FLYING VEHICLE SERVO UNIT Russian patent published in 2006 - IPC B64C13/36 

Abstract SU 1840176 A1

FIELD: aeronautical engineering.

SUBSTANCE: proposed servo unit has body with built-in hydraulic motor in form of piston with actuating rod, electrohydraulic booster, gear-and-rack reducer of cam mechanism mechanical drive, cam and microswitch. Fitted in body bore in parallel with microswitch are electrical relay and diode which are connected in series with control windings of electromechanical converter of control signal circuit.

EFFECT: automatic limitation of actuating rod travel.

1 dwg

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SU 1 840 176 A1

Authors

Popov Aleksandr Danilovich

Shapkov Vjacheslav Ivanovich

Sokolenkov Jurij Nikolaevich

Maslov Valentin Timofeevich

Vojtko Aleksej Fedorovich

Dates

2006-06-27Published

1980-10-01Filed