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
Title | Year | Author | Number |
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|
SU1840182A1 |
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Authors
Dates
2006-06-27—Published
1980-10-01—Filed