An aircraft landing gear wheel (202) includes a main body (206) with a hub portion (302) and a driven gear portion (208). The hub portion (302) includes a gear end (318) and an attachment end (316). The driven gear portion (208) integrally and drivingly connects with the hub portion (302) at the gear end 318).
AIRCRAFT LANDING GEAR WHEEL WITH INTEGRAL GEAR DRIVE
FLUGZEUGFAHRWERKRAD MIT INTEGRIERTEM GETRIEBE
ROUE DE TRAIN D'ATTERRISSAGE D'AVION AVEC ENTRAÎNEMENT PAR ENGRENAGE SOLIDAIRE
20.04.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft Landing Gear Drive Wheel Identification System
Europäisches Patentamt | 2016
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