A landing gear assembly for an aircraft includes a landing member and an actuation mechanism coupled to the landing member. The actuation mechanism is configured to selectively actuate the landing member into a first landing position and a second landing position. The landing member is configured to support the aircraft in either the first landing position or the second landing position.
ADJUSTABLE LANDING GEAR ASSEMBLY FOR USE IN AIRCRAFT
2021-04-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |