Aircraft safety fuel tank

Fluid handling – Control by change of position or inertia of system

Patent

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Details

137322, 141349, 244135R, 2511496, 2511497, 220900, F16K 1736

Patent

active

046090045

ABSTRACT:
An aircraft safety fuel tank is provided and consists of a safety seal fuel filler neck secured to an inlet opening of a housing, a quick coupling engine fuel line holder secured to an outlet opening of the housing, a protective covering wrapped around the housing and at least one strap for supporting the tank to the aircraft.

REFERENCES:
patent: 1810366 (1931-06-01), Martin
patent: 2428527 (1947-10-01), Plumb
patent: 2461096 (1949-02-01), Wagner
patent: 2630131 (1953-03-01), Snyder
patent: 3170667 (1965-02-01), Szohatzky
patent: 3538950 (1970-11-01), Porteners
patent: 3574314 (1971-04-01), Quercia
patent: 3622035 (1971-11-01), Suter
patent: 4323094 (1982-04-01), Paulis

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