ACTUATOR FOR FLYING VEHICLE CONTROL SYSTEM Russian patent published in 2006 - IPC B64C13/36

Abstract SU 1840174 A1

FIELD: aeronautical engineering.

SUBSTANCE: proposed actuator has body, hydraulic motor, locking device with control piston, cut-in and cross-feed valves connected with working cavities of locking device. Control piston is provided with profiled stop. Cross-feed valve is provided with cylindrical bead engageable with end face of control piston in one of extreme positions.

EFFECT: enhanced reliability.

1 dwg

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SU 1 840 174 A1

Authors

Banin Jurij Mikhajlovich

Demidovtsev Valerij Alekseevich

Dates

2006-06-27—Published

1986-12-18—Filed