A landing gear actuation system is disclosed herein. The landing gear actuation system includes an attachment point integral to a movable member, a flexible pull member having a first end coupled to the attachment point, and a motor configured to move the flexible pull member, wherein the movement of the flexible pull member moves the attachment point and the movable member.
LANDING GEAR ACTUATION SYSTEM
SYSTEME D'ACTIONNEMENT DE TRAIN D'ATTERRISSAGE
2023-10-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
European Patent Office | 2021
|DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
European Patent Office | 2021
|