An aircraft landing gear assembly (10) includes a main strut and an axle (18b) on which wheel and brake assemblies (20b, 22b) are mounted. An adaptor member (30) is mounted on a mounting pin and arranged to define a brake rod anchor point (28). The adaptor member is coupled to a part of the landing gear assembly so as to react brake torque and can be formed from a different material than a portion of the main strut.
Aircraft landing gear assembly
Flugzeugfahrwerkanordnung
Ensemble de train d'atterrissage d'avion
2017-03-29
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |