Servo-control device for aircraft flight control

Motors: expansible chamber type – Moving cylinder – Cylinder and piston have relative reciprocation on fixed axis

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Details

91216A, 91384, F01B 1500, F15B 910

Patent

active

044135475

ABSTRACT:
The device comprises a directional valve body which is movable with respect to guide means, and a spool which is slidably mounted in the body and connected to a control lever. The latter is pivotally mounted on a pin which is fixed relative to the body. This pin is carried by a support which is mounted on the body and means are provided for adjusting the position of the support relative to the body.

REFERENCES:
patent: 284 (1877-01-01), Hodson
patent: 2943606 (1960-07-01), Willis et al.
patent: 3122972 (1964-03-01), Rasmussen
patent: 3158068 (1964-11-01), Bokelmon
patent: 3295420 (1967-01-01), Gleason

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