Vented liquid reservoir

Gas separation – Means within gas stream for conducting concentrate to collector

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Details

55204, 137 43, 137 45, B01D 1900, F16K 1736

Patent

active

045457913

ABSTRACT:
A liquid reservoir, such as an oil tank, for use in missiles or aircraft which are subjected to extreme flight attitudes. The reservoir has a wall rotationally symmetrical about the longitudinal axis of the reservoir, and the liquid content of the reservoir is rotated about the longitudinal axis to provide, by centrifugal force, a central space within the reservoir which is essentially free of liquid. Air is vented from the reservoir through a fixed vent located within the central space created when the liquid content is rotated.

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patent: 3715863 (1973-02-01), Zanoni
patent: 3771287 (1973-11-01), Sunderland
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patent: 3982399 (1976-09-01), Rookey
patent: 4053291 (1977-10-01), Sims
patent: 4093428 (1978-06-01), Swogger
patent: 4197870 (1980-04-01), Hildebrandt et al.

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