Air inlet control for aircraft or the like

Aeronautics and astronautics – Aircraft power plants – Radiator arrangement

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Details

49 76, 98121A, 165 39, 165 41, 236352, 244 53B, B64C 114

Patent

active

042035660

ABSTRACT:
An air inlet control inset in the skin or outer wall surface of an aircraft or the like. The control device has an open position in which it is able to capture ram air flowing over the wall surface and which at the same time defines an open flow area through which lower pressure ambient air can be inducted when ram air is unavailable. The air inlet control includes a shutter opening into ram air flow, and an actuating mechanism therefor. In one disclosed form of the invention, the shutter is aerodynamically biased to reduce actuating forces required to close the shutter against ram air pressure.

REFERENCES:
patent: 1585091 (1926-05-01), Galli
patent: 3099423 (1963-07-01), Wilde et al.
patent: 3292864 (1966-12-01), Edkins
patent: 3388878 (1968-06-01), Peterson et al.

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