An aircraft landing gear assembly comprising a bogie beam (2), an axle (4) extending through the bogie beam and a jacking dome fitting (6) extending through a sidewall (8) of the bogie beam and arranged to transfer vertical loads applied to the jacking dome fitting to the axle.
Landing gear bogie beam with jacking dome
2016-03-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |