Fire and explosion detection and suppression

• US 4,719,973 A
• Filed: 11/25/1986
• Issued: 01/19/1988
• Est. Priority Date: 12/20/1985
• Status: Expired due to Fees

• Current Assignee: Kidde Fire Protection Ltd (Rtx Corporation)
• Original Assignee: Graviner Limited (Carrier Global Corporation)
• Inventors: Allen, Nicholas S., Moore, Peter E.
• Primary Examiner(s): Nase, Jeffrey V.
• Assistant Examiner(s): KANNOFSKY, JAMES
• Application Number:
  US06/934,669
• Time in Patent Office: 420 Days
• Field of Search: 340/578, 340/522, 244/114 R, 244/129.2, 169/60, 169/61, 169/23, 169/46, 169/47
• US Class Current: 169/61
• CPC Class Codes: G08B 17/12 Actuation by presence of radiation or particles, e.g. of infrared radiation or of ions
• CPC Class Codes: G08B 29/188 Data fusion; cooperative systems, e.g. voting among different detectors

Abstract

A fire and explosion detection and suppression system protects a hangar within which may be stored jet aircraft whose engines may be run up particularly in the re-heat mode. Two radiation sensors are mounted within the hangar and detect for at least predetermined amounts of radiation of predetermined and different types (e.g. one sensor may be a UV sensor and the other may be an IR sensor). When they simultaneously detect sufficient radiation, they operate an AND gate. This fires off suppressor units. To prevent false alarms due to radiation emitted by a running jet engine or a jet engine running in re-heat mode, such a running jet engine is sensed by a transducer responsive to the emitted acoustic or vibrational energy. This blocks the AND gate.

Claims

1. A fire and explosion detection system for detecting fire or explosion within an area to be protected, comprising

radiation detection means operative to produce an alarm signal in response to the detection of electromagnetic radiation from a source within the said area and thereby indicative of a fire or explosion in the said area,

non-radiation-responsive transducer means operative to detect the existence within the said area of a predetermined non-radiation parameter and thereby indicating that the source of electromagnetic radiation to which the radiation detection means is responsive is one in response to which no alarm signal is required, and

inhibit means responsive to the non-radiation-responsive transducer means for blocking such alarm signal.

2. A system according to claim 1, in which

the radiation detection means comprises a plurality of radiation sensors each producing a respective output signal in response to detection of predetermined radiation, and including

circuit means responsive to the outputs of the radiation sensors to produce the said alarm signal.

3. A system according to claim 2, in which

the circuit means includes a coincidence gate for producing the said alarm signal in response to simultaneous receipt of the output signals from the radiation sensors, and

the inhibit means comprises means for blocking such response of the coincidence gate.

4. A system according to claim 2, in which

the circuit means comprises logic means for producing the said alarm signal in response to simultaneous receipt of the output signals from a predetermined selection of the radiation sensors, and

the inhibit means comprises means for blocking such response of the logic means.

5. A system according to claim 1, in which the said source of electromagnetic radiation which is required not to produce an alarm signal is a running jet engine of a jet aircraft.

6. A system according to claim 5, in which the predetermined non-radiation parameter to which the non-radiation-responsive transducer means is responsive is the acoustic or vibrational energy emitted by the running jet engine.

7. A fire and explosion detection and suppression system, for protecting an area in which jet aircraft may be stored, comprising

radiation detection means for detecting electromagnetic radiation arising from such fires and explosions within the said area and for producing a respective alarm signal,

suppression means within the area and responsive to the alarm signal to discharge fire and explosion suppressant into the area, and

transducer means responsive to the acoustic or vibrational energy emitted by a running jet engine for inhibiting the production of the said alarm signal.

8. A system according to claim 7, in which

there are a plurality of such radiation detection means each capable of producing a said alarm signal, and

the non-radiation-responsive transducer means is connected to block the production of the alarm signal by at least one but not all of the said radiation detection means.

9. A system according to claim 7, in which

the radiation detection means comprises a plurality of radiation sensors each producing a respective electrical output in response to receipt of radiation of a predetermined type, and including

respective circuit means connected to receive the outputs from each plurality of sensors and to produce the said alarm signal in response thereto.

10. A fire and explosion detection and suppression method, for protecting an area in which jet aircraft may be stored, comprising the steps of

detecting electromagnetic radiation arising from such fires and explosions within the said area and for producing a respective alarm signal.

responding to the said alarm signal by discharging fire and explosion suppressant into the area, and

responding to the acoustic or vibrational energy emitted from a running jet engine by inhibiting the production of the said alarm signal.