US2762034A - Fire and explosion detection apparatus - Google Patents
Fire and explosion detection apparatus Download PDFInfo
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- US2762034A US2762034A US410016A US41001654A US2762034A US 2762034 A US2762034 A US 2762034A US 410016 A US410016 A US 410016A US 41001654 A US41001654 A US 41001654A US 2762034 A US2762034 A US 2762034A
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- explosion
- detector
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C99/00—Subject matter not provided for in other groups of this subclass
- A62C99/009—Methods or equipment not provided for in groups A62C99/0009 - A62C99/0081
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- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B17/00—Fire alarms; Alarms responsive to explosion
- G08B17/06—Electric actuation of the alarm, e.g. using a thermally-operated switch
Definitions
- This invention relates to apparatus for the detection of fire and of explosions. It is designed to operate in conjunction with an extinguishing device to suppress fires and explosions before they have reached dangerous proportions.
- a fire detector In order not to be subject to false alarms, a fire detector must detect some physical phenomenon exclusively associated with fires in the environment in which the detector is to operate.
- One of the properties of flames is that the radiant energy emanating therefrom is modulated in amplitude. this flicker occurs at fi'equencies in the sub-audio and lower audio ranges.
- Avery satisfactory fire detector distinguishes flames from other sources of flickering radiation by means of a band-pass filter which makes the detector sensitive only to flicker within lower and upper frequency
- the lower frequency limit which may be of the order of five cycles per second, prevents the actuation of the fire detector by very low frequency transients occurring, for instance, when venetian blinds are lowered.
- the upper frequency limit which may be of the order of twenty-five cycles per second, prevents the actuation of the fire detector by the flicker of lamps energized by alternating current.
- An integrating device is also provided to prevent the actuation of the fire detector until the occurrence of several cycles of flicker within the band-pass frequencies.
- An explosion detector and suppressor system has been proposed in which the detector comprises a pressureresponsive device which detects the rise in pressureoccurring in an incipient explosion.
- This detector operates a suppressor which is designed to release an explosion or fire-suppressing fluid.
- the suppressor comprises a frangible container for the explosion-suppressing fluid.
- a fastacting detonator which is actuated by the detector, is arranged to burst the container and thus scatter the explosion or fire suppressing fiuid which it contains.
- This explosion detector of the radiation type comprises a photocell the output of which is connected to an electronic valve through a diflerentiating network. This valve, which is normally nonconductive, conducts when the photocell detects a rise of radiation of the type found in incipient. explosions.
- the output of a radiation-sensitive cir cuit is used to operate an extinguishing device in the presence of a flame and in the presence of an incipient explosion.
- the flame detector channel between the photocell and the extinguishing device comprises a band-pass amplifier and an integrating circuit.
- the extinguishing device operates only after several cycles of flicker within the band passed by the amplifier have impinged on the photocell.
- An explosion-detector channel also connected between the photocell and the extinguishing device, bypasses most of the amplifier and the integrating circuit and operates the extinguishing device in the presence of a steep rise of radiation impinging upon the photocell 13.
- a resistor 11 and a photoconductive cell 13 connected in series be tween a power-supply terminal 15 and ground.
- the photoconductive cell 13 may be a lead sulfide cell, and its resistance at room temperature may be of the order of half a million ohms.
- the resistor 11 and the photocell 13 form a potential divider, and the potential at their junction point 17 is a function of the radiant energy impinging upon the photocell 13.
- the junction point 17 is connected through a first RC circuit comprising capacitor 19 and resistor 21 to a first amplifier comprising tube section 23, biasing resistor 25' and a load resistor 27 one end of which is connected to power-supply terminal 29.
- the anode terminal 31 of tube section 23 is connected through a second RC circuit comprising capacitor 33 and resistor 35 to a second amplifier comprising tube section 37, biasing resistor 39 and a load resistor 41.
- the anode terminal 43- of tube section 37 is connected through a third RC circuit comprising capacitor 45 and resistor 47 and a fourth RC circuit comprising resistor 49 and capacitor 51 to a third amplifier comprising tube section 53 and load resistor 55.
- The'anode terminal 57 of tube section 53 is connected to ground through a capacitor 59, and through an RC circuit comprising capacitor 61 and resistor 63 to the junction 65 of diodes 67 and 69.
- the cathode of diode 67- is connected to junction point 65, and its anode is connected to ground;
- the anode of diode 69 is connected to junction point 65, and its cathode is connected toground through resistor 71 and through an RC circuitcomprising resistor 73 and capacitor 75 to a fourth amplifier comprising tube section 77, biasing resistors 79 and 81, and a load 83 which is the coil of relay 85.
- the operation of the fire detector is as follows: in the presence of a flame, the flickering radiation which emanates therefrom'and impinges upon photocell 13 causes a corresponding fluctuation in the potential at junction point 17.
- This flicker comprises a plurality of frequencies having different amplitudes, the lower frequencies usually having greater amplitudes than the higher frequencies.
- the fluctuating potential .at junction 17, hereinafter termed signal goes through three stages of amplification, i. e., through tube sections 23, 37, and 5 3, before it reaches the anode 57 of tube section 53.
- the lowfrequency flicker components are attenuatedby means of the three RC circuits comprising capacitors 19,33, and 45 and resistors 21, 35, and 47, respectively.
- the RC circuit comprising resistor 49 and capacitor 51 is a low-pass filter designed to attenuate any residual ripple in the power supply: in the embodiment shown in the drawing, this RC circuit is designed. to attenuate the ripplefound in standard aircraft power supplies, which are energized by a 400 cycle line.
- the lowfrequency attenuation introduced between junction 17 and the anode 57 of tube section 53 is such that at the anode 57 flicker components in the band from 5 to 25 cycles appear to have magnitudes of the same order.
- Tube section 53 clips the amplified signal applied thereto, and the signal at its anode 57 would look like a series of square waves but for the presence of capacitor 59.
- Capacitor 59 charges slowly when tube section 53 is nonconductive and discharges rapidly when tube section conducts, so that the waveform of the signal at the anode 57 of tube 53 resembles a saw-tooth.
- This saw-tooth is differentiated over the RC circuit comprising capacitor 6.1 and resistor 63, the resulting waveform comprising positive and negative-going pulses.
- the negative-going pulses do not appear in the circuit,.as they are shortcircuited to ground by diode 67.
- the positivegoing pulses are passed by the diode 69.
- the signal at the cathode 91 of diode 69 thus comprises a series of positive pulses.
- these pulses are spaced farther apart than they are for a signal of higher frequency, in which case these pulses are bunched together.
- These pulses are integrated over the RC network comprising'resistor 73 and capacitor 75 and build on capacitor 75 a positive potential which is applied to the control grid of the relay tube 77.
- resistor 71 due to the presence of resistor 71, the charge built up on capacitor 75 is allowed to leak through resistors 73 and 71 to ground.
- Tube section 77 is held in a normally nonconductive state by applying a biasing potential to its cathode 95 by means of biasing resistors 79 and 81 connected in series between power-supply terminal 29 and ground. Resistor 81 is shown as a variable resistor to adjust the bias on tube section 77. Conduction through tube section 77 closes the relay 35 which operates the extinguishing device Before tube 77 conducts (and operates the extinguishing device 97), a positive potential of sufiicient magnitude must be built up on the capacitor 75.
- the pulses at cathode 91 are not close together, and not enough charging energy is applied to capacitor 75 to overcome the leak to ground through resistors 73 and 71 and thus build up enough of a positive potential on capacitor 75 to overcome the bias on tube section 77. If, on the other hand, the signal is of higher frequency (5 to 25 cycles, 'for instance), the pulses at cathode 91 are bunched together andbuild up enough ofv a potential on capacitor 75, in spite of the leak to ground through resistors 73 and 71, to overcome the bias on tube section 77. With its bias overcome, tube section 77 conducts, the relay 85 closes, and the extinguishing device 97 operates.
- the extinguishing device 97 In order to detect and suppress explosions, the extinguishing device 97 must be actuated very fast in the presence of a sudden rise in radiation impinging upon the photocell 13.
- a neon lamp 99 which is normally nonconductive, is connected between the anode terminal 31 of tube section 23 and the control grid of tube section 77.
- the sudden drop in resistance of photocell '13 causes a sharp negativegoing pulse to occur at junction point 17.
- This pulse which is sharp enough to be passed by the difierentiating circuit comprising capacitor 19 and resistor 21, greatly reduces or completely cuts ofi the conduction in tube section 23. This causes a sharp rise in the potential at the anode terminal 31 of tube section 23.
- the neon lamp 99 is part of a potential divider connected between a detonator 105.
- the wall of the housing 103 is re-' Jerusalem in thickness at the working end of the detonator 105.
- a frangible cup 107 made of phenolic-impregnated fabric, is securely attached to the backing plate 101 and forms a sealed cavity 109 in which an extinguishing agent is placed.
- the detonator is connected through the relay to the supply terminal 29 in such a way that it is operated when relay 85 closes.
- the detonator When the detonator operates, it shatters the frangible container 107,'scattering the extinguishing agent which it contains and suppressing a fire or explosion in the vicinity of the extinguishing device 97.
- both the photocell 13 and the extinguishing device 97 are placed in the volume to be protected, which may be, for instance, the interior of a wing of an aircraft.
- the fire detector operates the extinguishing device after 0 several cycles of flickering radiation have impinged upon the photocell 13. This is attained by means of a bandpass amplifier and an integrating circuit.
- the explosion detector also utilizes photocell 13 and by-passes most of the band-pass amplifier and the integrating circuit: it operates the extinguishing device within a small fraction of a second in the presence of a steep rise in the amount of radiant energy impinging upon the photocell 13.
- a fire and explosion'detector comprising a radiationsensitive circuit, an output device, a flame-detector channel comprising a band-pass amplifier and an integrating circuit, means connecting said flame-detector channel between said radiation-sensitive circuit and said output device, an explosion-detector channel responsive only to a steep rise in radiant energy impinging upon said radiationsensitive circuit, and means to connect said explosiondetector channel in shunt with said flame-detector channel.
- a fire and explosion detector comprising: a radiationsensitive circuit including a photoelectric cell, an amplifier tube having an input electrode and an output electrode, a differentiating circuit connected between the radiation-sensitive circuit and the input electrode of said amplifier tube, an output tube, a band-pass amplifier and an integrating circuit connected between the output electrode of said amplifier tube and said output tube, an explosion-detector channel responsive only to a steep rise in radiant energy impinging upon said photocell, and
Description
Sept. 4, 1956 B. T. JOYCE ET Al.
FIRE AND EXPLOSION DETECTION APPARATUS Filed Feb. 12, 1954 R E C Y E H m o u N 0 R R m T. K m T w m F A N O T p w E w y R B B A Y. B J
4 Claims. (Cl. 340227) This invention relates to apparatus for the detection of fire and of explosions. It is designed to operate in conjunction with an extinguishing device to suppress fires and explosions before they have reached dangerous proportions.
' In order not to be subject to false alarms, a fire detector must detect some physical phenomenon exclusively associated with fires in the environment in which the detector is to operate. One of the properties of flames is that the radiant energy emanating therefrom is modulated in amplitude. this flicker occurs at fi'equencies in the sub-audio and lower audio ranges. Avery satisfactory fire detector distinguishes flames from other sources of flickering radiation by means of a band-pass filter which makes the detector sensitive only to flicker within lower and upper frequency The lower frequency limit, which may be of the order of five cycles per second, prevents the actuation of the fire detector by very low frequency transients occurring, for instance, when venetian blinds are lowered. The upper frequency limit, which may be of the order of twenty-five cycles per second, prevents the actuation of the fire detector by the flicker of lamps energized by alternating current. An integrating device is also provided to prevent the actuation of the fire detector until the occurrence of several cycles of flicker within the band-pass frequencies.
One of the properties of an explosion of a mixture of a combustible vapor with air, as compared with the explosion of a substance which carries its own oxygen, is that it begins with a relatively slow build-up of energy, with correspondingly slow rises of pressure, heat, and radiation. This rise may be spread over several hundredths of a second before a critical energy level. is reached and a dangerous explosive pressure is developed.
An explosion detector and suppressor system has been proposed in which the detector comprises a pressureresponsive device which detects the rise in pressureoccurring in an incipient explosion. This detector operates a suppressor which is designed to release an explosion or fire-suppressing fluid. The suppressor comprises a frangible container for the explosion-suppressing fluid. A fastacting detonator, which is actuated by the detector, is arranged to burst the container and thus scatter the explosion or fire suppressing fiuid which it contains. This explosion-detecting and suppression system is described in detail in British Patent No. 643,188, published September 15, 1950.
It has been proposed to replace the pressure-responsive explosion detector by a faster-acting detector which is responsive to the rate of rise of electromagnetic radiation which occurs in an incipient explosion. This explosion detector of the radiation type comprises a photocell the output of which is connected to an electronic valve through a diflerentiating network. This valve, which is normally nonconductive, conducts when the photocell detects a rise of radiation of the type found in incipient. explosions.
In other words, flames flicker, and i 2,762,034 Patented Sept. 4, 1956 Conduction through the valve actuates the explosion suppressor.
It is an object of the present invention to provide apparatus which is capable of detecting both fires and explosions and of operating an extinguishing device before such fires or explosions have reach dangerous proportions.
In accordance with the illustrated embodiment of the present invention, the output of a radiation-sensitive cir cuit is used to operate an extinguishing device in the presence of a flame and in the presence of an incipient explosion. The flame detector channel between the photocell and the extinguishing device comprises a band-pass amplifier and an integrating circuit. The extinguishing device operates only after several cycles of flicker within the band passed by the amplifier have impinged on the photocell. An explosion-detector channel, also connected between the photocell and the extinguishing device, bypasses most of the amplifier and the integrating circuit and operates the extinguishing device in the presence of a steep rise of radiation impinging upon the photocell 13.
Other and incidental objects of the present invention will be apparent to those skilled in the art from a reading of the following specification and an inspection of theaccompanying drawing which shows a circuit diagram of an embodiment of the present invention.
Referring to the drawing, there is shown a resistor 11 and a photoconductive cell 13 connected in series be tween a power-supply terminal 15 and ground. The photoconductive cell 13 may be a lead sulfide cell, and its resistance at room temperature may be of the order of half a million ohms. The resistor 11 and the photocell 13 form a potential divider, and the potential at their junction point 17 is a function of the radiant energy impinging upon the photocell 13.
The junction point 17 is connected through a first RC circuit comprising capacitor 19 and resistor 21 to a first amplifier comprising tube section 23, biasing resistor 25' and a load resistor 27 one end of which is connected to power-supply terminal 29. The anode terminal 31 of tube section 23 is connected through a second RC circuit comprising capacitor 33 and resistor 35 to a second amplifier comprising tube section 37, biasing resistor 39 and a load resistor 41. The anode terminal 43- of tube section 37 is connected through a third RC circuit comprising capacitor 45 and resistor 47 and a fourth RC circuit comprising resistor 49 and capacitor 51 to a third amplifier comprising tube section 53 and load resistor 55.
The'anode terminal 57 of tube section 53 is connected to ground through a capacitor 59, and through an RC circuit comprising capacitor 61 and resistor 63 to the junction 65 of diodes 67 and 69. The cathode of diode 67-is connected to junction point 65, and its anode is connected to ground; The anode of diode 69 is connected to junction point 65, and its cathode is connected toground through resistor 71 and through an RC circuitcomprising resistor 73 and capacitor 75 to a fourth amplifier comprising tube section 77, biasing resistors 79 and 81, and a load 83 which is the coil of relay 85.
The operation of the fire detector is as follows: in the presence of a flame, the flickering radiation which emanates therefrom'and impinges upon photocell 13 causes a corresponding fluctuation in the potential at junction point 17. This flicker comprises a plurality of frequencies having different amplitudes, the lower frequencies usually having greater amplitudes than the higher frequencies. A: very rough estirnateof the relationship between the amplitude and the frequency of flicker components emanating from a typical fire would be that, above one cycle per second, the amplitude of a flicker component is flicker in the range from 5 to 25 cycles per second, means are provided to attenuate the high-magnitude, low-frequency flicker components.
The fluctuating potential .at junction 17, hereinafter termed signal, goes through three stages of amplification, i. e., through tube sections 23, 37, and 5 3, before it reaches the anode 57 of tube section 53. The lowfrequency flicker components are attenuatedby means of the three RC circuits comprising capacitors 19,33, and 45 and resistors 21, 35, and 47, respectively. The RC circuit comprising resistor 49 and capacitor 51 is a low-pass filter designed to attenuate any residual ripple in the power supply: in the embodiment shown in the drawing, this RC circuit is designed. to attenuate the ripplefound in standard aircraft power supplies, which are energized by a 400 cycle line.
Thus, even though at junction 17 the low-frequency flicker components have a considerably greater magnitude than flicker components of higher frequencies, the lowfrequency attenuation introduced between junction 17 and the anode 57 of tube section 53 is such that at the anode 57 flicker components in the band from 5 to 25 cycles appear to have magnitudes of the same order.
Tube section 53 clips the amplified signal applied thereto, and the signal at its anode 57 would look like a series of square waves but for the presence of capacitor 59. Capacitor 59 charges slowly when tube section 53 is nonconductive and discharges rapidly when tube section conducts, so that the waveform of the signal at the anode 57 of tube 53 resembles a saw-tooth. This saw-tooth is differentiated over the RC circuit comprising capacitor 6.1 and resistor 63, the resulting waveform comprising positive and negative-going pulses. However, the negative-going pulses do not appear in the circuit,.as they are shortcircuited to ground by diode 67. The positivegoing pulses are passed by the diode 69.
The signal at the cathode 91 of diode 69 thus comprises a series of positive pulses. For a low-frequency signal, these pulses are spaced farther apart than they are for a signal of higher frequency, in which case these pulses are bunched together. These pulses are integrated over the RC network comprising'resistor 73 and capacitor 75 and build on capacitor 75 a positive potential which is applied to the control grid of the relay tube 77. However, due to the presence of resistor 71, the charge built up on capacitor 75 is allowed to leak through resistors 73 and 71 to ground.
Tube section 77 is held in a normally nonconductive state by applying a biasing potential to its cathode 95 by means of biasing resistors 79 and 81 connected in series between power-supply terminal 29 and ground. Resistor 81 is shown as a variable resistor to adjust the bias on tube section 77. Conduction through tube section 77 closes the relay 35 which operates the extinguishing device Before tube 77 conducts (and operates the extinguishing device 97), a positive potential of sufiicient magnitude must be built up on the capacitor 75. If the signal is a low-frequency signal (1 to 4 cycles per second, for instance), the pulses at cathode 91 are not close together, and not enough charging energy is applied to capacitor 75 to overcome the leak to ground through resistors 73 and 71 and thus build up enough of a positive potential on capacitor 75 to overcome the bias on tube section 77. If, on the other hand, the signal is of higher frequency (5 to 25 cycles, 'for instance), the pulses at cathode 91 are bunched together andbuild up enough ofv a potential on capacitor 75, in spite of the leak to ground through resistors 73 and 71, to overcome the bias on tube section 77. With its bias overcome, tube section 77 conducts, the relay 85 closes, and the extinguishing device 97 operates. Signal frequencies over 25 cycles usually have low amplitudes at point 17 to start out with, and are attenuated by the capacitor 59 between anode 57 and ground. Thus, the fire detector of the drawing is responsive only to flicker in the range of 5 to 25 cycles per second, and several cycles of flicker in that range have to be integrated before the extinguisher operates.
In order to detect and suppress explosions, the extinguishing device 97 must be actuated very fast in the presence of a sudden rise in radiation impinging upon the photocell 13. For this purpose, a neon lamp 99, which is normally nonconductive, is connected between the anode terminal 31 of tube section 23 and the control grid of tube section 77.
in the presence of a steep rise in radiation, such as those occurring in incipient explosion, the sudden drop in resistance of photocell '13 causes a sharp negativegoing pulse to occur at junction point 17. This pulse, which is sharp enough to be passed by the difierentiating circuit comprising capacitor 19 and resistor 21, greatly reduces or completely cuts ofi the conduction in tube section 23. This causes a sharp rise in the potential at the anode terminal 31 of tube section 23. The neon lamp 99 is part of a potential divider connected between a detonator 105. The wall of the housing 103 is re-' duced in thickness at the working end of the detonator 105. A frangible cup 107, made of phenolic-impregnated fabric, is securely attached to the backing plate 101 and forms a sealed cavity 109 in which an extinguishing agent is placed. These construction details, which are not shown in the drawing, are illustrated in British Patent No. 643,188, supra.
The detonator is connected through the relay to the supply terminal 29 in such a way that it is operated when relay 85 closes. When the detonator operates, it shatters the frangible container 107,'scattering the extinguishing agent which it contains and suppressing a fire or explosion in the vicinity of the extinguishing device 97. In a practical installation, both the photocell 13 and the extinguishing device 97 are placed in the volume to be protected, which may be, for instance, the interior of a wing of an aircraft.
The fire detector operates the extinguishing device after 0 several cycles of flickering radiation have impinged upon the photocell 13. This is attained by means of a bandpass amplifier and an integrating circuit. The explosion detector also utilizes photocell 13 and by-passes most of the band-pass amplifier and the integrating circuit: it operates the extinguishing device within a small fraction of a second in the presence of a steep rise in the amount of radiant energy impinging upon the photocell 13.
We claim:
1. A fire and explosion'detector comprising a radiationsensitive circuit, an output device, a flame-detector channel comprising a band-pass amplifier and an integrating circuit, means connecting said flame-detector channel between said radiation-sensitive circuit and said output device, an explosion-detector channel responsive only to a steep rise in radiant energy impinging upon said radiationsensitive circuit, and means to connect said explosiondetector channel in shunt with said flame-detector channel. 0
between said radiationsensitive circuit and the. input of the first amplifier of said band-pass amplifying circuit, an output device, an integrating circuit connected between said output device and said amplifying circuit, and a gasfilled tube connected between the output of said first amplifier and said output device and in shunt with part of said band-pass amplifying circuit.
3. A fire and explosion detector comprising: a radiationsensitive circuit including a photoelectric cell, an amplifier tube having an input electrode and an output electrode, a differentiating circuit connected between the radiation-sensitive circuit and the input electrode of said amplifier tube, an output tube, a band-pass amplifier and an integrating circuit connected between the output electrode of said amplifier tube and said output tube, an explosion-detector channel responsive only to a steep rise in radiant energy impinging upon said photocell, and
means to connect said explosiondetector channel in shunt with said band-pass amplifier and said integrating circuit.
4. A fire and explosion detector according to claim 3 wherein said explosion-detector channel comprises a nor- 5 mally nonconductive neon lamp.
References Cited in the file of this patent UNITED STATES PATENTS 10 2,570,280 Roftman Oct. 9, 1951 2,579,884 Thomson et a1 Dec. 25, 1951 2,621,239 Cade Dec. 9, 1952
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US410016A US2762034A (en) | 1954-02-12 | 1954-02-12 | Fire and explosion detection apparatus |
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US410016A US2762034A (en) | 1954-02-12 | 1954-02-12 | Fire and explosion detection apparatus |
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US2762034A true US2762034A (en) | 1956-09-04 |
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US410016A Expired - Lifetime US2762034A (en) | 1954-02-12 | 1954-02-12 | Fire and explosion detection apparatus |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2907012A (en) * | 1955-12-30 | 1959-09-29 | Pitman Duncan | Sofar alarm |
US2919438A (en) * | 1958-01-08 | 1959-12-29 | Honeywell Regulator Co | Condition sensing apparatus |
US2994858A (en) * | 1957-12-13 | 1961-08-01 | William E Coffer | System for signalling failure of refrigeration devices |
US3156908A (en) * | 1961-12-04 | 1964-11-10 | Viking Corp | Flame responsive apparatus |
US3255441A (en) * | 1962-11-30 | 1966-06-07 | Goodwin | Smoke, flame, critical temperature and rate of temperature rise detector |
US3277458A (en) * | 1963-06-26 | 1966-10-04 | Thomas L Greenwood | Condition and condition duration indicator |
US3462652A (en) * | 1964-07-01 | 1969-08-19 | Philips Corp | Radiation-responsive circuit arrangement |
US3613062A (en) * | 1968-02-22 | 1971-10-12 | Memco Ltd | Flame quality and presence monitor for multiburner furnaces |
US4553031A (en) * | 1983-09-06 | 1985-11-12 | Firetek Corporation | Optical fire or explosion detection system and method |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2570280A (en) * | 1951-04-26 | 1951-10-09 | Roffman Eugene | Automatic fire-detecting and extinguishing apparatus |
US2579884A (en) * | 1947-12-11 | 1951-12-25 | Comb Control Corp | Flame failure safeguard |
US2621239A (en) * | 1950-08-22 | 1952-12-09 | Photoswitch Inc | Heat detector for aircraft |
-
1954
- 1954-02-12 US US410016A patent/US2762034A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2579884A (en) * | 1947-12-11 | 1951-12-25 | Comb Control Corp | Flame failure safeguard |
US2621239A (en) * | 1950-08-22 | 1952-12-09 | Photoswitch Inc | Heat detector for aircraft |
US2570280A (en) * | 1951-04-26 | 1951-10-09 | Roffman Eugene | Automatic fire-detecting and extinguishing apparatus |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2907012A (en) * | 1955-12-30 | 1959-09-29 | Pitman Duncan | Sofar alarm |
US2994858A (en) * | 1957-12-13 | 1961-08-01 | William E Coffer | System for signalling failure of refrigeration devices |
US2919438A (en) * | 1958-01-08 | 1959-12-29 | Honeywell Regulator Co | Condition sensing apparatus |
US3156908A (en) * | 1961-12-04 | 1964-11-10 | Viking Corp | Flame responsive apparatus |
US3255441A (en) * | 1962-11-30 | 1966-06-07 | Goodwin | Smoke, flame, critical temperature and rate of temperature rise detector |
US3277458A (en) * | 1963-06-26 | 1966-10-04 | Thomas L Greenwood | Condition and condition duration indicator |
US3462652A (en) * | 1964-07-01 | 1969-08-19 | Philips Corp | Radiation-responsive circuit arrangement |
US3613062A (en) * | 1968-02-22 | 1971-10-12 | Memco Ltd | Flame quality and presence monitor for multiburner furnaces |
US4553031A (en) * | 1983-09-06 | 1985-11-12 | Firetek Corporation | Optical fire or explosion detection system and method |
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