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
08.04.2025
Patent
Elektronische Ressource
Englisch
DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION
Europäisches Patentamt | 2025
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