U.S. patent number 3,825,754 [Application Number 05/381,814] was granted by the patent office on 1974-07-23 for dual spectrum infrared fire detection system with high energy ammunition round discrimination.
This patent grant is currently assigned to Santa Barbara Research Center. Invention is credited to Robert J. Cinzori, Gerald F. Stapleton.
United States Patent |
3,825,754 |
Cinzori , et al. |
July 23, 1974 |
**Please see images for:
( Reexamination Certificate ) ** |
DUAL SPECTRUM INFRARED FIRE DETECTION SYSTEM WITH HIGH ENERGY
AMMUNITION ROUND DISCRIMINATION
Abstract
Disclosed is a multichannel fire or explosion detection system
wherein an output fire suppression or control signal is generated
in response to fires or explosions which radiate power above a
predetermined threshold level. The system includes means which
discriminate against explosive fires in a fuel tank or other highly
combustible material on the one hand and high energy exploding
rounds of ammunition per se which do not subsequently cause a large
scale fire. Thus, the present detection system will not generate an
output fire suppression or control signal in the event a high
energy ammunition round explodes in the vicinity of a fuel tank
without igniting and exploding it. Additionally, fail safe
detection logic means are provided in the present system and
generate a time delayed fire suppression enable signal to thereby
enable an output signal gate in the event of a delayed or secondary
fire or explosion above a predetermined magnitude.
Inventors: |
Cinzori; Robert J. (Santa
Barbara, CA), Stapleton; Gerald F. (Santa Barbara, CA) |
Assignee: |
Santa Barbara Research Center
(Goleta, CA)
|
Family
ID: |
23506483 |
Appl.
No.: |
05/381,814 |
Filed: |
July 23, 1973 |
Current U.S.
Class: |
250/338.1;
250/349; 250/339.15; 340/578 |
Current CPC
Class: |
G08B
17/12 (20130101); G01S 7/2921 (20130101); G01S
1/02 (20130101) |
Current International
Class: |
G01S
1/02 (20060101); G01S 1/02 (20060101); G01S
1/00 (20060101); G01S 1/00 (20060101); G01S
7/292 (20060101); G01S 7/292 (20060101); G08B
17/12 (20060101); G08B 17/12 (20060101); G01t
001/16 () |
Field of
Search: |
;250/338,339,340,349,336
;340/228R |
References Cited
[Referenced By]
U.S. Patent Documents
|
|
|
3147380 |
September 1964 |
Buckingham et al. |
|
Primary Examiner: Lawrence; James W.
Assistant Examiner: Willis; Davis L.
Attorney, Agent or Firm: Bethurum; William J. MacAllister;
W. H.
Claims
What is claimed is:
1. A system for making energy dissipation comparisons while
detecting fires and explosions above predetermined power thresholds
within predetermined time periods including:
a. low threshold radiation channel means responsive to minimum
power fires or explosions for generating output enable signals,
b. high threshold radiation channel means responsive to fires or
explosions which exceed a predetermined energy threshold for
generating inhibit signals of a predetermined time duration or
durations, and
c. output logic gate means coupled to both said low and high
threshold radiation channel means for receiving both said enable
and inhibit signals, said output logic means being operative to
generate an output fire control or suppression signal after the
removal of said inhibit signals therefrom, whereby relatively short
lived fires or explosions within the time duration of said inhibit
signals are prevented from triggering an output fire detection or
control signal.
2. The system defined in claim 1 wherein said high threshold
radiation channel means includes:
a. a threshold gate of a selected switching threshold connected in
the signal path of said high threshold channel means and operative
to generate logic signals of a time duration dependent upon the
energy received from a fire or explosion,
b. first pulse delay generating means connected between said
threshold gate and one input of said output logic gate means for
generating a first inhibit signal of a first predetermined time
duration, and
c. second pulse delay generating means coupled between said
threshold gate and another input of said output logic gate means
for generating a second inhibit signal of a second predetermined
time duration, whereby said output logic gate means is enabled to
generate a fire control or suppression signal after the termination
of said inhibit signals and in the continued presence of enable
signals from said low threshold radiation channel means.
3. The system defined in claim 2 which further includes:
a. a second threshold gate having a second threshold switching
level and connected to receive the radiation responsive detection
signals from the main signal path of said high threshold channel
means to thereby generate enable logic pulses of another, different
predetermined time duration, and
b. a second output logic gate means connected to receive both logic
signals from said second threshold gate and from said second pulse
delay generating means for thereby generating output fire control
or suppression signals when said second output logic gate means is
enabled, thereby imparting an additional level of energy
discrimination to said high threshold radiation channel means.
4. The system defined in claim 3 which further includes an output
OR gate connected to receive the output signals from both said
first and second output logic gate means for generating the
system's output fire control or suppression signals upon receiving
enable signals from either of said first and second output logic
gate means.
5. The system defined in claim 1 wherein said low threshold
radiation channel means includes:
a. long wavelength channel means responsive to radiant energy in a
predetermined spectral band of electromagnetic radiation and
received from a fire or explosion for generating one output logic
signal,
b. short wavelength channel means responsive to radiant energy in
another predetermined spectral band and received from said fire or
explosion for generating another logic signal, and
c. means coupling said one and another output logic signals to said
output logic gate means for properly enabling same during the
presence of a fire or explosion above a predetermined minimum
threshold level.
6. The system defined in claim 5 wherein said coupling means
includes first and second signal delay stages connected in the
signal paths of said long and short wavelength channel means,
respectively, and further connected to first and second inputs of
said first output gate means for providing delayed enable signals
thereto, whereby said first output gate means is not immediately
enabled after the initiation of said fire or explosion, thereby
allowing said high threshold radiation channel means to properly
respond to predetermined energy levels of a radiation received from
said fire or explosion and thereby temporarily inhibit said first
output gate means for predetermined time durations.
7. The system defined in claim 6 wherein:
a. said long wavelength channel means is responsive to radiant
energy in a predetermined spectral band above about 6 microns of
electromagnetic radiation, and
b. said short wavelength channel means is responsive to radiant
energy in a predetermined spectral band less than about 2 microns
of electromagnetic radiation.
8. The system defined in claim 7 wherein said long wavelength
channel means is responsive to radiation in the 7 - 30 micron range
and said short wavelength channel means is responsive to radiation
in the 0.7 - 1.2 micron range, and said high threshold channel
radiation means is responsive to short wavelength radiation in the
0.7 - 1.2 micron range.
9. The system defined in claim 8 wherein:
a. both said high threshold radiation channel means and said short
wavelength radiation channel means includes a photodetector
connected at each input thereof, and
b. said long wavelength channel means includes a thermopile
detector connected at its input and responsive to a radiation in a
spectral band above about 6 microns of electromagnetic
radiation.
10. The system defined in claim 9 wherein said high threshold
radiation channel means includes:
a. a threshold gate of a selected switching threshold connected in
the signal path of said high threshold channel means and operative
to generate logic signals of a time duration dependent upon the
energy received from a fire or explosion,
b. first pulse delay generating means connected between said
threshold gate and one input of said output logic gate means for
generating a first inhibit signal of a first predetermined time
duration, and
c. second pulse delay generating means coupled between said
threshold gate and another input of said output logic gate means
for generating a second inhibit signal of a second predetermined
time duration, whereby said output logic gate means is enabled to
generate a fire control or suppression signal after the termination
of said inhibit signals and in the continued presence of enable
signals from said low threshold radiation channel means.
11. The system defined in claim 10 which further includes:
a. A second threshold gate having a second threshold switching
level and connected to receive the radiation responsive detection
signals from the main signal path of said high threshold channel
means to thereby generate enable logic pulses of another, different
predetermined time duration, and
b. a second output logic gate means connected to receive both logic
signals from said second threshold gate and from said second pulse
delay generating means for thereby generating output fire control
or suppression signals when said second output logic gate means is
enabled, thereby imparting an additional level of energy
discrimination to said high threshold radiation channel means.
12. The system defined in claim 11 which further includes an output
OR gate connected to receive the output signals from both said
first and second output logic gate means for generating the
system's output fire control or suppression signals upon receiving
enable signals from either of said first and second output logic
gate means.
13. A fire or explosion detection system for making predetermined
energy dissipation comparisons including:
a. threshold radiation channel means responsive to fires or
explosions which generate a predetermined amount of energy within a
predetermined period of time to in turn generate inhibit signals,
and
b. output gate means coupled to said radiation channel means and
responsive to said inhibit signals to prevent an output fire
suppression from being generated during the presence of said
inhibit signals, whereby said channel is operative to generate said
fire suppression signals after the termination of said inhibit
signals or in the event that no inhibit signals are generated.
14. The system defined in claim 13 wherein said threshold radiation
channel means includes logic means for generating an inhibit signal
whose time duration is proportional to the time that the radiated
power from said fire or explosion is above a predetermined
threshold level, whereby the variable duration of said inhibit
signals may be logically compared with other fixed signal delays to
prevent predetermined energy levels reached in predetermined
minimum times from generating an output fire control or suppression
signal.
Description
FIELD OF THE INVENTION
This invention relates generally to fire and explosion detection
and suppression systems and more particularly to a fast acting long
and short wavelength responsive multichannel radiation
detector.
BACKGROUND
Fire detection systems which respond to the sudden presence of
either a flame or an explosion to thereby generate an output
control signal are generally known. Such systems have a very
significant utility, for example, in applications with a variety of
explosive or fuel transport or storage tanks, and these systems
normally function to trigger the operation of a fire suppression
mechanism within a few milliseconds after the initiation of a fire
or explosion. It is frequently desirable to wire these fire
detectors into military armored personnel carrier vehicles which
transport various arms and explosives. A possible fire commonly
desired to be suppressed by these types of fire detection systems
is one which is produced in a fuel tank by a high energy round of
ammunition fired into the fuel tank from a remote location.
PRIOR ART
Hitherto, fire detection and suppression systems of the above type
employed one or more photon responsive short wavelength
photodetectors. These photodetectors sense the energy from
radiation emanating from a fire or explosion, such as infrared or
ultraviolet radiation in a particular spectral band and
characteristic of certain chemical elements or compounds within the
fire or explosion. Signals from these photodetectors are properly
compared and processed in order to generate a fire control output
signal. A disadvantage with this type of prior art fire detection
system is that the system is wholly dependent for its proper
operation upon receiving the proper photon energy within a given
spectral band and from the true source of interest, namely the fire
or explosion to be suppressed. As a result, these prior art fire
detection systems are frequently subject to false operation in
response to extraneous noise or other source radiation which is not
associated with a fire or explosion.
Various circuit techniques have been devised to discriminate
against these latter sources of extraneous radiation. But these
techniques have not been totally practical or satisfactory for all
conditions of operation and in the many noisy environments in which
the fire detection system must be capable of operating.
In copending application Ser. No. 375,265 filed June 29, 1973 of
Robert J. Cinzori, assigned to the present assignee, there is
disclosed a basic dual-channel fire and explosion detection system
which operates to eliminate the prior art problem of false
triggering in response to extraneous noise radiation in a
particular spectral band. Briefly, this operation is accomplished
in the above Cinzori copending application by the use of a long
wavelength-responsive radiation detection channel and a short
wavelength-responsive radiation detection channel. These two
channels respond respectively to separate wavelength ranges of
incident electromagnetic radiation and thereby eliminate the above
possibility of false triggering, either by an extraneous noise
source or by chopped radiation from a constant energy source, such
as the sun. However, the above Cinzori application does not provide
means for discriminating between large explosive fires on the one
hand and large explosions which cause no fire on the other. The
latter could be, for example, explosions of rounds of ammunition
which do not subsequently cause a full scale explosive fire. This
discrimination capability may obviously be a desirable feature in
certain fire detection applications in view of the cost and effort
required to suppress large scale fires.
THE INVENTION
The general purpose of the present invention is to provide further
novel and useful improvements to the above identified Cinzori
invention and particularly to provide a novel fire detection system
which features high energy ammunition round discrimination. This
purpose is accomplished by the provision of a three channel
infrared radiation detection system in which the three radiation
responsive channels are interconnected in a novel output logic
configuration. This system provides the above described
discrimination between large scale explosive fires on the one hand
and explosions of high energy ammunition rounds per se which do not
subsequently produce full scale fires or explosions on the other.
Our novel system includes different levels of discrimination in
that initially, a discrimination is made between the energy
generated by an exploding ammunition round impeded by burning and
combustion of surrounding matter and the energy generated by the
round exploding in the atmosphere when no burning or combustion is
present. However, after this initial discrimination, fail-safe
logic means are provided in each of the three radiation detection
channels to thereby respond appropriately to radiation produced by
a secondary or delayed fire which may occur after the above
described initial discrimination indicates that only an ammunition
round has exploded.
The above purposes are specifically achieved by the provision of a
detection system which includes a pair of main signal detection and
processing channels which are responsive to fires or explosions
above a given pan fire threshold level for generating output fire
control logic signals. These two main signal detection channels
each include a signal delay stage which introduces a time delay
into the radiation responsive signals processed in each channel.
These time delayed signals are then combined in the system's output
logic to control same and to generate a system output fire control
or suppression signal in the event the output logic is properly
enabled by further signals processed in another, ammunition round
threshold energy channel. This ammunition round threshold energy
channel, which is also referred to as the "high energy anti-tank
(HEAT) round discrimination channel," or for ease of description
herein merely as the "round channel," has its input detector
coupled to certain round threshold gates which form part of the
round channel's output discrimination logic. This output
discrimination logic operates to generate the necessary enabling
signals for insuring that the detection system produces an output
fire control signal only in the event of a full scale explosive
fire. The discrimination logic is connected in a novel manner (to
be described specifically below) to the system's main signal
channels and to the system's output logic. The signal delays in the
main signal channels, together with the logic signals generated in
the round channel, are combined in the system's output logic in
such a manner as to discriminate against round explosions per se
which do not produce a full scale explosive fire.
Accordingly, an object of the present invention is to provide a new
and improved explosive fire detection system which discriminates
between fires and ammunition round explosions which cause no
fires.
Another object is to provide a highly sophisticated, accurate and
extremely fast acting fire and explosion detection system of the
type described which is insensitive to false triggering, either by
extraneous noise sources or by chopped radiation from static
radiation sources not associated with a fire or an explosion.
A feature of the invention is the provision of a fire and explosion
detection system of the type described which includes various
levels of infrared radiation discrimination, including an initial
discrimination which is made between fires and round explosions
which cause no fire. Thereafter, the system operates in a fail-safe
manner to respond to secondary fires possibly resulting from the
previously sensed ammunition round explosion.
These and other objects and novel features of the present invention
will become more fully apparent in the following description of the
accompanying drawings.
DRAWINGS
FIG. 1 is a block diagram representation of the multi-channel fire
and explosion detection system according to the invention.
FIGS. 2a-2u illustrate a series of twenty-one voltage signal
waveforms at various points in the system of FIG. 1 identified as
letters "a" through "u" and for the sensed condition where an
anti-tank ammunition round hits an explosive target and causes a
full scale explosive fire.
FIGS. 3a-3u illustrate a similar series of 21 voltage waveforms at
the various points "a" through "u" in the system of FIG. 1 for the
two conditions respectively where: (1) the high energy ammunition
round misses the combustible target and causes no explosive fire or
explosion, and (2) the condition where the ammunition round misses
the combustible target, but subsequently causes a secondary fire at
the target.
FIGS. 4a-4u illustrate a series of 21 voltage waveforms at the
various points "a" - "u" in the system of FIG. 1 for the condition
where the ammunition round hits the target, causes an explosive
fire, and yet for some reason generates energy thresholds which are
initially inconsistent with having caused an explosive fire.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
In the following description of the system of FIG. 1, the term
"tank" refers to a fuel tank and will be used interchangeably with
the term "target," inasmuch as the present invention has been
recently experimentally and successfully tested for its proper
operation in response to exploding fuel tanks toward or into which
"anti-tank" rounds of ammunition are fired. Thus, the first case
(CASE I) to be described below with reference to FIG. 2 is for the
condition wherein the round of ammunition hits the tank, causing a
full scale fire. CASE II below describes the condition where the
anti-tank ammunition round misses the fuel tank, explodes itself,
but causes no resultant fire in the fuel tank towards which it was
fired. For this condition, the explosion of the ammunition round is
outside of the fuel tank, rather than inside, and it will result in
a radiated power which rapidly peaks to a maximum (See FIG. 3a) and
then drops off rather sharply, all over a relatively short period
of time, i.e., considerable energy is dissipated over a short
period of time. This latter case will be described below with
reference to FIG. 3.
Reference will also be made to FIG. 3 in the description of CASE
III below wherein the ammunition round explodes outside of the fuel
tank, and yet still produces a delayed or secondary fire. This is
possibly caused by the fuel tank fracturing and the leaking fuel
igniting at some later time. And CASE IV, which is described below
with reference to FIG. 4, describes that condition wherein the
ammunition round hits the fuel tank, thus causing a full scale
explosive fire but for some reason initially appears to have
exploded outside of the fuel tank (an apparent CASE II above). All
of these cases are described in detail immediately following the
brief identification of the various electronic stages of the
functional block diagram in FIG. 1.
Referring now to FIG. 1, the two main radiation detection channels
12 and 14 correspond in general to the two radiation detection
channels 12 and 14 in the above-identified Cinzori application.
These channels are connected as shown to the system's output logic
circuitry 16. A third ammunition round responsive channel 18 is
also connected as shown to drive the output logic circuitry 16, and
the round channel 18 includes therein certain round discrimination
logic 20 to be operationally described in detail.
The two channels 12 and 14 are also referred to herein as "pan
fire" channels, inasmuch as these channels do not discriminate
between explosive fires and exploding rounds of ammunition, and
will, in fact, respond to minimum threshold level or "pan" fires to
generate output signals on lines 22 and 24 which lead into the
output logic 16. These channels 12 and 14 process, respectively,
the 0.9 micron and the 10 micron wavelength radiation which is
passed by a pair of optical filters 26 and 28 with these respective
wavelength pass bands. These optical filters 26 and 28 are of
conventional design and, therefore, are not described in detail
herein.
Briefly, the purpose of these two pan fire channels 12 and 14,
which are capable of operating in the 0.7 - 1.2 micron and the 7 -
30 micron wavelength ranges, respectively, is to rapidly respond to
infrared radiation from relatively low level fires or explosions
and in turn generate output enable signals on lines 22 and 24.
Simultaneously, these channels 12 and 14 operate to prevent false
triggering of the system either by extraneous noise in a certain
spectral band or by chopped radiation from a constant energy
source. The specific operation of these two channels is discussed
in detail in the above Cinzori application. The 0.9 micron pan fire
channel 12 includes an input infrared radiation detector 30 which
is optically coupled to the 0.9 micron narrow band pass filter 28,
and advantageously this detector 30 is a silicon photodiode which
has a spectral response in the 0.7 - 1.2 micron range. This
photodiode detector 28 is connected to an output amplifier stage 32
which amplifies the detector's small signal detection voltage and
applies the amplified signal to the input of an inverter stage 34.
The inverter 34 is in turn connected through a threshold gate 36
which drives a time delay stage 38.
The 10 micron pan fire channel 14 advantageously utilizes a
thermopile or equivalent detector 40 which is operative to respond
to 10 microns of infrared radiation. The detector 40 is optically
coupled to the 10 micron filter 26, and this detector 40 typically
will have a spectral wavelength response in the range between 7 and
30 microns. The small signal output detection voltage from the
detector stage 40 is coupled to a frequency compensating amplifier
44 which, in turn, is coupled to an inverter stage 46. The inverter
stage 46 has its output signal coupled through a threshold gate 48
into a time delay stage 50, and the threshold gates 36 and 48 are
operative, as will be seen, to generate the step function output
pulses 52 and 54 as soon as the rapidly rising input signals
applied thereto reach a certain minimum threshold level. These
pulses 52 and 54 are also illustrated in FIGS. 2f and 2g,
respectively, and the leading edges of these pulses correspond to
the pan fire threshold switching levels of gates 48 and 36
respectively. These latter thresholds are noted as PT.sub.1 and
PT.sub.2 in FIGS. 2b and 2c respectively. The delayed output pulses
from stages 38 and 50 are coupled, as mentioned, into first and
second inputs 24 and 22, respectively, of a first output AND gate
56. The third and fourth input connections 58 and 60 of the AND
gate 56 are connected as shown to the round channel 18 and
controlled thereby in a manner to be described below.
The round channel 18 includes a 0.9 micron wavelength optical
radiation filter 62 which is suitably coupled to the input of an
infrared radiation detector 64, such as a silicon photodiode.
Wavelengths other than 0.9 microns can be used to accomplish the
discrimination according to the invention. However, 0.9 microns was
chosen because photodefectors with an 0.9 micron peak response are
readily available and the maximum HEAT round energy is in the
general spectral vicinity of 0.9 microns. The silicon photodiode
detector 64 may be identical to the photodiode detector 30, and in
fact the stages 28, 30, 32, and 34 can be used in lieu of the
stages 62, 64, 66 and 68. However, this scheme involves the use of
more costly associated signal processing electronics and it is not
the preferred system. The detector 64 has its output signal coupled
through an amplifier stage 66 and into an inverter stage 68, and
the output signal of the inverter 68 is, in turn, connected to the
respective inputs of first and second level round threshold gates
70 and 72, which constitute the input stages of the round
discrimination logic 20. The first level threshold gate 70
generates an output pulse 74 when the round detection input voltage
signal applied thereto reaches a first preestablished threshold
level as will be described. Similarly, the second higher level
threshold gate 72 produces an output voltage pulse 76 when the
input detection voltage applied thereto crosses a second threshold
level which is higher than that of the first level threshold gate
70. The first and second threshold levels of the two gates 70 and
72, respectively, are referenced at points 78 and 80, respectively,
in FIG. 3a.
The round channel 18 further includes a direct signal connection 82
between the output of the second level threshold gate 72 and a
first AND gate 84, and it also includes a second signal path into
the AND gate 84, including a monostable multivibrator 86 and a
delay stage 88 connected as shown. A second AND gate 90 is
connected as shown between the input and output connections for the
monostable multivibrator 86, and the output of the second AND gate
90 is coupled through an inverter stage 92 and into the input of a
signal crossover delay stage 94.
The output of the first AND gate 84 is connected to the input of a
25 second timing multivibrator 96 which, in turn, has one of its
two digital outputs, Q, directly connected to the fourth input
connection 60 of the AND gate 56. The other complementary output Q
of the multivibrator 96 is coupled through a delay stage 98 and
then to one input 100 of a second output AND gate 102. The other
input 104 of the AND gate 102 is directly connected as shown to the
output connection for the first level threshold gate 70, and the
output connections 106 and 108 of the two AND gates 102 and 56,
respectively, are connected to the two input connections for the
system's output OR gate 110.
In a functional and operational sense, the portion of the system
including the monostable 86, the AND gate 90, the inverter 92 and
the delay stage 94 can be considered to constitute a first pulse
delay generating means. Similarly, the delay stage 88, the AND gate
84, the monostable 96 and the delay stage 98 can be considered to
constitute a second pulse delay generating means.
Upon a careful inspection of the voltage waveform diagrams in each
of the FIGS. 2, 3 and 4, the novel round discrimination operation
of the detection system of FIG. 1 will become apparent. Some of the
voltage waveforms in FIGS. 2, 3 and 4, and appearing at various
points in the circuitry of FIG. 1, will not be specifically
mentioned in the following description. The consecutive letters a
through u denoted in FIG. 1 reference those circuit points in the
system of FIG. 1 at which the voltage waveforms in each of FIGS. 2a
- 2u, 3a - 3u and 4a - 4u appear for the particular operations
(CASE I, CASE II, CASE III or CASE IV) described below. Those
voltage waveforms in FIGS. 2, 3 and 4 which are particularly
significant to a full and complete understanding of the operation
of FIG. 1 will be discussed in some detail hereinafter.
Referring now to both FIGS. 1 and 2, consider a first possible
situation, CASE I, where the ammunition round fired hits the fuel
tank and causes an explosive fire. For this condition, the slowly
rising signal voltage in FIG. 2a corresponds in amplitude to the
power radiated from the exploding round and fuel in the tank. Since
the round of ammunition is exploding inside a fuel tank, the
infrared radiation emitted therefrom begins building relatively
slow and this corresponds to an energy transfer from the ammunition
round to the fuel and to the combustion taking place therein. This
produces a corresponding detection voltage at the output of the
detector 64 which, when amplified in stage 66, exceeds neither the
first level threshold of the gate 70 nor the second level threshold
of the gate 72 within the time required to allow the round channel
18 to respond to this radiation. For this reason, the logic levels
in the circuitry section 20 at the outputs of the first and second
level threshold gates 70 and 72 remain unchanged, and for this
condition, the input connections 58 and 60 of the AND gate 56 are
always enabled for a CASE I situation.
Following the initiation of the CASE I explosion in the fuel tank,
the radiation responsive signal voltages in FIGS. 2b and 2c at the
inputs of the threshold gates 48 and 36, respectively, generate the
slightly delayed output pulses 52 and 54 as indicated in FIGS. 2f
and 2g respectively. The delays in these pulses correspond, of
course, to the pan fire thresholds PT.sub.1 and PT.sub.2 of gates
48 and 36, and for this case, there is no change in the signal
levels at points d and e in FIG. 1.
The sharply rising pulses 52 and 54 drive the 4 millisecond delay
stages 50 and 38, respectively, to provide the delayed signals
illustrated in FIGS. 2i and 2j, respectively. When these voltage
signals in FIGS. 2i and 2j swing high to a logical "1" level after
the 4 millisecond delay indicated, all of the inputs 24, 22, 58,
and 60 of the AND gate 56 are enabled to, in turn, produce an
output logical 1 signal (FIG. 2t) on line 108 and at one input of
the system's output OR gate 110. For CASE I, the quiescent logic
level at the other input 106 of the OR gate 110 is low at a logical
"0" and, thus, an output fire suppression or control signal (FIG.
2u) is generated at the output terminal 114 of the OR logic gate
110. During this time, the logic signals in FIG. 2h and in FIGS. 2k
through 2s remain unchanged as a result of the signal level
stability in the round channel 18. So the output signal in FIG. 2t
from the AND gate 56 is generated immediately after the 4
millisecond delays of both of the two signals in FIGS. 2i and 2j,
respectively. The output signal voltage in FIG. 2u at the output of
the OR gate 110 is processed in electronics (not shown) to trigger
a fire suppression or control mechanism (not shown). Such a
mechanism may, for example, control a plurality of valves on a
pressurized bottle of freon gas.
Consider now the next condition (CASE II) where the round of
ammunition misses the fuel tank completely and causes no fire. For
this condition, of course, it is desired that no output signal be
generated at the output of the OR gate 110, and in a true CASE II
condition the explosion per se of the round of ammunition produces
no secondary fire. However, in the absence of the round channel 18,
this operation would not be possible. For CASE II, the signal at
point a in FIG. 1, and shown in FIG. 3a, rises rather sharply as
shown up through the first and second round threshold levels 78 and
80, and then begins to taper off rather sharply back through these
round threshold levels, as indicated. This signature indicates that
the energy from the round is being transferred into the atmosphere
or air and not into a combustible medium, such as gasoline or oil.
Thus, in this case all of the round explosion energy is dissipated
rather quickly.
When the round of ammunition explodes, the "pan fire" voltatages in
FIG. 3b and 3c are generated as in the previous CASE I, and these
signals, in turn, generate the output pulses 52 and 54, shown also
in the voltage waveforms of FIGS. 3f and 3g. These pulses 52 and 54
again initiate the respective switching actions in the 4
millisecond delay networks 50 and 38 which, in turn, produces the
delayed pulses shown in FIGS. 3i and 3j, as in CASE I above. Thus,
at this point in a CASE II operation, the inputs 24 and 22 of the
AND gate 56 are enabled. However, prior to the occurrence of the
leading edges 116 and 118 of the delayed pulses in FIGS. 3i and 3j,
respectively, the voltage of FIG. 3a crossed the first round
threshold level 78 to thereby generate the leading edge 120 of the
output voltage pulse in FIG. 3e. This pulse in FIG. 3e appears as
the output pulse 74 of the first level threshold gate 70 in the
round channel 18, and has a duration corresponding to the time that
the signal in FIG. 3a is above the first threshold level 78.
Therefore, the input 104 to the AND gate 102 is now enabled.
Now, leaving the operation of the AND gate 102 for the moment,
consider the fact that the leading edge 122 of the pulse in FIG. 3d
is generated as the signal voltage in FIG. 3a crosses the second
round threshold level 80 therein as shown. The leading edge 122 of
the square wave pulse in FIG. 3d is followed by its trailing edge
124 thereof, corresponding to the time that the signal in FIG. 3a
crosses back through the threshold level 80. The leading edge 122
in FIG. 3d triggers the monostable multivibrator 86, thus creating
the 5 millisecond pulse shown in FIG. 3h. Since the logic levels in
FIGS. 3d and 3h are at a logical 1, the point k will now swing to a
logical 1, be inverted in stage 92 and cause point n to swing to a
logical 0. Stage 94 will delay the latter pulse at point n by 0.5
milliseconds and drive point o to a logical zero, thereby disabling
the AND gate 56 before the occurrance of leading edges 116 and 118
in FIGS. 3i and 3j. Thus, the AND gate 56 cannot be enabled for the
duration of this disabling pulse at the input connection 56 of this
AND gate 56.
When the trailing edge 126 of the pulse in FIG. 3o returns this
pulse to its high logical level as shown, then the voltage levels
in FIGS. 3i, 3j and 3o all place lines 24 and 22 and 58 into the
AND gate 56 at a high or a 1 logical level. However, the AND gate
56 is still disabled by reason of the fact that input connection 60
thereto was switched to a logical zero level just 0.2 milliseconds
earlier. This can be shown as follows: When the voltage pulse in
FIG. 3d triggered the 5 millisecond duration monostable
multivibrator 86, the leading edge of the voltage pulse in 3h was
delayed for 4.8 milliseconds by he delay stage 88 and then coupled
into one of the inputs 128 of the AND gate 84. The outer input 82
of the AND gate 84 is already enabled at ths time by the voltage in
FIG. 3d, so the pulses in FIGS. 3-l and 3d now enable the AND gate
84 prior to the time that the voltage in FIG. 3a cross back through
the second threshold level 80. At this point in time, the output
pulse shown in FIG. 3m is generated to energize the 25 second
monostable multivibrator stage 96 so as to drive its output
waveform Q in FIG. 3p from a high logical level to a low logical
level to thereby maintain the AND gate 56 disabled for at least 25
more seconds. If the detection system in FIG. 1 is now actually
seeing a CASE II condition described above, then the voltages in
FIGS. 3i and 3j will be returned to their low or zero logical
levels by the end of this 25 second period. Thus, in the absence of
a secondary fire, it will not be possible for the AND gate 56 to be
enabled after the voltage in FIG. 3p returns again to its high
logical state after 25 seconds.
Consider now the CASE III situation where the round of ammunition
explodes outside the fuel tank to generate the rapidly rising and
falling voltage in FIG. 3a, but for some reason causes a delayed or
"secondary" fire in the fuel tank. This could be caused, for
example, by flack piercing the fuel tank and causing a short delay
in the fuel leaking therefrom, which subsequently ignites. This
secondary fire will, after some time, return the voltage signal in
FIG. 3a back to the first threshold level 78 as indicated at point
130 in FIG. 3a. When this happens, the positive going output pulse
74 (FIG. 3e) at the output of threshold stage 70 will enable the
input 104 of the AND gate 102. The Q output of stage 96 goes to a
logical 1 level at the beginning of the 25 second pulse duration in
FIG. 3q, and the delay gate 98 delays this signal for another 65
milliseconds. This causes the output of stage 98 to subsequently
swing to a logical 1 as shown in FIG. 3r, so that the AND gate 102
is now enabled at the leading edge 130 of the pulse in FIG. 3r. The
output pulses in FIGS. 3s and 3u are generated for this CASE III
situation when the voltage in FIG. 3a once again crosses the first
threshold level at point 131.
At the end of the 25 second pulse duration of the monostable
multivibrator 96, the Q output of this stage 96 (FIG. 3q) returns
to its low logical condition to disable the AND gate 102, and the Q
signal on line 60 leading into the AND gate 56 returns to its high
logical level to now again enable this input and prepare the fire
detection system for another detection operation. Now inputs 58 and
60 of AND gate 56 are again high, so that the main signal
processing channels 12 and 14 are now ready to respond to
appropriate wavelength infrared radiation to once again enable the
AND gate 56.
Referring now to FIG. 4, consider a CASE IV situation wherein an
ammunition round hits the fuel tank and causes an explosive fire
therein, but for some reason also causes the voltage in FIG. 4a to
exceed both the first and second level thresholds as indicated at
points 132 and 134 in FIG. 4a. However, for this CASE IV condition,
the minimum energy requirement (See FIG. 3a) of CASE II above is
not satisfied, since the round did explode in whole or in part in
the tank, or at least hit the tank in some fashion. The latter
condition causes the signal in FIG. 4a to fall rapidly back through
the second and first round threshold levels 78 and 80 as indicated
at points 138 and 136, respectively. Thus, for CASE IV, the minimum
energy requirement for the "round missed-no fire" CASE II situation
above is not satisfied; but the round threshold levels 78 and 80
noted above are exceeded. Thus, the electronics of FIG. 1 must now
be capable of generating an output fire control signal (FIG. 4u)
for this condition, since a full scale fire and explosion is
produced.
For this CASE IV condition, the signals in FIGS. 4b and 4c are
generated immediately following the explosion of the round. When
the pan fire thresholds PT.sub.1 and PT.sub.2 of channels 14 and 12
are exceeded, as noted in FIGS. 4b and 4c, then the corresponding
signal voltages in FIGS. 4f and 4g are driven to a high logical
level as indicated. The voltage pulses 52 and 54 (FIGS. 4f and 4g)
at the outputs of the threshold gates 48 and 36, respectively, are
each delayed 4 milliseconds in the delay stages 50 and 38, and they
subsequently appear as the delayed signals in FIGS. 4i and 4j as
shown at the input 22 and 24 of the AND gate 56. Thus, at the end
of the 4 milliseconds delay indicated in FIGS. 4i and 4j, the lines
22 and 24 leading into AND gate 56 are in the high or "enabled"
state.
Consider now the signal level condition on line 58. When the second
round threshold level at point 134 in FIG. 4a was initially
crossed, the AND gate 90 was temporarily enabled to thereby
generate the leading edge 140 of the pulse shown in FIG. 4k. Thus,
voltage level in FIG. 4k is temporarily driven high and inverted in
stage 92, so that the delayed signal input 58 to AND gate 56 is
temporarily disabled for a CASE II situation. Line 60 is also high,
so at this time only line 58 into AND gate 56 is disabled. However,
upon the return of the signal in FIG. 4a back through the second
threshold level 80 and upon the occurrence of the trailing edge 142
of the delayed pulse in FIG. 4o at the output of delay stage 94,
the signal level on line 58 is again driven high at a time just
prior to the occurrence of leading edges 144 and 146 of the pulses
in FIGS. 4i and 4j, respectively. Thus, upon the occurrence of the
leading edges 144 and 146 of these latter pulses, all four inputs
22, 24, 58 and 60 of the AND gate 56 are enabled, and output
signals will be generated as shown in FIGS. 4t and 4u.
Since the voltage pulse in FIG. 4h is delayed 4.8 milliseconds in
the delay stage 88 and appears as the narrow delayed pulse in FIG.
4-l at the input 128 of the AND gate 84, then this pulse in FIG.
4-l first occurs at a time when the voltage pulse in FIG. 4d on
line 82 has terminated at its trailing edge 148. This, of course,
is the result of the signal in FIG. 4a crossing back through the
second round threshold level as noted at point 136. Therefore, the
lines 128 and 82 are never simultaneously at a high logical level
in CASE IV, and thus the AND gate 84 is not enabled for this
operation.
Thus, the AND gate 84 output signal as shown in FIG. 4m remains at
a logical 0 level for a CASE IV condition, and the 25 second
monostable multivibrator stage 96 is never enabled for this CASE IV
condition. Therefore, the output signal voltage in FIG. 4p remains
continuously at the high logical level, and the output voltage
pulse in FIG. 4t is generated simultaneously with the occurrence of
the leading edges 144 and 146 of the pulses in FIGS. 4i and 4j,
respectively The pulse in FIG. 4t generates the corresponding
output pulse in FIG. 4u at the output of the OR gate 110. Thus, the
fire detection system described above is constructed to provide a
fire control or suppression signal as shown in FIG. 4u,
notwithstanding the fact that the round thresholds at points 132
and 134 in FIG. 4a have been exceeded.
It will be appreciated by those skilled in the art that the present
invention is not limited to the particular types of radiation
detectors used or to the specific spectral bands disclosed.
Furthermore, the particular logic techniques disclosed could
obviously be modified by a logic designer to vary the switching
response of the system in order to meet certain fire detection
application requirements.
It should also be understood that the present invention is not
limited in its use to any particular type of output fire
suppression means. One suitable technique for suppressing fires and
explosions which is most compatible for use with the detection
system described above utilizes a plurality of pressurized freon
gas bottles, each of which are electro-mechanically driven by a
count down register (not shown) at the output of the above
described system. Each successive output pulse generated by the
system can be utilized to drive the count down register (which is
of conventional design), so as to activate a separate bottle each
time there is a fire or explosion. In this manner the system can be
used to fully guard against a condition where the system operates
to extinguish an initial fire, and then is not equipped for further
response to a delayed or secondary fire, or even to a second
primary fire which occurs later at the same location. As a
practical matter, the pressurized bottles of freon are presently
commercially available and contain the necessary gas exit orifices,
so that the freon gas exits these orifices under a very high
pressure and completely empties the bottle in about 20 milliseconds
or less.
It is also to be understood and it will be appreciated by those
skilled in the digital electronics arts that the novel energy
discrimination techniques and concepts of this invention may be
carried out using only the round channel of FIG. 1 or some design
modification thereof. For example, if it is desired to only
discriminate between exploding ammunition rounds whose released
energy is unsuppressed (on the outside of the fuel tank) and
exploding ammunition rounds whose released energy is totally or
partially suppressed (exploding inside the fuel tank or otherwise
suppressed in energy by the fuel tank), then the round channel
alone is capable of performing this energy discrimination function.
Thus, the round channel will either respond to full scale explosive
fires and generate an output signal after a predetermined period of
time; or the round channel will generate inhibit signals when
minimum energy requirements are met and then still produce an
output fire control signal after the termination of the inhibit
signal in the event that a secondary or delayed full scale
explosive fire is caused. In the absence of this full scale
explosive fire after the explosion of an unsuppressed ammunition
round, then the inhibit signals will properly prevent output fire
control or suppression signals from being generated. Of course,
when only the round channel 18 is used, then it is subject to false
operation; for example, by chopped radiation by a constant energy
source, i.e., the sun. This single channel operation may obviously
be desirable in certain applications which have other measures for
preventing such false operation.
* * * * *