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
06.07.2023
Patent
Elektronische Ressource
Englisch
AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
Europäisches Patentamt | 2025
|Aircraft control surface with integrated hydraulic actuator
Europäisches Patentamt | 2025
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