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
2023-07-06
Patent
Electronic Resource
English
AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
European Patent Office | 2023
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