A landing gear actuation system is disclosed herein. The landing gear actuation system includes an attachment point (216) integral to a movable member, a flexible pull member (220) having a first end coupled to the attachment point (216), and a motor (218) configured to move the flexible pull member (220), wherein the movement of the flexible pull member (220) moves the attachment point (216) and the movable member.
LANDING GEAR ACTUATION SYSTEM
FAHRWERKBETÄTIGUNGSSYSTEM
SYSTÈME D'ACTIONNEMENT DE TRAIN D'ATTERRISSAGE
11.10.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
Europäisches Patentamt | 2025
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