Fire suppression systems for vehicles

• US 5,052,493 A
• Filed: 05/25/1990
• Issued: 10/01/1991
• Est. Priority Date: 05/27/1989
• Status: Expired due to Fees

• Current Assignee: British Aerospace, Inc.
• Original Assignee: British Aerospace, Inc.
• Inventors: Court, Anthony J. T.
• Primary Examiner(s): Basinger, Sherman
• Assistant Examiner(s): Avila, Stephen P.
• Application Number:
  US07/528,545
• Time in Patent Office: 494 Days
• Field of Search: 169/54, 169/62, 169/5, 169/9, 169/11, 169/14, 169/16, 169/37, 244/129.2, 244/118.5
• US Class Current: 169/9
• CPC Class Codes: A62C 13/70 characterised by means for releasing the pressure gas
• CPC Class Codes: A62C 3/07 in vehicles, e.g. in road vehicles

Abstract

A fire and smoke suppression system suitable for passenger aircraft capable of `surviving` a crash consists of a plurality of individually and independently operable unit (17) each including its own self-contained supply of fire/smoke suppressant, such as water, as well as its own self-contained supply of a pressurizing device, such as CO₂ bottle (23) which, on activation, expels the suppressant under pressure. Each unit (17) is an integrated assembly including a spray head (18) terminating in a nozzle (20) in flow communication with a flexible bag tank (25) containing water and accommodated in a rigid outer shell (24).

Claims

1. An aircraft fire and smoke suppression system, said system comprising a plurality of suppressant fluid spray nozzle assemblies (17) disposed at pre-selected locations within the same enclosure of said aircraft, each of said spray nozzle assemblies (17) including:

its own spray nozzle (20);

its own self-contained supply (25) of suppressant fluid;

its own self-contained supply (23) of fluid pressurizing means; and

co-ordinatable system activating means (22;

     28) capable of activating each said assembly (17) selectably independently of each other said assembly (17) and simultaneously with at least some of the other said assemblies (17);

the arrangement being such that, when activated, each said individual supply (23) of fluid pressurizing means causes said suppressant fluid to be discharged within said enclosure as a dense mist or spray from said spray nozzle(s) (20) under substantially constant pressure such that, in combination, the output of the plurality of spray nozzles (20) defines a fire- and smoke-suppressing blanket for a critical time period for evacuation of the aircraft.

2. The invention according to claim 1 wherein said suppressant fluid is contained within a tank (25) connected to said fluid pressurizing means supply (23) and to said spray nozzle assembly (17).

3. The invention according to claim 1, wherein said suppressant fluid is water.

4. The invention according to claim 1, wherein said tank (25) is a flexible bag contained within a storage tank (24), said flexible bag (25) being connected to said spray nozzle head (18) and the storage tank (24) is connected to said pressurizing means supply (23) such that when activated the space between the wall(s) of said storage tank (24) and said flexible bag (25) is pressurized by said pressurizing means supply (23) to apply a constant discharging pressure on said suppressant fluid.

5. The invention according to claim 1, wherein said self-contained supply of pressurizing means comprises a `one-shot` compressed CO₂ bottle (23) or cartridge.

6. The invention according to claim 1, wherein said activating means comprises at least one of:

electrical signalling means and mechanical actuation means (28).

7. An aircraft fire and smoke suppression system comprising a plurality of water spray nozzle assemblies (17) disposed at preselected locations within a single enclosure of the said aircraft, each of said assemblies (17) including:

a storage tank (24);

a flexible bag (25) contained in the storage tank (24) and permanently containing water;

a spray nozzle head (18) having an outlet communicating with said enclosure;

a connecting duct (26) connecting the interior of the flexible bag (25) with the spray nozzle head (18);

a one-shot container (23) of compressed gas for pressurizing the flexible bag (25);

a delivery tube (27) for delivering compressed gas from said one-shot container (23) to the interior of the flexible bag (25); and

system activating means (22;

     28) effective selectably to activate one of;

any selected one, and any selected group, of said water spray nozzle assemblies (17),

the arrangement being such that in the event of fire within the said enclosure the system remains readily activated such that the selected water spray nozzle assembly(ies) (17) will discharge a dense spray of water at substantially constant pressure to knock down toxic smoke and cool the temperature within said enclosure for a sufficient time to evacuate persons in said enclosure.