Landing gear shrink link mechanism
AssigneeThe Boeing Company
InventorsChristopher M. Alley, Leanne M. Campbell, Gabriela K. Defrancisci, Gregory J. Vering, Aaron P. Knock, Mitchell Mellor, Justin D. Cottet
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Estimating the term…
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AssigneeThe Boeing Company
InventorsChristopher M. Alley, Leanne M. Campbell, Gabriela K. Defrancisci, Gregory J. Vering, Aaron P. Knock, Mitchell Mellor, Justin D. Cottet
Estimating the term…
A landing gear including an outer cylinder, a shock strut assembly, and a passive shrink mechanism. The outer cylinder is coupled to a frame of an aircraft about a trunnion axis of rotation. The shock strut assembly is coupled to the outer cylinder for reciprocation along a longitudinal axis of the outer cylinder. The passive shrink mechanism includes: a first shrink link member coupled to the outer cylinder, a second shrink link member coupling the first shrink link member to the shock strut assembly, a crank member coupled to the outer cylinder, a first connecting link coupling the crank member to a walking beam of a landing gear retract mechanism, and a second connecting link coupling the crank member to the first shrink link member. The passive shrink mechanism is passively extended and shortened through actuation of the landing gear retract mechanism with deployment and retraction of the landing gear.
A landing gear comprising:
An aircraft comprising:
A method of operating a landing gear of an aircraft, the method comprising:
Dependencies are inferred from the claim text.