Compensation actuator for a rotorcraft flight control

Electricity: motive power systems – Automatic and/or with time-delay means – Sound – supersonic vibration or mechanical vibration

Reexamination Certificate

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Details

C318S632000, C318S655000, C244S075100, C244S07600R, C244S175000, C244S177000, C244S178000

Reexamination Certificate

active

07969110

ABSTRACT:
The invention relates to an actuator having an (auto)synchronous rotary electric motor and a reversible speed-reducing gearbox coupled to the motor to be driven in rotation thereby An outlet shaft is coupled to the speed-reducing gearbox to be driven in rotation thereby A first angular position sensor and a control circuit are connected to the motor. The circuit delivers a motor power supply signal that varies as a function of a position setpoint signal applied to the control circuit and as a function of signals delivered by the angular position sensor. The gearbox has a plurality of speed-reducing each having a pair of gears mounted to rotate about two parallel axes of rotation.

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French Search Report dated Apr. 30, 2008.

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