Flight control device and method for increased rigging precision

    公开(公告)号:US12071222B2

    公开(公告)日:2024-08-27

    申请号:US17826684

    申请日:2022-05-27

    CPC classification number: B64C13/50

    Abstract: The present disclosure relates to a flight control device that can be mounted to a body of a wing of an aircraft to reduce or eliminate backlash in electromechanical actuators (EMAs). The flight control device can include a flight control member and first and second actuators for moving the flight control member relative to the wing of the aircraft. The first and second actuators can be mechanically isolated from one another except for their mutual connection to the flight control member. The first and second actuators can cooperate to apply torsional loading to the flight control member about an axis of the flight control member to reduce or eliminate backlash.

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