An assembly (20) is provided for an aircraft. This aircraft assembly (20) includes an aircraft control surface (24) and a hydraulic actuator (26). The hydraulic actuator (26) includes a housing (70) and a piston (74) within the housing (70). The housing (70) is formed integral with the aircraft control surface (24).
AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
FLUGZEUGSTEUERFLÄCHE MIT INTEGRIERTEM HYDRAULISCHEN AKTUATOR
GOUVERNE D'AÉRONEF À ACTIONNEUR HYDRAULIQUE INTÉGRÉ
2023-07-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
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