A fairing drive assembly (200) couples a flap assembly of a wing of an aircraft to a fairing of the wing. The fairing drive assembly may include a fairing cam (204) including a first joint and a second joint, and a flap link (240) pivotally coupled to the first joint of the fairing cam and the flap assembly. A fairing drive arm (220) is pivotally coupled to the second joint and the fairing. The fairing cam is configured to rotate upon actuation of the flap assembly and deflect the fairing away from the flap assembly.
AIRCRAFT WING ASSEMBLY COMPRISING A WING FAIRING DRIVE ASSEMBLY
FLUGZEUGFLÜGELANORDNUNG UMFASSSEND EINER FLÜGELVERKLEIDUNGSANTRIEBSANORDNUNG
ENSEMBLE D'AILE D'AVION COMPRENANT UN ENSSEMBLE DE COMMANDE DE CARÉNAGE D'EMPLANTURE D'AILE
2019-12-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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