An aircraft landing gear arrangement may comprise a landing gear bogie (300) having an axle, a torque tube (200) surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body (208) extending between a first end (210) and a second end (220). A flange (212) may be disposed at the first end. A mating surface (222) may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange (312) may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.
AIRCRAFT BRAKE TORQUE LOAD REACTION THROUGH LANDING GEAR BOGIE STRUCTURE
BREMSMOMENTLASTREAKTION EINES FLUGZEUGS DURCH DIE FAHRWERKSDREHGESTELLSTRUKTUR
RÉACTION DE CHARGE DE COUPLE DE FREINAGE D'AÉRONEF PAR L'INTERMÉDIAIRE D'UNE STRUCTURE DE BOGIE DE TRAIN D'ATTERRISSAGE
13.03.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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