Aircraft fire protection system

Fire extinguishers – Special applications – For vehicles

Patent

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2441292, A62C 308

Patent

active

050406116

ABSTRACT:
An aircraft fire protection system which includes a plurality of water spray nozzles spaced along a plurality of longitudinal conduits all cross-connected by a plurality of transverse conduits, with "choking" type flow restrictors spaced between groups of spray nozzles to limit flow following conduit rupture. Conduits are connected to the aircraft on-board water supply system via a pump and non-return valve in series and, additionally or alternately, a plurality of externally mounted self-sealing couplings are interconnected to the conduits, one of which couplings should be accessible to fire-fighting personnel for fire tender hose hookup regardless of aircraft orientation and attitude. A two-way flow restrictor includes a housing with a captured ball valve element with flutes by-passing opposing seating shoulders for the ball to provide two predetermined "choked" flow rates for normal and reverse flow modes.

REFERENCES:
patent: 1854220 (1932-04-01), Pollard
patent: 1866008 (1932-07-01), Burke, Jr.
patent: 2560091 (1951-07-01), Davis
patent: 2938687 (1960-05-01), Krapf, Jr.
patent: 3783946 (1974-01-01), Petrinec et al.
patent: 4347901 (1982-09-01), Wilhoit
patent: 4372395 (1983-02-01), Hammett
K. R. Miniszewski and T. E. Waterman, Fire Management/Suppression Systems/Concepts Relating to Cabin Fire Safety, Oct. 1983, FAA Report, pp. 51-63.

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