Valve gravity-controlled in dependence upon the flight attitude

Details Valve gravity-controlled in dependence upon the flight attitude Valve gravity-controlled in dependence upon the flight attitude

1979-07-09

1981-02-24

Nilson, Robert G.

Fluid handling

Control by change of position or inertia of system

F16K 1736

Patent

active

042521408

ABSTRACT:
Valve gravity-controlled in dependence upon the current flight attitude of an aircraft, which includes an outer valve housing a plurality of equally spaced conduit connectors for the inlet of a flowing medium. A collector chamber is located between the outer valve and an inner valve housing of the valve, the collector chamber communicating with an outlet for the medium. Spring loaded valve members are associated with each inlet conduit connector of which at least one establishes communication between the respective inlet connector and the collector chamber under the gravity-controlled action of a ball arranged in the inner valve housing.

REFERENCES:
patent: 2239098 (1941-04-01), Hunter
patent: 2324464 (1943-07-01), Parker
patent: 2409220 (1946-10-01), Melichar
patent: 2933095 (1960-04-01), Rumsey
patent: 4185651 (1980-01-01), Paulsen

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