Cargo fire-suppression agent distribution system

Patent metadata

Field	Value
Publication number	US-9526931-B2
Application number	US-201213707616-A
Country	US
Kind code	B2
Filing date	Dec 7, 2012
Priority date	Dec 7, 2012
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

A cargo-fire-suppression agent distribution system and methods are presented. A fire-warning signal indicating presence of fire in a cargo compartment onboard a class E cargo aircraft at a first altitude is received. An initial fire-suppression agent is distributed in the cargo compartment at the first altitude sufficient to suppress fire for an initial fire suppression time interval during a depressurization phase during which the class E cargo aircraft flies to a second altitude below the first altitude. A re-enforcing fire-suppression agent is distributed in the cargo compartment during a re-pressurization phase when a cabin altitude is below a predetermined cabin pressure level (PL) during which the class E cargo aircraft flies from the second altitude to a landing, after the initial fire-suppression time interval elapses. The re-enforcing fire-suppression agent distribution is maintained during a re-enforcing fire-suppression time interval.

First claim

The invention claimed is:

1. A method for enhancing fire-suppression for a class E cargo aircraft, comprising:
receiving a fire-warning signal indicating presence of fire in a cargo compartment onboard a class E cargo aircraft, the class E cargo aircraft receiving the fire-warning signal while the class E cargo aircraft is at a first altitude;
distributing an initial fire-suppression agent in the cargo compartment for an initial fire-suppression time interval, the initial fire-suppression time interval occurring during a depressurization phase during which the class E cargo aircraft flies to a second altitude below the first altitude and ending when the class E cargo aircraft reaches an oxygen level low enough to maintain fire-suppression;
blocking distribution of any fire-suppression agent for a time interval in response to a determination that the aircraft has reached a predetermined low oxygen level sufficient to maintain fire-suppression, wherein the time interval follows the initial fire-suppression time interval;
distributing a re-enforcing fire-suppression agent in the cargo compartment during a re-pressurization phase when a cabin altitude is below a predetermined cabin pressure level (PL) during which the class E cargo aircraft flies from the second altitude to a landing, after the initial fire-suppression time interval elapses; and
maintaining distribution of the re-enforcing fire-suppression agent during a re-enforcing fire-suppression time interval.

2. The method of claim 1 , wherein the first altitude is about 11 km (36,000 feet) equivalent oxygen pressure altitude.

3. The method of claim 1 , wherein the second altitude is about 7.6 km (25000 feet) equivalent oxygen pressure altitude.

4. The method of claim 1 , wherein the predetermined cabin PL is equivalent to an atmospheric pressure at about 6.1 km (20,000 feet) equivalent oxygen pressure altitude.

5. The method of claim 1 , wherein the initial fire-suppression time interval is about 5 minutes.

6. The method of claim 1 , wherein the re-enforcing fire suppression time interval is about 23 minutes.

7. The method of claim 1 , wherein the initial fire-suppression agent and the re-enforcing fire-suppression agent each comprises at least one of the group consisting of: an active agent, and Halon.

8. A cargo fire-suppression agent distribution system onboard a class E cargo aircraft comprising:
a fire detector operable to receive a fire-warning signal indicating presence of fire in a cargo compartment, the class E cargo aircraft receiving the fire-warning signal while the class E cargo aircraft is at a first altitude;
a fire-suppression agent time determination module operable to activate an initial fire suppression agent and a re-enforcing fire-suppression agent at a first activation time and a second activation time respectively; and
a controller operable to:
distribute an initial fire-suppression agent in the cargo compartment at the first altitude sufficient to suppress fire for an initial fire-suppression time interval, the initial fire-suppression time interval ending when the class E cargo aircraft reaches an oxygen level low enough to maintain fire-suppression and during which the class E cargo aircraft enters a depressurization phase and flies to a second altitude below the first altitude;
block distribution of any fire-suppression agent for a time interval in response to a determination that the aircraft has reached a predetermined low oxygen level sufficient to maintain fire-suppression, wherein the time interval follows the initial fire-suppression time interval;
distribute a re-enforcing fire-suppression agent in the cargo compartment after the initial fire-suppression time interval elapses during a re-pressurization phase, when a cabin altitude is below a predetermined cabin pressure level (PL) and the class E cargo aircraft descends from the second altitude to a landing; and
maintain distribution of the re-enforcing fire-suppression agent during a re-enforcing fire-suppression time interval.

9. The system of claim 8 , wherein the first altitude is about 11 km (36,000 feet) equivalent oxygen pressure altitude.

10. The system of claim 8 , wherein the second altitude is about 7.6 km (25000 feet) equivalent oxygen pressure altitude.

11. The system of claim 8 , wherein the predetermined cabin PL is equivalent to an atmospheric pressure at about 6.1 km (20,000 feet) equivalent oxygen pressure altitude.

12. The system of claim 8 , wherein the initial fire-suppression time interval is about 5 minutes.

13. The system of claim 8 , wherein the re-enforcing fire suppression time interval is about 23 minutes.

14. The system of claim 8 , wherein the initial fire-suppression agent comprises at least one of the group consisting of: an active agent, and Halon.

15. The system of claim 14 , wherein the active agent comprises at least one of the group consisting of: HFC-125, Pentafluoroethane (CF3CHF2), and Halon.

16. The system of claim 8 , wherein the initial fire-suppression agent and the re-enforcing fire-suppression agent are supplied by a fire-suppression agent supply source coupled to a vehicle ducting.

17. The system to claim 16 , wherein the fire-suppression agent supply source comprises at least one member selected from the group consisting of: a metered system, a descent storage bottle, and a dump bottle.

18. The system of claim 16 , wherein the fire-suppression agent supply source comprises at least one member selected from the group consisting of: a storage bottle, an On-Board Inert Gas Generation System (OBIGGS), an HFC-125 supply source, a Pentafluoroethane (CF3CHF2) supply source, a Nitrogen supply source, an Argon supply source, a Helium supply source, an aerosolized liquid mist supply source, an FK 5-1-12 (C6F12O) supply source, a water supply source, and a Halon supply source.

Assignees

• Boeing Co

Inventors

• Ferguson Douglas E
• Tutson Arthur L

Classifications

• A62C37/36

  an actuating signal being generated by a sensor separate from an outlet device · CPC title

• A62C99/0018

  using gases or vapours that do not support combustion, e.g. steam, carbon dioxide · CPC title

• A62C37/04

  with electrically-controlled release · CPC title

• A62C3/08 Primary

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