Patent ID: 11927249
Assignee: WOODWARD, INC.
Field: Mechanical elements (Mechanical engineering)
Classification: CPC F  B | IPC B  F

Claim 14:
15. The apparatus of claim 10, wherein:
the first actuator housing and the second actuator housing are configured to be coupled to an airframe structure of an aircraft, and the rotor arm is configured to be coupled to a moveable control surface of the aircraft, such that the moveable control surface is configured to move relative to the airframe structure by the linear-to-rotary motion apparatus; or
the first actuator housing and the second actuator housing are configured to be coupled to the moveable control surface of the aircraft, and the rotor arm is configured to be coupled to the airframe structure of an aircraft, such that the moveable control surface is configured to move relative to the airframe structure by the linear-to-rotary motion apparatus.