An assembly is provided for an aircraft. This aircraft assembly includes an aircraft control surface and a hydraulic actuator. The hydraulic actuator includes a housing and a piston within the housing. The housing is formed integral with the aircraft control surface.
Aircraft control surface with integrated hydraulic actuator
2025-03-11
Patent
Electronic Resource
English
AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
European Patent Office | 2023
|AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
European Patent Office | 2023
|