An aircraft landing gear assembly comprising an oleo-pneumatic shock absorber 50 comprising an outer cylinder 52 and sliding tube 54 movable between a compressed position and an extended position, further comprising a sprung element 71 coupled to the shock absorber 50, movable between a spaced position and an engaged position, and further comprising a weight-on-wheels sensor (62, 64, 66) arranged to monitor movement of the sprung element 71 from the spaced position to the engaged position against spring 68.
Aircraft landing gear assembly
2024-12-04
Patent
Electronic Resource
English