Suppressing a fire condition within a cargo container

Patent metadata

Field	Value
Publication number	US-9555271-B2
Application number	US-201213458575-A
Country	US
Kind code	B2
Filing date	Apr 27, 2012
Priority date	Jun 17, 2011
Publication date	Jan 31, 2017
Grant date	Jan 31, 2017

Abstract

Various concepts are provided for suppressing a fire condition in an aircraft. In one embodiment, the presence of a fire condition in an aircraft is detected. After such a detection, extinguishing agents can be dispensed and/or certain areas of the aircraft can be depressurized.

First claim

The invention claimed is:

1. A method for suppressing a fire condition in an aircraft, the method comprising the steps of:
detecting a presence of a fire condition in one or more areas of an aircraft each area having a corresponding initial pressure;
after detecting the presence of the fire condition in the one or more areas of the aircraft, depressurizing the one or more areas of the aircraft from the corresponding initial pressures in accordance with a depressurizing procedure for the aircraft, wherein depressurizing the one or more areas of the aircraft reduces the amount of oxygen in the one or more areas of the aircraft;
after depressurizing the one or more areas of the aircraft, releasing a first rapid discharge of an extinguishing agent in the one or more areas of the aircraft; and
after releasing the rapid discharge of the extinguishing agent, releasing a second controlled discharge of the extinguishing agent in the one or more areas of the aircraft;
wherein the extinguishing agent comprises a liquefied gas or a solid compound that generates an aerosol containing potassium compounds.

2. The method of claim 1 , wherein the second controlled discharge of extinguishing agent is released once the aircraft has started a descent to land.

3. A method for suppressing a fire condition in an aircraft, the method comprising the steps of:
detecting a presence of a fire condition in one or more areas of an aircraft;
after detecting the presence of the fire condition in the one or more areas of the aircraft, releasing a first discharge of an extinguishing agent in the one or more areas of the aircraft;
after releasing the first discharge of the extinguishing agent, depressurizing the one or more areas of the aircraft in accordance with a depressurizing procedure for the aircraft, wherein depressurizing the one or more areas of the aircraft reduces the amount of oxygen in the one or more areas of the aircraft; and
after depressurizing the one or more areas of the aircraft, releasing a second discharge of the extinguishing agent in the one or more areas of the aircraft;
wherein the extinguishing agent comprises a liquefied gas or a solid compound that generates an aerosol containing potassium compounds.

4. The method of claim 3 , wherein the first discharge of the extinguishing agent comprises a rapid discharge of the extinguishing agent in the one or more areas of the aircraft.

5. The method of claim 4 , wherein the second discharge of the extinguishing agent comprises a controlled discharge of the extinguishing agent in the one or more areas of the aircraft.

Assignees

• Ransom Jr John H
• United parcel service america inc

Inventors

• Ransom Jr John H

Classifications

• A62C2/24

  Operating or controlling mechanisms {(emergency operation of doors and windows E05F1/002, E05F15/72)} · CPC title

• A62C2/246

  having non-mechanical actuators · CPC title

• A62C2/248

  pneumatic · CPC title

• A62C2/247

  electric · CPC title

• A62C3/00

  Fire prevention, containment or extinguishing specially adapted for particular objects or places ({in oil wells E21B29/08, A62C35/00; in mines or tunnels E21F5/00} ; for nuclear reactors G21C9/04) · CPC title