Cargo fire-suppression agent distribution system

Patent metadata

Field	Value
Publication number	US-10238901-B2
Application number	US-201615357714-A
Country	US
Kind code	B2
Filing date	Nov 21, 2016
Priority date	Dec 7, 2012
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

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 cargo fire-suppression agent distribution system comprising:
a fire detector operable to receive a fire-warning signal indicating presence of fire in a cargo compartment of an aircraft, the aircraft receiving the fire-warning signal while the 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 the initial fire-suppression agent in the cargo compartment at the first altitude sufficient to suppress fire for an initial fire-suppression time interval, during which the 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 the re-enforcing fire-suppression agent in the cargo compartment after the time interval elapses during a re-pressurization phase, when a cabin altitude is below a predetermined cabin pressure level (PL) and the 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.

2. The cargo fire-suppression agent distribution system of claim 1 , wherein the first altitude is about 11 km (36,000 feet) equivalent oxygen pressure altitude.

3. The cargo fire-suppression agent distribution system of claim 1 , wherein the second altitude is about 7.6 km (25000 feet) equivalent oxygen pressure altitude.

4. The cargo fire-suppression agent distribution system 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 cargo fire-suppression agent distribution system of claim 1 , wherein the initial fire-suppression time interval is about 5 minutes.

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

7. The cargo fire-suppression agent distribution system 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. The cargo fire-suppression agent distribution system of claim 7 , wherein the active agent comprises at least of one of the group consisting of: HFC-125, Pentafluoroethane (CF3CHF2), Nitrogen, Argon, Helium, aerosolized liquid mist, fire protection fluid (C6F12O), and water.

9. The cargo fire-suppression agent distribution system of claim 1 , 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.

10. The cargo fire-suppression agent distribution system of claim 9 , 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.

11. The cargo fire-suppression agent distribution system of claim 9 , 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.

12. A method for enhancing fire-suppression, comprising:
receiving, by a fire detector of a cargo fire-suppression agent distribution system, a fire-warning signal indicating presence of fire in a cargo compartment of an aircraft, the fire detector receiving the fire-warning signal while the aircraft is at a first altitude;
distributing, by the cargo fire-suppression agent distribution system, an initial fire-suppression agent in the cargo compartment at the first altitude sufficient to suppress fire for an initial fire-suppression time interval, during which the aircraft enters a depressurization phase and flies to a second altitude below the first altitude;
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, by the cargo fire-suppression agent distribution system, a re-enforcing fire-suppression agent in the cargo compartment after the time interval elapses during a re-pressurization phase, when a cabin altitude is below a predetermined cabin pressure level (PL) and the aircraft descends from the second altitude to a landing; and
maintaining, by the cargo fire-suppression agent distribution system, distribution of the re-enforcing fire-suppression agent during a re-enforcing fire-suppression time interval.

13. The method of claim 12 , wherein the first altitude is about 11 km (36,000 feet) equivalent oxygen pressure altitude, and wherein the second altitude is about 7.6 km (25000 feet) equivalent oxygen pressure altitude.

14. The method of claim 12 , wherein the predetermined cabin PL is equivalent to an atmospheric pressure at about 6.1 km (20,000 feet) equivalent oxygen pressure altitude.

15. The method of claim 12 , wherein the initial fire-suppression time interval is about 5 minutes, and wherein the re-enforcing fire-suppression time interval is about 23 minutes.

16. The method of claim 12 , 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.

Assignees

• Boeing Co

Inventors

• Ferguson Douglas E
• Tutson Arthur L

Classifications

• A62C99/0018

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

• A62C37/36

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

• A62C37/04

  with electrically-controlled release · CPC title

• A62C3/08 Primary

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