Aeronautics and astronautics – Aircraft structure – Fuel supply
Patent
1978-07-25
1981-12-22
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft structure
Fuel supply
244140, 244149, 137572, B64D 3726
Patent
active
043066933
ABSTRACT:
A powered aircraft has a jettisonable fuel tank releasably secured in the bottom of its fuselage. A valve is arranged to shut off fuel flow from the tank upon releasing of the tank from the fuselage, whereupon a parachute connected to the tank is released to slow the descent of the tank. Additionally, a reserve fuel tank in the fuselage is normally connected to the jettisonable fuel tank, and the valve is so arranged that fuel flow communication is normally maintained between the jettisonable fuel tank and the aircraft engine while fuel is prevented from flowing from the reserve tank to the engine. However, when the jettisonable fuel tank is released from the fuselage, the valve shuts off the flow of fuel from the jettisonable fuel tank and establishes open communication between the reserve tank and the engine to permit continued operation of the aircraft under power of the engine.
REFERENCES:
patent: 2623721 (1952-12-01), Harrington
patent: 2702680 (1955-02-01), Heinemann et al.
patent: 2749065 (1956-06-01), Soule
patent: 2764374 (1956-09-01), Anderson et al.
patent: 3409254 (1968-11-01), Nastase
patent: 3677284 (1972-07-01), Mendez
patent: 3754569 (1973-08-01), Fallotico
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