Emergency aircraft fuel system

Aeronautics and astronautics – Aircraft structure – Fuel supply

Patent

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Details

244135R, 137 67, B64D 3732

Patent

active

057383049

ABSTRACT:
A fuel tank has an outlet fuel line with a valve adjacent the tank. The valve is air operated open and spring biased toward closed. A frangible envelope surrounds the fuel tank and is pressurized from the same air line as that to the valve so loss of air pressure in the envelope leads to closing of the valve in case of a crash situation that causes the envelope to rupture.

REFERENCES:
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patent: 3035797 (1962-05-01), Neuschotz
patent: 3043542 (1962-07-01), Neuschotz
patent: 3312431 (1967-04-01), Vogt
patent: 3509942 (1970-05-01), Lindberg
patent: 4172573 (1979-10-01), Moore et al.
patent: 4323094 (1982-04-01), Paulis et al.
patent: 4609004 (1986-09-01), Greene et al.
patent: 4651952 (1987-03-01), Tavano
patent: 4715417 (1987-12-01), Coloney
patent: 4784354 (1988-11-01), Tavano
patent: 4886225 (1989-12-01), Bates

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