Systems and methods for controlling aircraft flaps and spoilers

Details Systems and methods for controlling aircraft flaps and spoilers Systems and methods for controlling aircraft flaps and spoilers

B - Operations, Transporting

64

C

B64C 9/10 (2006.01) B64C 9/20 (2006.01) B64C 9/32 (2006.01)

Patent

CA 2706676

An aircraft wing system and method is disclosed. The system includes a wing having a trailing edge, and a flap positioned proximate to the wing trailing edge and being deployable relative to the wing. The system also includes a first actuator operatively coupled to the flap to move the flap relative to the wing, and a spoiler positioned at least proximate to the flap, the spoiler being deployable relative to the wing. The system also includes a second actuator operatively coupled to the spoiler to drive the spoiler during a first mode of operation, the second actuator being configured to release at least a portion of a driving force applied to the spoiler during a second mode of operation to allow the flap to mechanically contact and drive the spoiler.

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