Patent ID: 11884384
Assignee: GOODRICH CORPORATION
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 17:
18. A landing gear for an aircraft, comprising:
a trunnion configured to be rotatably mounted to an aircraft structure;
a landing gear assembly having a main strut mounted to the trunnion;
a wheel assembly coupled to the main strut of the landing gear assembly; and
an actuation system configured to extend and retract the landing gear, the landing gear is configured to rotate about the trunnion in response to the actuation system at least one of extending and retracting the landing gear, the actuation system including:
a trunnion sprocket coupled to the main strut, the trunnion sprocket is concentric with the trunnion;
a first motor configured to move the landing gear assembly; and
a flexible drive member extending between and to the trunnion sprocket and the first motor.