A rotary geared actuator (RGA) (211b) is described herein for actuating movement of a first movable surface (210A) and a second movable surface (210B); the RGA (211b) comprising: an input shaft (231) configured to receive torque in use, and an output shaft (232) comprising means configured to communicate with and move both said first surface (210A) and said second surface (210B) in use. The actuator may be used in a leading edge high lift architecture for an aircraft wing, or may be used in other applications.
LEADING EDGE HIGH LIFT ARCHITECTURE
VORDERKANTEN-HOCHAUFTRIEBSARCHITEKTUR
ARCHITECTURE HYPERSUSTENTATRICE DE BORD D'ATTAQUE
26.10.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |