Patent ID: 11884394
Assignee: THE BOEING COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 17:
18. A dual actuation assembly for a wing assembly, the dual actuation assembly comprising:
a frame comprising a mount configured to be coupled to a wing support structure;
a single actuator supported by the frame;
an inboard carrier beam pivotally coupled relative to the frame, operatively coupled to the single actuator, and configured to be operatively coupled to an inboard flight control surface of the wing assembly; and
an outboard carrier beam pivotally coupled relative to the frame, operatively coupled to the single actuator, and configured to be operatively coupled to an outboard flight control surface of the wing assembly;
wherein the single actuator is configured to selectively transition the inboard carrier beam and the outboard carrier beam, in tandem, amongst a retracted configuration and a range of extended configurations.