Negative gravity swivel device

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

Patent

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Details

1376254, 244135R, F16K 1736

Patent

active

042034582

ABSTRACT:
An apparatus for withdrawing fluid from the fuel tank of an aircraft or missile. A structure of coaxial cylinders with one slidable member responding to transient variations in the direction of the gravitation ("g") force acting on the reservoir by reversing the fluid withdrawal location. When the "g" force is positive, the fluid is drawn from the reservoir below. If the "g" force becomes negative, the slidable cylinder translates to align a different set of passage ports within the structure, changing the location of the fluid draw to one within the fluid.

REFERENCES:
patent: 2860648 (1958-11-01), Harrison
patent: 2934077 (1960-04-01), Whiting
patent: 3317250 (1967-05-01), Martin

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