Aeronautics and astronautics – Aircraft structure – Fuel supply
Patent
1983-06-06
1989-12-12
Blix, Trygve M.
Aeronautics and astronautics
Aircraft structure
Fuel supply
220900, B64D 3732
Patent
active
048862258
ABSTRACT:
An inflatable bladder is placed between the wall of an aircraft inlet duct nd the liquid fuel to reduce the potential damage caused by hydrodynamic ram effects from a projectile penetrating the fuel tank. The inflatable bladder is inflated by a regulated gas source prior to combat. The inflatable bladder may be formed as a double layered section of a rubber bladder fuel cell type fuel tank, or an inflatable bladder may be bonded to the inner surface of an integral fuel tank wall.
REFERENCES:
patent: 2404418 (1946-07-01), Walker
patent: 2609118 (1952-09-01), Cattaneo
patent: 2623721 (1952-12-01), Harrington
patent: 2653780 (1953-09-01), Pepersack
patent: 2657884 (1953-11-01), Merril
patent: 2690314 (1954-09-01), Porter et al.
patent: 2735635 (1956-02-01), Hoffman
patent: 2736356 (1956-02-01), Bender et al.
patent: 2844269 (1958-07-01), Durbin
patent: 3737125 (1973-06-01), Farmer
patent: 3966147 (1976-06-01), Wittko et al.
Blix Trygve M.
Corl Rodney
Sheinbein Sol
Sliwka Melvin J.
The United States of America as represented by the Secretary of
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