An aircraft landing gear has a suspension mechanism which has a four-bar linkage that comprises four links rigidly extending between a corresponding four pivots. A lower link of the four-bar linkage supports front and rear wheels, and is movable relative to an upper link between lengthened and shortened positions. A shock absorber urges the four-bar linkage towards the lengthened position. A length of the upper link of the four-bar linkage is adjustable.
AIRCRAFT LANDING GEAR
2025-06-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
LANDING GEAR OF AIRCRAFT AND AIRCRAFT COMPRISING LANDING GEAR
European Patent Office | 2018
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