A locking actuator arrangement may comprise an actuator housing defining a retaining cavity, an actuator piston comprising a piston head and a piston rod extending from the piston head, a receptacle body defining a receiving cavity, wherein the receiving cavity is configured to receive at least a portion of the piston rod, and the piston rod is configured to be received by the receiving cavity in response to alignment of at least two coupled links.
Landing gear folding brace with locking actuator
2019-11-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |