U.S. patent number 3,800,750 [Application Number 05/170,564] was granted by the patent office on 1974-04-02 for method and apparatus for providing a nonlinear pressure transducer output signal.
This patent grant is currently assigned to The Bendix Corporation. Invention is credited to Junuthula N. Reddy.
United States Patent |
3,800,750 |
Reddy |
April 2, 1974 |
**Please see images for:
( Certificate of Correction ) ** |
METHOD AND APPARATUS FOR PROVIDING A NONLINEAR PRESSURE TRANSDUCER
OUTPUT SIGNAL
Abstract
By deriving a substantially linear voltage signal from a
pressure transducer and using that signal to control a plurality of
current sources and current sinks, the controlled currents
generated thereby may be passed through a resistance of known value
to produce a usable output signal having a nonlinear relationship
with respect to the pressure sensed by the transducer. If current
sources to be controlled are designated by N, the resultant curve
can have N-1 breakpoints where the slope of the curve of output
voltage with respect to sensed pressure changes. By controlling a
plurality of current sources which are active for all values of
sensed pressure, the slope of the resultant curve can change from
positive to negative values and back again.
Inventors: |
Reddy; Junuthula N.
(Horseheads, NY) |
Assignee: |
The Bendix Corporation
(Southfield, MI)
|
Family
ID: |
22620377 |
Appl.
No.: |
05/170,564 |
Filed: |
August 10, 1971 |
Current U.S.
Class: |
123/485 |
Current CPC
Class: |
F02D
41/32 (20130101) |
Current International
Class: |
F02D
41/32 (20060101); F02m 051/00 () |
Field of
Search: |
;123/32EA,119 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Goodridge; Laurence M.
Assistant Examiner: Flint; Cort
Attorney, Agent or Firm: Flagg; Gerald K.
Claims
I claim:
1. A fuel control circuit for an internal combustion engine whose
fuel requirement relates nonlinearly to engine air-consumption
related parameter, said control circuit providing a signal having a
value corresponding to engine fuel requirement and comprising:
means for receiving a first signal that is linearly related to the
value of the engine air-consumption related parameter;
a plurality of signal generating circuit subsections, each
including:
means defining a conductive electrical path for providing an output
signal, said conductive path including an impedance element and a
semiconductor means having a first electrode connected to one side
of said impedance element;
control signal means for applying a control signal to a second
electrode of said semiconductor means to control the value of the
output signal, the value of said output signal being determined by
the value of any signal decrease across said impedance element;
output signal varying means for applying values of said first
signal to the second electrode of said semiconductor means to vary
said output signal only when said first signal is displaced in one
direction from the value of said control signal and to maintain
said output signal at a predetermined value greater than zero when
said first signal is displaced in the other direction from said
control signal;
conductor means for commonly connecting a voltage source with the
other side of said impedance element of each of said signal
generating circuit subsection; and
signal combining means connected in series with a third electrode
of each of said semiconductor means of each said signal generating
circuit subsection for combining the output signals from each said
signal generating circuit subsection to produce a signal that
varies in response to first signal variations in a manner
determined by the values of the control signals of each said signal
generating circuit subsections, said control signals having values
that cause said resultant signals to be nonlinearly related to said
variable engine operating parameter and to have a magnitude
proportional to the engine fuel requirement.
2. A fuel control circuit for an internal combustion engine whose
fuel requirement relates nonlinearly to engine air-consumption
related parameter, said control circuit providing a signal having a
value corresponding to engine fuel requirement and comprising:
means for receiving a first signal that is linearly related to the
value of the engine air-consumption related parameter;
a plurality of signal generating circuit subsections, each
including:
means defining a conductive electrical path for providing an output
signal, said conductive path including an impedance element and a
semiconductor means having a first electrode connected to one side
of said impedance element;
control signal means for applying a control signal to a second
electrode of said semiconductor means to control the value of the
output signal, the value of said output signal being determined by
the value of any signal decrease across said impedance element;
output signal varying means for applying values of said first
signal to the second electrode of said semiconductor means to vary
said output signal only when said first signal is displaced in one
direction from the value of said control signal and to maintain
said output signal at a predetermined value greater than zero when
said first signal is displaced in the other direction from said
control signal;
conductor means for commonly connecting a voltage source with the
other sides of said impedance element of each of said
subsections;
signal combining means connected in series with a third electrode
of each said semiconductor means of each said circuit subsections
for combining the output signals from each signal generating
circuit subsections to produce a resultant signal that varies in
response to first signal variations in a manner determined by the
values of the control signals for each of said signal generating
means circuit subsections, said control signals having values that
cause said resultant signals to be nonlinearly related to said
variable engine operating parameter and to have a magnitude
proportional to the engine fuel requirement; and
energy dissipating means connected to said signal combining means
and switchingly connected to said each of said signal generating
circuit subsections for draining energy from said signal combining
means in proportion to the value of signals received from said
signal generating circuit subsections.
3. A fuel control circuit for providing a signal varying with the
engine fuel requirement of an internal combustion engine having a
fuel requirement nonlinearly related to an engine air-consumption
related parameter comprising:
a. an energy source for providing electrical energy;
b. output impedance means for developing an output signal from a
plurality of controllable currents;
c. transducer means for providing an air-consumption signal varying
with said engine air-consumption related parameter;
d. a plurality of controllable current sources, each
comprising:
i. input means electrically connected to receive said
air-consumption signal from said transducer means;
ii. source impedance means electrically connected to receive
electrical energy from said energy source for providing one of said
controllable currents;
iii. output means electrically connecting said source impedance
means to communicate said one controllable current to said output
impedance means; and
iv. current value establishing means connecting said input means
and said output means for establishing said controllable current at
a constant value greater than zero when the values of said
air-consumption signal comprise a first range of values preselected
for each said current source and for establishing said controllable
current at a varying value less than said constant value greater
than zero varying in accordance with a first predetermined
relationship to values of said air-consumption signal when said
air-consumption signal comprises a second range of values
preselected for each said current source;
whereby said each controllable current source communicates just one
of said constant variable currents to said output impedance means
depending on whether said air consumption signal comprises said
preselected first or second ranges and whereby said output
impedance means combines said constant and varying values so that
said output signal varies nonlinearly with said engine
air-consumption related parameter.
4. The fuel control circuit of claim 3 wherein at least one of said
controllable current sources has its said output means electrically
connected to current sink means for establishing a second
predetermined relationship to values of said air-consumption
related parameter by uniformly decreasing the said varying values.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
The instant application is related to commonly assigned copending
applications bearing U.S. Ser. No. 170,565 now U.S. Pat. No.
3,765,380 entitled "Electronic Fuel Control System With
Non-linearizing Means Interconnecting the Pressure Transducer with
the Main Computation Means" by Todd L. Rachel and to my commonly
assigned copending application bearing U.S. Ser. No. 384,481 and
titled "Apparatus and Method for Providing a Nonlinear Pressure
Transducer Output Signal".
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to the field of electronic fuel
control systems for reciprocating piston internal combustion
engines where the consumption of air by the engine constitutes an
input parameter for the electronic fuel control system. More
particularly, the present invention relates to that portion of the
above described field in which the pressure of the air in the
intake manifold is used as prime input paramater to determine the
instantaneous fuel requirements for the associated engine.
Specifically, the present invention relates to means for providing
an electrical signal indicative of sensed pressure and
representative of engine fuel requirements.
2. Description of the Prior Art
The prior art teaches that in electronic fuel control systems for
reciprocating piston internal combustion engines, various devices
may be used to generate an electrical or electronic analog of the
air pressure in the intake manifold of the engine. Such devices
include inductive pressure transducers with an aneroid controlled
movable core, capacitive pressure transducers with an aneroid
controlled movable capacitive plate relationship and aneroid
controlled rheostats or potentiometers. However, it is known that
reciprocating piston internal combustion engines have a fuel
requirement which does not relate in a linear fashion to the air
pressure in the engine intake manifold. As a consequence, it has
been necessary for the fuel control system designers to determine
empirically the shape of the fuel requirement curve as a function
of air pressure for a given engine and to thereafter suitably adapt
or modify one of the known pressure sensors to satisfy the
empirically determined curve. Such solutions are complicated and
expensive to implement since they require a nonlinear movement or
irregularly shaped or formed electrical members. It is, therefore,
an object of the present invention to provide a circuit for
interfacing between a known pressure sensor of simple and
inexpensive construction and the main computing means to provide a
suitably shaped curve of output signal characteristic with respect
to intake manifold air pressure which curve closely matches the
curve of fuel requirement with respect to intake manifold air
pressure. Since such curves may be expected to change slope
frequently and to go from positive to negative slopes, it is a
further object of the present invention to provide such an
interfacing circuit as may produce an output signal characteristic
which changes slope frequently and which may go from negative to
positive or from positive to negative slopes. Keeping the above
objects in mind, it is a specific object of the present invention
to provide an active circuit capable of satisfying the above
enumerated objects.
As the art of electronics becomes more and more sophisticated, the
cost of sensors required to produce an output which is nonlinearly
related to input will begin to represent a more substantial
percentage of the cost of the total system than is currently the
case. It is, therefore, an object of the present invention to
provide an electronic means to interface between a pressure
transducer having a substantially linear response with response to
variations in air pressure which circuitry may be fabricated in
accord with the state of the art of electronics to suitably
nonlinearize the electrical signal produced by the pressure
transducer.
The devices currently available in the prior art are furthermore
handicapped in that they can only provide a very rough
approximation to the desired electrical output for various air
pressure inputs. It is, therefore, a further object of the present
invention to provide an electronic interfacing network for coupling
a resistive aneroid type pressure transducer to the main computing
portion of an electronic fuel control system capable of providing
an electrical response which is nonlinear with respect to
variations in the air pressure in the intake manifold. It is a more
specific object of the present invention to provide such an
interfacing network capable of providing an output electrical
voltage curve having a plurality of points at which the slope of
the curve may change. It is a still more specific object of the
present invention to provide an active electronic interfacing
network which produces a voltage output signal which is nonlinearly
related to a voltage input signal having a substantially linear
relationship with respect to variations in air pressure in the
intake manifold of the associated engine. It is a specific object
of the present invention to provide an electronic interfacing
network comprised of a plurality of current generating means which
may be simultaneously controlled to provide, at a reference
location, an electrical current having a magnitude which is a
nonlinear function of air pressure in the intake manifold.
One proposed solution to the above-noted problem having
sequentially controlled variable current generating means has
required a large number of active solid state devices and has
required information feedback (or precisely sized components) to
match operational characteristics of successively variably operated
current generating means. This had the disadvantages incident to
increased complexity and the statistical unreliability associated
with large numbers of active devices. It is a still further object
of the present invention to provide a nonlinearizing circuit
capable of producing an output response curve capable of smooth or
abrupt transitions in slope and capable of both positive and
negative slopes.
SUMMARY OF THE PRESENT INVENTION
The present invention contemplates generating a voltage signal
which is approximately linearly related to the pressure in the air
intake manifold and using this signal to control a plurality of
current generating means which are arranged to be variably
operative over overlapping selected ranges of air intake manifold
pressure. The present invention further contemplates combining the
currents generated thereby into a single current which is
dissipated through a fixed resistor wherein the voltage drop across
the fixed resistor constitutes the output signal.
An additional aspect of the present invention resides in the
provision of at least one current sink means to provide an
additional source of variation in the current to be dissipated by
the fixed resistance.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 shows a schematic diagram of an electronic fuel control
system which may utilize the present invention.
FIG. 2 shows a block diagram representation of the electronic
control unit of FIG. 1.
FIG. 3 shows a schematic diagram of a preferred embodiment of a
transducer nonlinearizing circuit according to the present
invention.
FIG. 4 shows a graph representative of current generated in
response to variations in the pressure in the intake manifold and
including a graph illustrative of current variation when a current
sink is activated.
FIG. 5 shows a graph of currents generated by selected sources and
currents dissipated by selected sinks for variations in intake
manifold air pressure and a composite resultant curve.
DETAILED DESCRIPTION OF THE DRAWINGS
Referring now to FIG. 1, an electronic fuel control system is shown
in schematic form. The system is comprised of a main coupling means
or electronic control unit 10, a manifold pressure sensor 12, a
temperature sensor 14, an input timing means 16 and various other
sensors denoted as 18. The manifold pressure sensor 12 and the
associated other sensors 18 are mounted on throttle body 20.
Throttle body 20 includes throttle valves 20V operative to control
the flow of air within throttle body passages 20p. Pressure sensor
12 may, for instance, be a potentiometer whose slider member is
coupled to the throttle shaft 20s so that output thereof is a
function of throttle angle, .theta.. The output of the computing
means 10 is coupled to an electromagnetic injector valve member 22
mounted in intake manifold 24 and arranged to provide fuel from
tank 26 via pumping means 28 and suitable fuel conduits 30 for
delivery to a combustion cylinder 32 of an internal combustion
engine otherwise not shown. While the injector valve member 22 is
illustrated as delivering a spray of fuel towards an open intake
valve 34, it will be understood that this representation is merely
illustrative and that other delivery arrangements are known and
utilized. Furthermore, it is well known in the art of electronic
fuel control systems that computing means 10 may control an
injector valve means comprised of one or more injector valve
members 22 arranged to be actuated singly or in groups of varying
numbers in a sequential fashion as well as simultaneously. The
computing means is shown as energized by battery 36 which could be
a vehicle battery and/or battery charging system as well as a
separate battery.
The logic diagram shown in FIG. 2 illustrates the computing means
10 in a non-particularized manner as applied to two-group
injection. In FIG. 2, there is shown a switching device 38 capable
of producing alternating output signals and receiving as input a
signal or signals representative of engine crank angle as from
sensor 16. Mechanically, sensor 16 could be a single lobed cam,
driven by the engine and alternately opening and closing a pair of
contacts. Since this arrangement could generate spurious signals,
as by contact bounce, the switching device 38 will be described and
discussed as a flip flop since the flip flop is known to produce a
substantially constant level of output at one output location and
zero level at the other output location in response to a triggering
signal which need only be a spike input but may also be of longer
duration and a flip flop may be readily made insensitive to other
types of signals. Traces 1 and 2 illustrate the alternating
triggering input signals while traces 3 and 4 illustrate the time
relationship of the two switching device output signals. Signals
received on the nontriggering input will, of course, have no effect
on a flip flop. Outputs 40 and 42 are connected to the inputs of a
logic gate 44. Gate 44 is arranged to give a relatively short
duration pulse whenever the flip flop 38 changes state and to
produce a constant level d.c. output at all other times. Outputs 40
and 42 are also connected to the inputs of a pair of AND gates with
output 40 being connected to one input of AND gate 46 and the
output 42 being connected to one input of AND gate 48. The output
of the gate 44 is connected to the input of an adaptive delay means
50 which receives, as control inputs, signals from the various
engine parameter sensors, as at 52, indicative of engine operating
conditions and, therefore, of engine fuel requirement. As will be
readily observed, one of the inputs at 52 is derived from signal
generator 54 which receives, as its input, the signal .theta.,
derived from the pressure sensor 12 of FIG. 1 and representative of
the instantaneous manifold pressure. Since, according to this
invention, pressure sensor 12 may be a simple potentiometer having
a substantially linear response with respect to pressure, the
derived output signal, which may be a voltage Vpr, is expressed
herein in terms of .theta., and the angular movement of the slider
element of a potentiometer or in terms of V.sub.O the actual
electrical output signal. The output of the adaptive delay means 50
is fed through an inverter 56 and the output of the inverter 56 is
connected to a second input of each AND gate 46 and 48. The output
of AND gate 46 is connected to amplifier 58 which, in turn,
supplies controlling current to the first injector group. AND gate
48 is connected to amplifier 60 which supplies controlling current
to the second injector group.
As will be readily apparent, the presence of an output signal from
the flip flop 38 will occur at one output location to the exclusion
of the other. This signal will then appear at one input of only one
AND gate of only one amplifier. This signal selectively designates
an injector or injector group for imminent injection. For this sake
of example, we shall assume that the output signal of the flip flop
38 is at output location 40 so that the signal also appears at one
input of AND gate 46. The signal from the output 40 of the flip
flop 38 also appears at the gate 44 where, assuming the flip flop
38 has just changed state, a short duration signal is passed to the
adaptive delay means 50. The adaptive delay means 50 is operative
to produce an output after the passage of a predetermined amount of
time. This time is determined by the values of the various sensory
inputs applied at 52 to the adaptive delay 50. During this initial
period of time when the output of the adaptive delay 50 is zero,
the inverter 56 is producing a full-strength output signal. This
signal is applied to one input of each of the AND gates 46 and 48.
Because of the intrinsic nature of AND gates, an output signal is
produced only while an input signal is being applied to each and
every input. This then dictates that AND gate 46 will produce an
output to be amplified by amplifier 58 to open the first injector
group since it is receiving an injector selection command directly
from the flip flop 38 and an injector control command from the
inverter 56. At the end of the time delay period, adaptive delay
means 50 produces a signal which is then inverted from a positive
signal to a zero level signal by the inverter 56 so that the
injection control command output signal of the inverter 56 is
removed from the input to the AND gate 46 and the output of the AND
gate 46 goes to zero thereby allowing the first injector group to
close. During the period of time the first injector group is open,
a metered amount of fuel under pressure is injected by the first
injector group.
Referring now to FIG. 3, the nonlinearizing circuit of the present
invention is illustrated in a preferred embodiment which for
purposes of illustration is shown as including five current
generating means labeled A through E and five current sinking means
labeled V through Z. In addition, circuit 100 also provides a
constant current source 102. Constant current source 102 is used to
provide vertical shift of the composite curve 66 (as illustrated in
FIG. 5). The effect of constant current source 102 has not been
illustrated in FIG. 5.
Constant current source 102 is comprised of a pair of transistors
104, 106, a pair of voltage divider resistors 108 and 110, a load
resistor 112, and a current resistor 114. Resistor 108
intercommunicates the base of transistor 104 to the B+ supply and
resistor 110 intercommunicates the base of transistor 104 to the
ground or common potential. These resistors thereby establish the
conductive condition of transistor 104. Load resistor 11w
intercommunicates the emitter of transistor 104 to ground and the
emitter of transistor 104 is also coupled to the base of transistor
106. Current resistor 114 interconnects the emitter of transistor
106 with the source of electrical supply designated as B+. The
voltage established across the voltage divider network comprised of
resistors 108 and 110 is present at the emitter of transistor 106
and this voltage establishes the amount of current flowing through
current resistor 114. This current will appear substantially
unchanged in output current lead 116 where it will feed into common
conductor 118 to be dissipated across the output resistor 120.
Each of the current generating means A through E is comprised of an
input transistor 122 whose base, or control electrode, is coupled
to the input signal Vpr indicative of manifold pressure, a pair of
voltage divider resistors 124, 126 which interconnect the emitter
of transistor 122 with the source of electrical energy and the
common or ground location, a current controlling transistor 128,
and a current resistor 130. The current resistor 130 interconnects
the emitter of transistor 128 with the source of electrical energy,
and the current flowing therethrough is determined by the voltage
appearing at the base of transistor 128. This voltage is determined
by the voltage divider effect of resistors 124, 126 or the voltage
appearing at the base of transistor 122 (reduced by the
base-emitter voltage drop) whichever voltage is higher. For
convenience, the corresponding elements within each current
generating means A through E bear identical numerals with the
suffix letter corresponding to the particular generating means.
This system of numbering has also been applied to the current
sinking means V, W, X, Y and Z.
The output conductors 132 communicate with switching means 134
having a switch element 136 capable of contacting either of two
terminals 138, 140. Terminal 138 is coupled to the base of
transistor 142 and the base of transistor 142 is also coupled to
the ground or common point by resistor 144. The emitter of
transistor 142 is coupled to a load resistor 146 also going to the
ground or common point. The collector of transistor 142 is coupled
directly to the terminal 140 and a communicating lead 148 couples
terminal 140 to the common conductor 118.
In current sinking means V, X and Y, the switch member
interconnects terminals 134 and 138 while in current sinking means
W and Z, the conducting member 136 interconnects the terminals 134
and 140. The switching structure which is comprised of terminals
134, 138 and 140 and switching member 136 is not considered to be
essential inasmuch as the interconnection provided by the switching
structure will be a permanent interconnection once the specific
output curve of the circuit is determined. Thus, the entire circuit
embodiment of FIG. 3 represents the basic or starting circuit which
would be tailored by the appropriate connection of current lead 132
to either of terminals 138 or 140. Additional variation may be
achieved by using variable resistors for resistances 130, 144 and
146.
In current sinking means W and Z, the lack of a connection to
terminal 138 renders transistor 142 nonconductive and the current
appearing in current leads 132A and 132E will be transmitted via
terminals 140 and output conductor 148 to the common conductor 118
and then through resistor 120 to ground. In current sinking means
V, X and Y, the current appearing in the output current conductor
132 will be dissipated through resistor 144 in such a manner that
transistor 142 is switched into the conduction mode. This will
cause a current to flow out of the common conductor 118 and into
the lead 148 from which it will flow through transistor 142 and
resistor 146 to ground. Thus, taking current sinking means V, for
example, the current generated within current generating means A
will be completely dissipated by resistor 144 while transistor 142
and resistor 146 are operative to extract further amounts of
current from the common conductor 118 thereby lessening the signal
appearing at output terminal V.
Referring now to FIG. 4, a graph is shown illustrating the
relationship of current with respect to variations in air intake
manifold pressure and the input voltage signal Vpr. The input
signal Vpr is directly related to .theta. which may represent, for
example, the angular rotation of throttle valves 20v (in FIG. 1)
from the fully closed position. Two current versus pressure curves
are illustrated with curve 62 showing positive current (i.e.,
current added) and curve 64 showing negative current (i.e., current
subtracted). Curve 64 is intended to illustrate the possibility
that a current sink may be operatively coupled to a current source
to reduce the total current generation while curve 62 illustrates
the regular current output of a current generator. As can be
observed, both values of current start at a low absolute value and
increase to a high absolute value over the range denoted by V.sub.1
and thereafter maintain a constant value equal to 1.sub.1 for curve
62 and 1.sub.2 for curve 64. The magnitude of 1.sub.2 exceeds the
magnitude of 1.sub.1. This is indicative of the fact that with the
illustrated embodiment, the current generated by the associated
current generating means as well as calculatable amounts of current
generated by other current generating means will be dissipated
within a current sink. While a particular current sink may be
coupled to a selected current generating means so that response
over the variable range will be matched, the current sink here
illustrated is adapted to dissipate greater amounts of current than
are generated by the associated current generating means.
Performance over the variable range, as denoted by the range
O-V.sub.l, on the horizontal axis will be controlled by the
variable range of the associated current generating means.
Referring now to FIG. 5, the currents generated by the various
current generating means as modified by the associated current
sinks and a composite current graph is illustrated. The currents
graphed correspond to the circuit illustrated in FIG. 3. The
currents produced are labeled for convenience B and D while the
currents being "sinked" are labeled V, X and Z. As can be seen, the
various curves B, D, V, X and Z, when combined, produce the
composite final shape curve 66. In the graphs of both FIGS. 4 and
5, the vertical axis is labeled + and - to indicate currents
generated (+) and currents "sinked" (-).
The present invention thus clearly satisfies the stated objectives
in the form of the preferred embodiment as well as in those
variations within the skill of the man of ordinary skill in the
art. The current sinks, for example, may be controlled as shown by
connecting selected current generating means to the current sinks
instead of to the output resistance or in the alternative, may be
directly controlled by the input signal to be selectively active
over specific regions of intake manifold air pressure. The specific
form of the various sources and sinks as well as the total number
thereof may also vary.
* * * * *