US3044050A - Fire detection system - Google Patents

Fire detection system Download PDF

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Publication number
US3044050A
US3044050A US834263A US83426359A US3044050A US 3044050 A US3044050 A US 3044050A US 834263 A US834263 A US 834263A US 83426359 A US83426359 A US 83426359A US 3044050 A US3044050 A US 3044050A
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Prior art keywords
cable
fire detection
cables
detection system
alarm
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US834263A
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Andre T Abromaitis
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McGraw Edison Co
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McGraw Edison Co
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    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62CFIRE-FIGHTING
    • A62C3/00Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/07Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles
    • A62C3/08Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles in aircraft
    • GPHYSICS
    • G08SIGNALLING
    • G08BSIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B17/00Fire alarms; Alarms responsive to explosion
    • G08B17/06Electric actuation of the alarm, e.g. using a thermally-operated switch

Definitions

  • the present fire detection system uses typically sensing devices of cable form such as are described and claimed in the Kelly et al. Patent No. 2,740,874, issued April 3, 1956.
  • Such fire detector cables have a center wire and a spaced,
  • the fire detection system will provide an alarm when any portion of such cable is overheated.
  • the advantage of using a sensingdevice of cable form is that the cable can be disposed throughout the whole area to be monitored for fire.
  • This form of fire detection system is now commonly used on aircraft for detecting engine oil fires. In this application the system must. perform with utmost reliability not only in giving a positive alarm when fire occurs but also in having maximum freedom from false alarm, notwithstandingthat the conditions of useare very severe.
  • the present invention is designed to reduce throughout the areabeing monitored for fire but with the cables connected serially to form a single unitary sensing bridge 10 having one branch with fixed impedance arms 11 and 12 and a second branch with one'fixed impedance arm 13 and a variable resistance arm 14 constituting the sensing means of the fire detection system.
  • the arm 14 comprises two temperatureresponsive, serially connected, resistance type sensing devices designated in the circuit simply as variable resistors 15 and 16.
  • the temperature sensitive resistors are located along each other in an area to be monitored represented by the dash-dot enclosure 17.
  • the arm '12 opposite that of the sensing means is a'resistor which determines the state of balance of the bridge when the sensing means is at a predetermined operate temperature.
  • the arms 11 and 13 are preferably resistors as shown but could be reactive impedances if an A.C. source of potential were employed.
  • the present bridge is operated from a D.C. supply derived from the 115 volt, 400 c.p.s.
  • D.C. supply may be ungrounded to between the arms of one branch to the junction point between the arms of the other branch is a receiving device 24 controlling through a line 25 an alarm or other indicating device 26, as diagrammatically shown.
  • the receiving device may compise simply a sensitive relay or it may inelude also a magnetic or transistor amplifier permitting device.
  • the invention is in using two I of such parallel disposed, electrically seriallyconnected cables as a'single arm of a Wheatstone bridge which has a receiving device diagonally connected thereto with the bridge adjusted to provide an alarm or other indication when the bridge is in a balanced or null condition.
  • An object of the invention is therefore to provide an improved fire detection system which has the utmost in re liability adapted to 'rneet the high standards required of fire detection systems for aircraft.
  • a still further object is to provide a fire detection system of improved reliability having aminimum complication over the prior forms of fire detection systems using single fire detector cables.
  • the receiving device may be set to operate when the bridge is in a predetermined state of unbalance,.but'preferably in order to reduce sensitivity of the system to variations in the voltage supply the bridge is adjusted so that it will be substantially balanced at the operate temperature.
  • the receiving device is therefore one which will provide an alarm or other indication when the control current in the is shown in more detail as comprising respective fire detector cables 27 and 28 of the resistance type described in the Kelly et al. PatentNo. 2,740,874 beforementioned.
  • cable 27 has a flexible metallic sheath 27a,
  • Such cables have a negative temperature coefiicient of resistance causing them to have a high resistance between the center wire and sheath at low temperatures and a sharply decreasing resistance as any portion of the cable is heated to a predetermined elevated temperature, the resistance being typically 100 ohms or less when the heating is to an overheat or flame tempera ture.
  • the cables are mounted along-side each other in the space 17 being monitored. In applications for detecting engine oilfires on aircraft, the cables are mounted on thefire wall behind the engines with ground connection ,of' the sheaths to the airplane structure as indicated at 23.
  • the cables 27 and 28 have-center wire terminals at each end, which are normally intercom nected through respective single-pole double-throw test switches. 29 and 30.
  • One end terminal of each cable has a permanent connection to thebridge sothat the conductive path of the sensing arm.
  • I4 is from center wire to grounded sheath of one cable and from grounded sheath to center'wire of the other cable.
  • the permanently con nected end terminal of each cable is connected also toa j Patented July 10, 1962 v aticn.
  • the receiving device is operated to give a false alarm. 'It is especially important in aircraft fire detection systems to avoid ever, giving any false alarm.
  • the test means has the following'operationz normal operation is indicated when upon pressing'either test switch no alarm is givenand upon pressing both test switches at the same time an alarm is given.
  • a shortcircuit condition is indicated in one cable'or its circuitry when upon pressing the test switch of the other cable an alarm is given.
  • An open circuit condition is indicated when upon pressing both test switches at thesame time no alarm is given.
  • a fire detection system comprising a pair of fire detector cables each having a pair of spaced apart conductors separated by a temperature-responsive resistive material which is essentially an insulator at room temperature and a conductor at a predetermined elevated temperature indicative of fire, said cables having resistances which vary continuously as the temperature changes progressively from said room temperature to said pretioned alongside each other and exposed equally to overheat conditions in the space being monitored, an electrical bridge comprising two parallelconnected' branches of which one branch comprises two fixed impedance arms serially connected and the other branch comprises a third fixed impedance arm serially connected-with a fourth arm including said cables electrically serially connected via the centerwire and sheath of one cable and the sheath and center wire of the other cable in the sequence here named, and a receiving device connected between said branches dia gonally of said bridge for providing an indication when a source of voltage is applied across said branches and a portion of each of said cables is heated to said predetermined elevated temperature.
  • the fire detection system set forth in claim 1 including an underground source of DC. potential connected across said branches, and a connection between the sheaths of said cables connected to ground.

Description

July 10, 1962 A. T. ABROMAITIS FIRE DETECTION SYSTEM Filed Aug. 17, 1959 INVENTOR. ANDRE "r. ABROMA rr IS AGENJT;
United States Patent This'invention relates to fire detection systemsof the type using temperature-responsive resistance-variable sensing devices, and more particularly it relates to an improved form of such system wherein two of such sensing devices are used in a novel manner in the space being monitored to provide greater reliability in the operation of the system.
The present fire detection system uses typically sensing devices of cable form such as are described and claimed in the Kelly et al. Patent No. 2,740,874, issued April 3, 1956. Such fire detector cables have a center wire and a spaced,
metallic sheath with an intervening semiconductive material which has a negative temperature coeflicientof resistance. The fire detection system will provide an alarm when any portion of such cable is overheated. The advantage of using a sensingdevice of cable form is that the cable can be disposed throughout the whole area to be monitored for fire. This form of fire detection system is now commonly used on aircraft for detecting engine oil fires. In this application the system must. perform with utmost reliability not only in giving a positive alarm when fire occurs but also in having maximum freedom from false alarm, notwithstandingthat the conditions of useare very severe.
It has been found from experience that'usually when failure or false alarmsoccur it is because ofan open or short-circuit condition in the sensing cables or associated circuitry arising from the heavyvibration and varying weather and temperature conditions to which the cables are exposed. The present invention is designed to reduce throughout the areabeing monitored for fire but with the cables connected serially to form a single unitary sensing bridge 10 having one branch with fixed impedance arms 11 and 12 and a second branch with one'fixed impedance arm 13 and a variable resistance arm 14 constituting the sensing means of the fire detection system. In accordance with the invention the arm 14 comprises two temperatureresponsive, serially connected, resistance type sensing devices designated in the circuit simply as variable resistors 15 and 16. These temperature sensitive resistors are located along each other in an area to be monitored represented by the dash-dot enclosure 17. The arm '12 opposite that of the sensing means is a'resistor which determines the state of balance of the bridge when the sensing means is at a predetermined operate temperature. The arms 11 and 13 are preferably resistors as shown but could be reactive impedances if an A.C. source of potential were employed. Preferably, the present bridge is operated from a D.C. supply derived from the 115 volt, 400 c.p.s. source S as typically provided on aircraft This source is connected through a transformer 18 having a secondary winding with a center tap 19 forming one terminal of theD.C.' supply to the bridge, the secondary winding being connected through respective half wave rectifiers 20 and 21 to a junction 22 forming the other terminal of the D.C. supply. Such D.C. supplymay be ungrounded to between the arms of one branch to the junction point between the arms of the other branch is a receiving device 24 controlling through a line 25 an alarm or other indicating device 26, as diagrammatically shown. The receiving device may compise simply a sensitive relay or it may inelude also a magnetic or transistor amplifier permitting device. More particularly, the invention is in using two I of such parallel disposed, electrically seriallyconnected cables as a'single arm of a Wheatstone bridge which has a receiving device diagonally connected thereto with the bridge adjusted to provide an alarm or other indication when the bridge is in a balanced or null condition. y
An object of the invention is therefore to provide an improved fire detection system which has the utmost in re liability adapted to 'rneet the high standards required of fire detection systems for aircraft.
' \A further object is to. provide such improved system which can be easily checked for operability both as to short-and open-circuits in the sensing devices and associated circuits. I
, A still further object is to providea fire detection system of improved reliability having aminimum complication over the prior forms of fire detection systems using single fire detector cables.
the use of a less sensitive and more rugged relay. The receiving device may be set to operate when the bridge is in a predetermined state of unbalance,.but'preferably in order to reduce sensitivity of the system to variations in the voltage supply the bridge is adjusted so that it will be substantially balanced at the operate temperature. The receiving device is therefore one which will provide an alarm or other indication when the control current in the is shown in more detail as comprising respective fire detector cables 27 and 28 of the resistance type described in the Kelly et al. PatentNo. 2,740,874 beforementioned.
For example, cable 27 has a flexible metallic sheath 27a,
a center wire 27b running the length thereof andan intervening' semi-conductive material 270 such as of a manganese oxide. Such cables have a negative temperature coefiicient of resistance causing them to have a high resistance between the center wire and sheath at low temperatures and a sharply decreasing resistance as any portion of the cable is heated to a predetermined elevated temperature, the resistance being typically 100 ohms or less when the heating is to an overheat or flame tempera ture. The cables are mounted along-side each other in the space 17 being monitored. In applications for detecting engine oilfires on aircraft, the cables are mounted on thefire wall behind the engines with ground connection ,of' the sheaths to the airplane structure as indicated at 23. To facilitate testing, the cables 27 and 28 have-center wire terminals at each end, which are normally intercom nected through respective single-pole double-throw test switches. 29 and 30. One end terminal of each cable has a permanent connection to thebridge sothat the conductive path of the sensing arm. I4 is from center wire to grounded sheath of one cable and from grounded sheath to center'wire of the other cable. The permanently con nected end terminal of each cable is connected also toa j Patented July 10, 1962 v aticn.
far end terminal from the end terminal connected directly to the bridge, and connects the far end terminal to ground.
If a short circuit develops in the single cable systems as heretofore used, the receiving device is operated to give a false alarm. 'It is especially important in aircraft fire detection systems to avoid ever, giving any false alarm.
In the present dual cable system a short-circuit in either cable will not give a false alarm and will not even render the system inoperable but, has. only the effect of reducing slightly the operate temperature at which an alarm is given, the amount by which the operate temperature is so reduced being typically about 40 F. for the type of cable herein particularly considered. The advantage of the present invention resides in the probability that both cables will not likely develop a short-circuit at the same time, that such fault in either cable will not give rise to a false alarm and that such fault in either cable can be easily detected by the test means described.
Because of the 'dual connection made to each cable an I open circuit in either cable, such as a break in the center wire or even the whole cable, or a break in the circuit connection at either end of the cable, will not give any false alarm or atfect the operation of the system. However, once any such open circuit has developed at one point in either cable the system would be seriously impaired were such open circuit to develop at still another a point. It is therefore important to be able to detect also by the present test means whenever any open circuit condition has developed.
The test means has the following'operationz normal operation is indicated when upon pressing'either test switch no alarm is givenand upon pressing both test switches at the same time an alarm is given. A shortcircuit condition is indicated in one cable'or its circuitry when upon pressing the test switch of the other cable an alarm is given. An open circuit condition is indicated when upon pressing both test switches at thesame time no alarm is given.
From the foregoing description it will be apparent that I have provided a fire detection system which will not likely ever produce a false alarm from the usual faults which may occur; and further, the occurrence of any such usual fault can be detected readily by a simple test oper- Moreover, the invention is carried out with a 4 minimum complication over the prior fire direction systems.
The embodiment of my invention herein particularly shown and described is intended to be illustrative-and not limitative of the invention since the same is subject to changes and modifications without departure from the scope of my invention, which I endeavor to express according to the following claims.
I claim:
1. A fire detection system comprising a pair of fire detector cables each having a pair of spaced apart conductors separated by a temperature-responsive resistive material which is essentially an insulator at room temperature and a conductor at a predetermined elevated temperature indicative of fire, said cables having resistances which vary continuously as the temperature changes progressively from said room temperature to said pretioned alongside each other and exposed equally to overheat conditions in the space being monitored, an electrical bridge comprising two parallelconnected' branches of which one branch comprises two fixed impedance arms serially connected and the other branch comprises a third fixed impedance arm serially connected-with a fourth arm including said cables electrically serially connected via the centerwire and sheath of one cable and the sheath and center wire of the other cable in the sequence here named, and a receiving device connected between said branches dia gonally of said bridge for providing an indication when a source of voltage is applied across said branches and a portion of each of said cables is heated to said predetermined elevated temperature.
2. The fire detection system set forth in claim 1 including an underground source of DC. potential connected across said branches, and a connection between the sheaths of said cables connected to ground.
References Cited in the file of this patent UNITED STATES PATENTS y Poitras Mar. 1, 1960
US834263A 1959-08-17 1959-08-17 Fire detection system Expired - Lifetime US3044050A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3175206A (en) * 1964-07-14 1965-03-23 Lindberg Fire detector with integrity-testing device
US3340527A (en) * 1965-01-13 1967-09-05 Technical Marketing Associates Condition monitoring system
US3429183A (en) * 1966-07-14 1969-02-25 John E Lindberg Temperature averaging system
EP0128601A1 (en) * 1983-05-10 1984-12-19 Leuven Research & Development Temperature monitoring device
US5134248A (en) * 1990-08-15 1992-07-28 Advanced Temperature Devices, Inc. Thin film flexible electrical connector
US9472078B2 (en) * 2015-01-05 2016-10-18 Honeywell International Inc. Method and apparatus for integration of electrical fire sensor with fire panel

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1977121A (en) * 1926-09-11 1934-10-16 Ericsson Telefon Ab L M Fire alarm system
US2028653A (en) * 1930-05-07 1936-01-21 Ericsson Telefon Ab L M Fire alarm system
US2059510A (en) * 1932-12-01 1936-11-03 Ekman Olof Ingemar Harald Automatic alarm system
US2737642A (en) * 1954-01-07 1956-03-06 Arthur J Waldorf Supervised fire detection and alarm system
US2740874A (en) * 1951-08-15 1956-04-03 Edison Inc Thomas A Electric fire-detector cable
US2764659A (en) * 1955-06-27 1956-09-25 Edison Inc Thomas A Resistance type fire detector cable
US2781505A (en) * 1952-10-18 1957-02-12 Specialties Dev Corp Temperature responsive system
US2871466A (en) * 1955-12-30 1959-01-27 American District Telegraph Co Automatic fire alarm system
US2901740A (en) * 1956-11-23 1959-08-25 Specialties Dev Corp Electrical network automatically responsive to a change in condition
US2906928A (en) * 1955-09-26 1959-09-29 Specialties Dev Corp Electrical network automatically responsive to a rate of change of a condition and a predetermined change of the condition
US2927309A (en) * 1953-11-02 1960-03-01 Edward J Poitras Liquid-vapor phase differential fire and overheat detector and control

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1977121A (en) * 1926-09-11 1934-10-16 Ericsson Telefon Ab L M Fire alarm system
US2028653A (en) * 1930-05-07 1936-01-21 Ericsson Telefon Ab L M Fire alarm system
US2059510A (en) * 1932-12-01 1936-11-03 Ekman Olof Ingemar Harald Automatic alarm system
US2740874A (en) * 1951-08-15 1956-04-03 Edison Inc Thomas A Electric fire-detector cable
US2781505A (en) * 1952-10-18 1957-02-12 Specialties Dev Corp Temperature responsive system
US2927309A (en) * 1953-11-02 1960-03-01 Edward J Poitras Liquid-vapor phase differential fire and overheat detector and control
US2737642A (en) * 1954-01-07 1956-03-06 Arthur J Waldorf Supervised fire detection and alarm system
US2764659A (en) * 1955-06-27 1956-09-25 Edison Inc Thomas A Resistance type fire detector cable
US2906928A (en) * 1955-09-26 1959-09-29 Specialties Dev Corp Electrical network automatically responsive to a rate of change of a condition and a predetermined change of the condition
US2871466A (en) * 1955-12-30 1959-01-27 American District Telegraph Co Automatic fire alarm system
US2901740A (en) * 1956-11-23 1959-08-25 Specialties Dev Corp Electrical network automatically responsive to a change in condition

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3175206A (en) * 1964-07-14 1965-03-23 Lindberg Fire detector with integrity-testing device
US3340527A (en) * 1965-01-13 1967-09-05 Technical Marketing Associates Condition monitoring system
US3429183A (en) * 1966-07-14 1969-02-25 John E Lindberg Temperature averaging system
EP0128601A1 (en) * 1983-05-10 1984-12-19 Leuven Research & Development Temperature monitoring device
US5134248A (en) * 1990-08-15 1992-07-28 Advanced Temperature Devices, Inc. Thin film flexible electrical connector
US9472078B2 (en) * 2015-01-05 2016-10-18 Honeywell International Inc. Method and apparatus for integration of electrical fire sensor with fire panel

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