Method and system for fire prevention and/or fire fighting

Patent metadata

Field	Value
Publication number	US-9861844-B2
Application number	US-201213606621-A
Country	US
Kind code	B2
Filing date	Sep 7, 2012
Priority date	Sep 9, 2011
Publication date	Jan 9, 2018
Grant date	Jan 9, 2018

Abstract

A method for fire prevention and/or fire fighting on board an aircraft comprises the steps detecting a fire event, leading an extinguishant to a fire source through a cooling-system piping system ( 12 ) which serves, in the normal operation of the aircraft, to supply a refrigerant to a cooling station ( 14 a , 14 b ) and/or discharge a refrigerant from a cooling station ( 14 a , 14 b ), and flooding the fire source with the extinguishant.

First claim

The invention claimed is:

1. A method for fire prevention and/or fire fighting on board an aircraft, comprising:
detecting a fire event,
leading an extinguishant to a fire source through a cooling-system piping system,
supplying a refrigerant to a cooling station and/or discharging the refrigerant from a cooling station via the cooling-system piping system before the extinguishant is led through the cooling-system piping system in the normal operation of the aircraft,
draining the refrigerant from the cooling-system piping system into a storage tank before the extinguishant is led through the cooling-system piping system to the fire source, and
wherein an amount of the refrigerant is used as the extinguishant.

2. The method according to claim 1 ,
wherein the extinguishant is led through the cooling system piping system together with the refrigerant led through the cooling-system piping system in the normal operation of the aircraft, and the fire source is flooded with a mixture of extinguishant and refrigerant led through the cooling-system piping system in the normal operation of the aircraft.

3. The method according to claim 1 ,
wherein the refrigerant led through the cooling-system piping system in the normal operation of the aircraft is used as propellant in order to convey the extinguishant through the cooling-system piping system to the fire source.

4. The method according to claim 1 ,
wherein the refrigerant led through the cooling-system piping system in the normal operation of the aircraft is utilised as extinguishant in a fire event.

5. The method according to claim 1 ,
wherein a two-phase refrigerant, in particular CO2, is employed as the refrigerant led through the cooling-system piping system in the normal operation of the aircraft.

6. The method according to claim 1 ,
wherein the flooding of the fire source with extinguishant takes place at an interval or a plurality of intervals.

7. A system for fire prevention and/or fire fighting on board an aircraft, having:
a detection device configured to detect a fire event,
a cooling-system piping system which is configured to, in the normal operation of the aircraft, (a) supply a refrigerant to a cooling station and/or discharge a refrigerant from a cooling station, and (b) lead an extinguishant to a fire source in response to the detection device detecting the fire event, and
a supply device configured to supply the cooling-piping system with the extinguishant,
a drain device including a valve to drain the refrigerant, that is led through the cooling-system piping system in the normal operation of the aircraft, from the cooling-system piping system into a storage tank, and
a controller including a computer readable medium having instructions for causing a computer to execute a method to control the valve of the drain device to drain the refrigerant from the cooling-system piping system before the extinguishant is led through the cooling-system piping system to the fire source
wherein an amount of the refrigerant is used as the extinguishant.

8. The system according to claim 7 ,
wherein the cooling-system piping system is configured to lead the extinguishant, together with the refrigerant led through the cooling-system piping system in the normal operation of the aircraft, to the fire source, and in that the device for flooding the fire source with the extinguishant is configured to flood the fire source with a mixture of extinguishant and refrigerant led through the cooling-system piping system in the normal operation of the aircraft.

9. The system according to claim 7 ,
wherein the cooling-system piping system is configured to use the refrigerant led through the cooling-system piping system in the normal operation of the aircraft as propellant in order to convey the extinguishant through the cooling-system piping system to the fire source.

10. The system according to claim 7 ,
wherein the system is configured to utilise the refrigerant led through the cooling-system piping system in the normal operation of the aircraft as extinguishant in a fire event.

11. The system according to claim 7 ,
wherein a two-phase refrigerant, in particular CO2, is employed as the refrigerant led through the cooling-system piping system in the normal operation of the aircraft.

12. The system according to claim 7 ,
wherein the device for flooding the fire source with the extinguishant is structured to flood the fire source with extinguishant at an interval or a plurality of intervals.

13. The system according to claim 7 ,
further comprising a control system which is configured to control the operation of the system for fire prevention and/or fire fighting on board an aircraft in dependence on signals characteristic of the seriousness and the other nature of the fire event and/or in dependence on data on the nature of the fire.

14. The method according to claim 1 ,
wherein the amount of the refrigerant used as extinguishant is led through the cooling-system piping in the normal operation of the aircraft.

15. The system according to claim 7 ,
wherein the amount of the refrigerant used as extinguishant is led through the cooling-system piping in the normal operation of the aircraft.

16. A method for fire prevention and/or fire fighting on board an aircraft, comprising:
detecting a fire event,
leading an extinguishant to a fire source from a storage tank through a cooling-system piping system, which serves, in the normal operation of the aircraft, to supply a refrigerant to a cooling station and/or discharge the refrigerant from a cooling station,
if an amount of extinguishant in the storage tank is insufficient, opening a shutoff valve assigned to a reservoir, such that the reservoir supplies extinguishant to the cooling system piping system,
flooding the fire source with the extinguishant,
wherein an amount of the refrigerant is used as the extinguishant.

Assignees

• Sieme Martin
• Piesker Markus
• Airbus Operations Gmbh

Inventors

• Sieme Martin
• Piesker Markus

Classifications

• A62C35/68

  Details, e.g. of pipes or valve systems (valves in general F16K) · CPC title

• A62C5/008

  for producing other mixtures of different gases or vapours, water and chemicals, e.g. water and wetting agents, water and gases · CPC title

• A62C3/08 Primary

  in aircraft {(A62C3/0207 takes precedence)} · CPC title