in the Analog Backup System is operating, as indicated by the contact input (OPCOP), this closes the governor valve and thus overrides the DEH Speed Control System; consequently in this case, no speed control computations are performed.

Assuming that neither of these situations exist, the speed error is calculated. If the system is in the Simulation/Training mode, this error is the difference between the reference and simulated speed; the speed error is the difference between the reference and actual speed in all other cases. Following this error computation, a decision is made as to whether the turbine is on governor or throttle control. Appropriate calls are then made to the PRESET subroutine to evaluate the proportional-plus-reset controller action for the throttle or governor valve. This subroutine takes care of evaluating the controller algorithm and the high/low limit checks to eliminate reset windup.

LOAD CONTROL FUNCTION

As in the Speed Control System, all parameters in the Load Control System are keyboard entered constants, which may be tuned or adjusted in the Maintenance Test mode. As always, changes of this type require transfer to manual control for the adjustment, after which the DEH system will track and permit return to automatic control.

To provide the simulation and training feature disclosed previously, FIG. 28 shows additional program paths which internally generate simulated megawatt and impulse pressure signals (SIMMW and SIMPI) in the Maintenance Test mode of operation. These are accomplished by feeding back the load reference (REF2) and the value set point (VSP)(through software) to first order lag transfer functions which approximate the generator and turbine responses. These simulated signals then replace the actual feedbacks in developing megawatt and impulse pressure errors during the Simulation/Training mode of operation.

A check is first made (FIG. 29) to determine if a change has occurred in the throttle pressure limit state (TPLIM); if so the LOGIC ask aligns all status variables accordingly. The LOAD CONTROL program next checks the speed transducer failure state (SPTF). If there is no failure, the speed feedback loop is evaluated with a call to the SPDLOOP subroutine; if there is a speed transducer failure, the speed feedback loop is bypassed and the speed compensation factor (X) is set to zero. Whichever is the case, the factor (X) is summed with the turbine load reference (REFDMD) to form the speed compensated load reference (REF1). A low-limit-check against zero is performed on REF1 to keep it from going negative, which is possible should a turbine overspeed condition result.

The LOAD CONTROL program then checks the maintenance test contact input (OPRT), which is set means the DEH system is being used as a simulator/trainer or control system tuning is underway. In either case, simulated megawatt and impulse pressure signals (SIMMW and SIMPI) are generated; if the turbine is not in this mode, then the simulated signals are set equal to the actual signals.

The state of the megawatt feedback loop (MWI) is checked; if the loop is out of service, the speed/megawatt compensated load reference (REF2) is simply set equal to the speed compensated load reference (REF1). But if the megawatt loop is in service, the megawatt error is computed and ranged to a per unit value by using the ranging gain (GR2), which is normally set at rated turbine generator megawatts. Then the PRESET subroutine is called to evaluate the megawatt proportional-plus-reset controller, including high/low limit checking. The result of this computation is the megawatt trim factor (Y), which is then applied to the speed compensated load reference (REF1) in a product relationship to form and speed/megawatt corrected load reference (REF2).

The speed/megawatt compensated load reference (REF2) is converted to an impulse pressure set point (PISP) by use of ranging gain (GR3). The state of the impulse pressure feedback loop (IPI) is then interrogated; if it is out of service the governor valve set point (VSP) is simply set equal to the impulse pressure set point (PISP) in psi. But if the impulse pressure loop is in service, then the impulse pressure error is computed and used as the driving signal for the proportional-plus-reset controller, which is evaluated by a call to the PRESET subroutine; this also does the high/low limit checking.

Finally, the governor valve set point (VSP) in psi is converted to a governor valve set point from 0 to 100 percent by use of the ranging gain (GR4), which is normally set at rated impulse pressure. The program then transfers to the final stages of the CONTROL task which actually compute the throttle and governor valve outputs.

THROTTLE VALVE CONTROL FUNCTION

The throttle control state (TC) is interrogated (FIG. 30); if it is set, this means the throttle valves are in positive control, and the program computes the throttle valve analog output from the speed controller value (SPD) and the keyboard entered ranging constant (GR6). However, if the throttle control state (TC) is not set, then the governor control state (GC) is checked. If it is not set, this means that the turbine is unlatched and that the throttle valves should be at their minimum position of completely closed. The program then computes the throttle valve analog output of zero.

If the governor control state (GC) is set, it is then necessary to determine if the throttle/governor transfer is complete by checking the TRCOM state. If TRCOM is not set, this means the transfer is still in progress; an additional check is made to determine if the governor valves have closed as indicated by GVMIN. If GVMIN is not set, then the throttle valves are still in positive control and the program computes the throttle valve analog output as required by the speed controller value (SPD) and the ranging gain (GR6).

Eventually the state GVMIN will be set to indicate that the governor valves are now in positive control. Then the throttle valve maximum position state (TVMAX) is questioned. If it is not set, then the throttle valve bias integrator (TVBIAS) is incremented by the bias constant (BTVO) and the throttle valve analog output set accordingly. In a short time the throttle valves are wide open; after this all logical states will be set to indicate this fact. Succeeding passes through the THROTTLE VALVE CONTROL program will then hold the throttle valve analog outputs wide open until the turbine is unlatched and tripped for some reason.

GOVERNOR VALVE CONTROL FUNCTION

The governor valve position, as set by the governor valve control function, is compared to (and high limited by) the valve position limit (VPOSL) at all times. This gives the operator the ability to override the control system at any time that he considers it necessary, and allows him to control the position of the governor valves from VALVE POSITION LIMIT RAISE and LOWER pushbuttons on the Operator's Panel. If the governor valves are limited by the valve position limit (VPOSL), the lamp behind the VALVE POSITION LIMIT DISPLAY pushbutton flashes, thus alerting the operator to the condition.

Various logical numerical checks are necessary to determine which of the five situations the turbine is currently in, on a second-by-second real time basis. Further, the actual governor valve analog output computation is made for each of these five situations, along with the valve position limit checking feature and additional bookkeeping computations necessary for coordination of the various DEH programs.

Considering the flow chart of FIG. 31 at statement 1200, the valve position limit state (VPLIM) is reset at each pass through the governor valve control program. Then the governor control state (GC) is interrogated; if it is not set, the throttle control state (TC) is checked. If throttle control (TC) is not set, this means the turbine is unlatched and the governor valve minimum state (GVMIN) is checked. If GVMIN is not set, then at statement 1270 all governor valve open states are reset and all governor valve close states, including GVMIN, are set. The program then transfers to statement 1320 for analog output computation and valve position limit checking to hold the governor valves closed. Succeeding passes through the program will find the GVMIN state set and transfer directly to statement 1320.

If the turbine is latched, then the throttle control state (TC) is set. The governor valve control function finds itself at statement 1210, where the governor valve maximum state (GVMAX) is interrogated. If it is not set, then the governor valve bias integrator (GVBIAS) is incremented by the governor valve open-bias constant (BGVO), which is keyboard entered constant usually set at 10 percent to open the governor valves incrementally when the turbine is latched. The program then transfers to statement 1240 where the governor control state (GC) is again checked, since this point in the program may be reached from alternate paths. For the present situation, GC will not be set, thus leading to a check on whether the governor valve bias integrator (GVBIAS) has reached 100 percent and therefore have positioned the governor valves wide open. Assuming that GVBIAS has incremented up to 100 percent, all governor valve close states are reset and all governor valve open states are set, including GVMAX. The program then transfers to statement 1320 for analog output computation and valve position limit checking to hold the governor valves wide open. Succeeding passes through the program find the GVMAX state set at statement 1210 and transfer directly to statement 1320.

Each of the cases discussed above apply when the governor control state (GC) is not set. Once the throttle/governor transfer is initiated, however, this sets the governor control state (GC), in which case the GOVERNOR VALVE CONTROL program arrives at statement 1220. The state of the breaker (BR) is checked; if BR is set, this means the DEH system is on load control and the program transfers to statement 1340 for load computation of the governor valve analog outputs and valve position limit checking.

However, if the breaker (BR) is open and the DEH system still in speed control, the check of BR at statement 1220 finds it not set. Then the throttle/governor transfer complete state (TRCOM) is checked; assuming it has not yet been set, the governor valve closed state (GVMIN) is checked. Normally this will not be set at this point in time, thus requiring the governor valve bias integrator (GVBIAS) to be decremented by the governor valve close-bias constant (BGVC), which is a keyboard entered quantity normally set at 100 percent to instantly close the governor valves when the transfer from throttle to governor control is initiated.

The program then passes on to statement 1240 where the governor control state (GC) is checked again; since GC is set for the present discussion, then at statement 1260 the manual contact input (TM) is interrogated. If the turbine is in manual control at this time, the program transfers to statement 1270 for appropriate bookkeeping which will be described shortly. If the turbine is in automatic control, then the test at statement 1260 on the state of TM finds it not set and an additional test is made on whether the governor valve bias integrator (GVBIAS) has reached zero to indicate the governor valves are closed. If it has not, then the program cycles through this area until the GVBIAS value is zero. Normally this will take only a few passes since the closing bias constant (BGVC) will be quite large to achieve a fast, smooth throttle/governor valve transfer.

Once GVBIAS is zero, the GOVERNOR VALVE CONTROL program searches to determine if the turbine speed (WS) has dropped below the speed at transfer WSTRANS by an amount WSDIP, which is a keyboard entered constant usually set at 10 rpm. When this has occurred, and assuming that the analog backup system has followed the computer governor valve analog output as indicated by the manual not tracking state (MONOTRAK) the GOVERNOR VALVE CONTROL program transfers to statement 1270. All governor valve open states are reset and all governor valve close states, including GVMIN, are set and the program passes on to statement 1320 for computation of the governor valve analog output and valve position limit checking to hold the governor valves closed.

The setting of GVMIN at statement 1270 leads to execution of the LOGIC task, which then uses this information to generate the throttle/governor valve transfer complete state (TRCOM). SUcceeding passes through the GOVERNOR VALVE CONTROL program at statement 1220 find TRCOM set and immediately transfer to statement 1380 for computation of the governor valve analog output and valve position limit checking to control turbine speed. The portion of the program at statement 1320 is that necessary to hold the governor valves at the value residing in the governor valve bias integrator (GVBIAS).

The computations necessary to position the governor valves on load control determine where the load control governor valve set point (GVSP) lies with respect to a nonlinear curve which characterizes the governor valve stroke mechanism. The result of this search positions GVSP along the abscissa of the curve, after which the actual valve position (GVPOS) is computed from analytical solution of points along the curve,

The computed governor valve position (GVPOS) is compared with the current valve position limit (VPOSL). If GVPOS is below VPOSL, no action is taken, if GVPOS is greater than VPOSL, then the valve position limiting state VPLIM is set, RUNLOGIC is set and the actual governor valve position GVPOS is reset to the value residing in VPOSL. The LOGIC and FLASH task perform their assigned functions of aligning the DEH system to these conditions and flashing the VALVE POSITION LIMIT DISPLAY lamp, respectively.

In the computation necessary to position the governor valves on speed control, the speed controller percent output (SPD), suitably ratioed to account for differences between the speed ranging gain (GR7) and the maximum ranging factor of 20.47, is checked against the current valve position limit (VPOSL). If the ratioed speed controlled output is below VPOSL, no special action is taken; if VPOSL is violated, then the valve position limiting states (VPLIM and RUNLOGIC) are set to trigger the appropriate responses from the LOGIC and FLASH tasks. In addition the speed controller output (SPD) and the speed integrator (RESSPD) are reset to values consistent with VPOSL.

A FORTRAN DO loop is executed to make final checks on both the throttle and governor valve analog outputs. They are low-limit-checked to guarantee that they do not go below zero and high-limit checked to guarantee that they do not go above the maximum analog output voltage pattern. Then, the analog output handler is called to output the computed throttle and governor valve patterns. Finally, the CONTROL task exits to the Monitor for the next bid 1 sec later.

First Order Lag Function

The first order lag transfer function is a more or less standard component of control systems. It provides an output signal which is a time delayed version of the input signal. The time constant T of the first order lag is a measure of the time delay in seconds produced by the lag. Approximately 5T (i.e. five time constants) after the input makes a step change, the output has essentially reproduced this change.

The uses of the first order lag function vary somewhat. In some cases, it is valuable as a filter to smooth out random noise pulses or spikes in signals. In other cases, the first order lag is useful in simulating known response of various devices or portions of systems. This latter situation is the way in which the first order lag is used in the DEH application. When the MAINTENANCE TEST switch is moved to the TEST position; thus placing the DEH system in the simulation/training mode of operation, appropriate computer variables are sent into first order lag transfer functions. The output of these functions represents simulated analog inputs such as turbine speed, impulse pressure and megawatts.

In order to perform the mathematical function of a first order lag in a computer, it is necessary to use numerical techniques to approximate the function. A number of algorithms are available, each of which have certain advantages and disadvantages. Although the trapezoidal rule yields the most accurate first order lag response, it requires additional storage for past history of the input. For this reason, the rectangular rule is used in the DEH system; it requires less storage and, though it is not as accurate as the trapezoidal rule, such accuracy is not required in the use of the first order lag in a simulator/trainer context.

The algorithm used by the DEH system to evaluate the first order lag is given by: ##EQU8## Definition of terms in Equation (23) follows:

(N) The current instant of real time (N-1) The last instant of real time DT The sampling interval, or the time interval between evaluations of the first order lag algorithm. In the DEH system this is normally 1 sec T The first order lag time delay in sec ZIN(N) The current value of the input ZOUT(N) The current value of the output ZOUT(N-1) The last value of the output

To use the algorithm of Equation (23), the DEH system is organized so that the parameters (DT and T), the input variable (ZIN(N)), and the output variables (ZOUT(N)) and ZOUT(N-1) are in known COMMON areas of storage. The algorithm itself is programmed in the form of a FORTRAN STATEMENT FUNCTION, so that use of the first order lag is restricted to the CONTROL task. To evaluate the lag transfer function, it is necessary only to write the statement function expression in-line at the appropriate place in the CONTROL task.

The first order lag is programmed as a FORTRAN STATEMENT function to minimize the overhead storage requirements that occur if programmed as a subroutine.

FOLAG(ZIN,TDELAY,ZOUT)=(TDELAY*ZOUT+ZIN)/(IDELAY+1) (24)

this statement expresses the algorithm of Equation (23), with some collecting of terms and substitution of 1.0 for the general sampling interval (DT), since the CONTROL task runs every 1 sec. The dummy arguments (ZIN,TDELAY and ZOUT) represent the input, the time delay and the output variables needed to evaluate the first order lag.

Nonlinear Characterization Function

The nonlinear characterization function provides an important feature for accommodating the nonlinear nature of process equipment. This function produces an output related in a nonlinear fashion to the input.

The form of the curve comprising the characterization function varies somewhat with the application and with the mechanism available for incorporating this feature in the control system. In some analog systems, the curve may have two or at most three segments to accomplish its function. In some highly sophisticated computer systems, the curve may have as many as eight or ten segments. The DEH Control System provides a nonlinear characterization function having five straight-line segments composed of six points describing the intersections of these segments. The slope of any segment may be positive, zero or negative, while the points defining the intersections of various segments may have any positive value. For the DEH application requirements, it is only necessary to work with curves in the first quadrant.

The nonlinear characterization function in the DEH system is used to describe the governor valve position-versus-stroke relationship on load control. Accurate representation of this curve allows operation of the DEH system in automatic control (with the megawatt and impulse pressure feedback loops out of service) to be effectively linearized. Megawatt load demand can be achieved quite closely on automatic control without the feedback loops, which may be out of service due to faults with the transducers, or due to other problems. Of course, with the loops in service, operation then is exactly aligned between load demand and actual megawatt load. The axis of ordinates POS and the axis of abscissa SP consist of six points each. These are all keyboard entered quantities which may be tuned or adjusted in the maintenance test mode of operation.

The program isolates the segment of the SP axis within which the input value (GVSP) lies. Having found this, the program then evaluates the output value (GVPOS) using the slope intercept form of a stright-line from analytical geometry considerations. The ratio of the difference between corresponding values of POS and SP yields the slope of that section. This slope is multiplied by the exact position within the I-th section, which is given by the difference between the current value of the input (GVSP) and the left end point SP(I'1)). The resultant product is added to the intercept (POS(I--1)) for this section to yieldl the required governor valve position (GVPOS).

ANALOG BACKUP SYSTEM

Throttle Valve Control

Throttle values are used on wide-range speed control from turning gear to approximately 90 percent of rated speed. From this point to full rated speed, governor valves are used for control.

When the DEH Control System is in the Operator Automatic mode of operation, the control signal from the computer analog output card (TVAAZ1) is permitted to control the throttle valves, through the Servo/Linear Variable Differential Transformer (S/LVDT) Cards. The Analog Backup System tracks the computer output.

To accomplish this tracking, the analog comparator compares the TVAAZ1 signal to the output of digital-to-analog (D/A) converter (TVMAZ1). If TVAAZ1 exceeds TVMAZ1, the comparator generates a raise signal. This signal causes the up/down counter to count up at a preset rate and increase its digital output. The digital-to-analog (D/A) converter output (TVMAZ1) increases until it equals TVAAZ1. Thus the Analog Backup System continuously tracks signal TVAAZ1, when the DEH Control System is in the Operator Automatic mode.

When the DEH Control System is in the Turbine Manual mode of operation, the analog output (TVMAZ2) controls the throttle valves through the S/LVDT Cards; the computer output (TVAAZ2) is blocked. The auto/manual logic circuitry blocks the analog comparator output and allows the TV RAISE and TV LOWER pushbuttons on the Operator B Ppanel to control the up/down counter. Pressing the TV Raise button causes the up/down counter to count up at a slow rate. If the FAST ACTION pushbutton is pressed at the same time however, a faster rate is selected. The up/down counter output is converted to an analog output and used to control the throttle valves (TVMAZ2). With the DEH Control System in the Turbine Manual mode, the digital portion tracks the analog output with a computer software program.

In summary, when the system is in the Operator Automatic mode, the Analog backup System tracks the computer output. When the system goes to the Turbine Manual mode, the analog system output equals the computer output and the transfer is made without moving the throttle valves (bumpless transfer). While the system is in Turbine Manual, the TV RAISE and TV LOWER pushbuttons control the throttle valve position and the digital portion tracks the analog system output. If the system is put back in the Operator Automatic mode, the transfer is made without a bump.

Governor Valve Control

Governor valves are used for speed and load control. If there are separate valve actuators for each valve, the DEH Control System may be in either single valve or sequential valve operation.

There are two types of inputs to the S/LVDT Cards. One type is the sequential valve inputs (GV1AZ1, GV2AZ1); these signals are generated independently of the Analog Backup System. The second type of input (GV*AZ1) is the single valve input; this input is generated either by the computer (GVAAZ2) or by the analog system (GVMAZ2).

When the system is in single valve operation (or when sequential valve operation is not supplied), the squential valve inputs to the S/LVDT Cards are zero. The GV*AZ1 signal controls the governor valves. Except for the fact that the analog output is biased so that positive and negative values can be obtained, the governor valve control circuits are the same as the throttle value control circuits previously discussed.

The Analog Backup System tracks the computer output (GVAAZ1) when the control system is in the Operator Automatic mode. The analog system is controlled by the GV RAISE and GV LOWER Pushbuttons when the control system is in the Turbine Manual Mode and the Computer tracks the analog output. The control signal (GV*AZ1) goes to all S/LVDT Cards; all valves move the same amount at the same time.

When the control system is in sequential valve operation (and in the Operator Automatic mode), the sequential inputs (GV1AZ1, GV2AZ1) are controlled by the computer. The computer alos sets the single valve input (GV*AZ1) to zero. The computer then uses the sequential inputs to individually control the governor valves.

If the control system transfers to the Turbine Manual mode while in sequential valve operation, the computer keeps the sequential valve input signals (GV1AZ1, GV2AZ1) constant. Bumpless transfer occurs since the governor valves do not move. When the transfer is complete, the operator can position the valves with the GV RAISE and GV LOWER pushbuttons. Pressing the GV RAISE pushbutton increases the outputs of the D/A converter (GVMAZ) and thus increases the single valve input signal (GV*AZ1). GV*AZ1 is summed with the sequential input signals (GV1AZ1 and GV2AZ1); this increases the output of the S/LVDT Cards, and opens all the valves by the same amount.

If the GV LOWER pushbutton is pressed, the single valve input signal (GV*AZ1) is decreased. This signal is summed with the sequential input signals, causes a decrease in S/LVDT Card output, and closes all the valves by the same amount. The up/down counter counts below its mid range and causes the D/A converter output (GVMAZ1) to go negative. This feature allows the valves to be closed, even though the sequential valve input remains constant.

The digital system continuously tracks the single valve input (GV*AZ1) with a computer software program. When transfer to Operator Automatic is initiated (by pressing the OPER AUTO pushbutton), transfer occurs without changing the valve position (bumpless transfer).

In summary, for units with individual servos, the governor valves can operate in either the single valve or sequential valve mode. In either case, the Analog Backup System tracks the computer generated single valve output signal when in Operator Automatic mode, and positions the valves when in Turbine Manual mode.

Claims

We claim:

1. A turbine for an electric power generating system comprising:

a turbine for driving a plant generator,

means for controlling the flow of an energizing fluid to said turbine,

means for automatically controlling said flow controlling means to control the turbine speed during and after startup,

means for automatically controlling said flow controlling means to control the turbine load after the turbine reaches synchronous speed,

said automatic controlling means including means for generating electric signals for said flow controlling means as a function of reference and feedback signals,

means for controlling the operation of said flow controlling means in response to the electric signals and in turn the operating state of said turbine,

means for generating at least one simulated response to predetermined outputs generated by said automatic controlling means,

means for connecting said automatic controlling and said generating means to operate in a simulation mode including means for applying the simulated response to said automatic controlling means,

and means for operating said backup control means to control said turbine when said automatic controlling means is placed in the simulation mode.

2. A turbine as set forth in claim 1 wherein the turbine is a steam turbine having inlet steam valves, said flow controlling means includes said valves, and said automatic controlling means provide position control over said valves.

3. A turbine as set forth in claim 2 wherein said simulated response generating means is included as a part of said automatic controlling means.

4. A turbine as set forth in claim 2 wherein said automatic controlling means includes a digital computer, said computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

5. A control system as set forth in claim 4 wherein said automatic controlling means includes a digital computer, said computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

6. A turbine as set forth in claim 2 wherein means are provided for generating a signal representing actual turbine speed, said automatic controlling means includes means for generating a speed demand as a function of a speed reference and the actual turbine speed, and said simulated response generating means includes means for generating a simulated turbine speed response as a function of the speed demand and for applying the simulated turbine speed response to speed demand generating means in place of the actual turbine speed when the simulation mode is selected.

7. A turbine as set forth in claim 6 wherein said simulated turbine speed response generating means includes a first order lag function generator to which the speed demand is applied.

8. A turbine as set forth in claim 6 wherein said automatic controlling means includes a digital computer, and computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

9. A turbine as set forth in claim 2 wherein means are provided for generating a signal representing actual turbine load, said automatic controlling means includes means for generating a load demand as a function of a load reference and the actual turbine load, and said simulated response generating means includes means for generating a simulated turbine load response as a function of the load demand and for applying a simulated turbine load response to load demand generating means in place of the actual turbine load when the simulation mode is selected.

10. A turbine as set forth in claim 9 wherein load demand is impulse pressure demand and the actual load is represented by impulse pressure.

11. A turbine as set forth in claim 9 wherein the load demand is an electrical load demand and the actual load is represented by an electrical load signal.

12. A turbine as set forth in claim 9 wherein said load demand generating means includes means for generating an electrical load demand as a function of an electrical load reference and actual electrical load and means for generating an impulse pressurue demand as a function of the electrical load demand and actual impulse pressure, said simulated response generating means includes an impulse pressure response generator and an electrical load response generator, and said electrical load and impulse pressure generators responding respectively to the electrcial load demand and the impulse pressure demand to generate respective simulated generator electrical load and turbine impulse pressure simulation responses for respective application to said electrical load and impulse pressure generators.

13. A turbine as set forth in claim 12 wherein said automatic controlling means includes a digital computer, and said backup control means is an analog control external to the computer.

14. A turbine as set forth in claim 9 wherein said simulated turbine speed response generating means includes a first order lag function generator to which the speed demand is applied.

15. A turbine as set forth in claim 9 wherein means are provided for generating a signal representing actual turbine speed, said automatic controlling means includes means for generating a speed demand as a function of a speed reference and the actual turbine speed, and said simulated response generating means includes means for generating a simulated turbine speed response as a function of the speed demand and for applying the simulated turbine speed response to speed demand generating means in place of the actual turbine speed when the simulation mode is selected.

16. A turbine as set forth in claim 15 wherein said automatic controlling means includes a digital computer, and said backup control means is an analog control external to the computer.

17. A turbine as set forth in claim 9 wherein said automatic controling means includes a digital computer, and said backup control means is an analog control external to the computer.

18. A turbine as set forth in claim 1 wherein an operator panel is provided with means for generating a simulation mode selection signal, means are provided for coupling said selection means to said automatic controlling means and said simulation response generating means.

19. A turbine as set forth in claim 18 wherein the turbine is a steam turbine having inlet steam valves, said flow controlling means includes said valves, and said automatic controlling means provide position control over said valves.

20. A turbine as set forth in claim 18 wherein said automatic controlling means includes a digital computer, said computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

21. A control system for a steam turbine having inlet steam valves, said control system comprising:

means for controlling the flow of an energizing fluid to said turbine,

means for automatically controlling said flow controlling means to control the turbine speed during and after startup,

means for automatically controlling said flow controlling means to control the turbine load after the turbine reaches synchronous speed,

said automatic controlling means including means for generating electric signals for said flow controlling means as a function of reference and feed back signals,

means for controlling the operation of said flow controlling means in response to the electrical signals and in turn the operating state of said turbine,

means for generating at least one simulated response to predetermined outputs generated by said automatic controlling means,

means for connecting said automatic controlling and said generating means to operate in a simulation mode including means for appling the simulated response to said automatic means,

and means for operating said backup control means to control said turbine when said automatic controlling means is placed in the simulation mode.

22. A control system as set forth in claim 21 wherein the turbine is a steam turbine having inlet steam valves, said flow controlling means includes said valves, and said automatic controlling means provide position control over said valves.

23. A control system as set forth in claim 22 wherein an operator panel is provided with means for generating a simulation mode selection signal, means are provided for coupling said selection means to said automatic controlling means and said simulation response generating means.

24. A turbine as set forth in claim 21 wherein means are provided for generating a signal representing actual turbine speed, said automatic controlling means includes means for generating a speed demand as a function of a speed reference and the actual turbine speed, and said simulated response generating means includes means for generating a simulated turbine speed response as a function of the speed demand and for applying the simulated turbine speed response to speed demand generating means in place of the actual turbine speed when the simulation mode is selected.

25. A control system as set forth in claim 24 wherein said simulated turbine speed response generating means includes a first order lag function generator to which the speed demand is applied.

26. A control system as set forth in claim 24 wherein said automatic controlling means includes a digital computer, said computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

27. A control system as set forth in claim 24 wherein said automatic controlling means includes a digital computer, said computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

28. A control system as set forth in claim 24 wherein an operator panel is provided with means for generating a simulation mode selection signal, means are provided for coupling said selection means to said automatic controlling means and said simulation response generating means, and said operator panel includes means for generating a speed reference signal and means for coupling the speed reference signal to said automatic controlling means during turbine startup.

29. A control system as set forth in claim 28 wherein means are provided for automatically generating a speed reference during turbine startup, and said operator panel includes means for generating an automatic startup select signal which is applied to said automatic controlling means.

30. A control system as set forth in claim 28 wherein said operator panel includes means for generating a load reference signal and means for coupling the load reference signal to said automatic controlling means during the turbine load mode.

31. A control system as set forth in claim 21 wherein means are provided for generating a signal representing actual turbine load, said automatic controlling means includes means for generating a load demand as a function of a load reference and the actual turbine load, and said simulated response generating means includes means for generating a simulated turbine load response as a function of the load demand and for applying the simulated turbine load response to load demand generating means in place of the actual turbine load when the simulation mode is selected.

32. A control system as set forth in claim 31 wherein load demand is impulse pressure demand and the actual load is represented by impulse pressure.

33. A control system as set forth in claim 31 wherein the load demand is an electrical load demand and the actual load is represented by an electrical load signal.

34. A control system as set forth in claim 31 wherein said load demand generating means includes means for generating an electrical load demand as a function of an electrical load reference and actual electrical load and means for generating an impulse pressure demand as a function of the electrical load demand and actual impulse pressure, said simulated response generating means includes an impulse pressure response generator and an electrical load response generator, and said electrical load and impulse pressure generators responding respectively to the electrical load demand and the impulse pressure demand to generate respective simulated generator electrical load and turbine impulse pressure simulation responses for respective application to said electrical load and impulse pressure generators.

35. A control system as set forth in claim 34 wherein said automatic controlling means includes a digital computer, said computer incudes said simulated response generating means, and said backup control means is an analog control external to the computer.

36. A control system as set forth in claim 31 wherein said simulated turbine speed response generating means includes a first order lag function generator to which the speed demand is applied.

37. A control system as set forth in claim 31 wherein means are provided for generating a signal representing actual turbine speed, said automatic controlling means includes means for generating a speed demand as a function of a speed reference and the actual turbine speed, and said simulated response generating means includes means for generating a simulated turbine speed response as a function of the speed demand and for applying the simulated turbine speed response to speed demand generating means in place of the actual turbine speed when the simulation mode is selected.

38. A control system as set forth in claim 31 wherein said automatic controlling means includes a digital computer, said computer includes said simulated response generating means, and said backup control means is an analog control external to the computer.

39. A control system as set forth in claim 31 wherein an operator panel is provided with means for generating a simulation mode selection signal, means are provided for coupling said selection means to said automatic controlling means and said simulation response generating means, and said operator panel includes means for generating a load reference signal and means for coupling the load reference signal to said automatic controlling means during the turbine load mode.