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
DREHGESTELLBALKEN EINES FAHRWERKS MIT AUFBOCKHAUBE
BALANCIER DE BOGIE DE TRAIN D'ATTERRISSAGE MUNIE D'UN DÔME DE LEVAGE
06.04.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |