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

Claim 21:
22. A wing assembly, comprising:
an inboard flight control surface;
an outboard flight control surface, positioned adjacent to and outboard of the inboard flight control surface; and
a dual actuation assembly coupled to and forming a linkage between the inboard flight control surface and the outboard flight control surface, wherein the dual actuation assembly is configured to selectively transition the inboard flight control surface and the outboard flight control surface, in tandem, amongst a retracted configuration and a range of extended configurations, and wherein the dual actuation assembly comprises:
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 and operatively coupled between the single actuator and the inboard flight control surface; and
an outboard carrier beam pivotally coupled relative to the frame and operatively coupled between the single actuator and the outboard flight control surface.