Structure for mounting and sealing a piston sleeve within an act

Expansible chamber devices – Cylinder detail – Cylinder or liner retained in casing by casing closure or...

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Details

92165R, 921691, 92168, F01B 1102

Patent

active

055114636

ABSTRACT:
A fluid pressure actuator for aircraft ailerons comprises a body having a bore within which a piston sleeve or bushing is mounted only by its inner end. The fluid pressure actuated piston is in turn slidably and sealably mounted in the piston sleeve independently of the actuator body.

REFERENCES:
patent: 2282502 (1942-05-01), Suth
patent: 2692584 (1954-10-01), Armington et al.
patent: 4574591 (1986-03-01), Bertsch
patent: 5172625 (1992-12-01), Latham

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