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
05.07.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT CONTROL SURFACE WITH INTEGRATED HYDRAULIC ACTUATOR
Europäisches Patentamt | 2023
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