Disclosed is a wing (5) for an aircraft (1), comprising a fixed wing (7), a high lift system (9) including a high lift surface (27) movably mounted to the fixed wing (7), and a high lift actuation system (29) for moving the high lift surface (27) relative to the fixed wing (7) between a retracted position and at least one deployed position, a foldable wing tip portion (11) mounted to the fixed wing (7) pivotally about an axis of rotation (35) between an extended position and a folded position, a tip actuation unit (13) for moving the foldable wing tip portion (11) between the extended position and the folded position. The object to provide a simple, cost-efficient and light-weight wing, is achieved in that the high lift actuation system (29) is drivingly coupled to the tip actuation unit (13) to provide power to the tip actuation unit (13)
КОНСОЛЬ КРЫЛА ДЛЯ ЛЕТАТЕЛЬНОГО АППАРАТА
2020-06-05
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |
КОМПОЗИТНЫЕ НЕРВЮРЫ КРЫЛА ЛЕТАТЕЛЬНОГО АППАРАТА, ИМЕЮЩИЕ ТОКОПРОВОДЯЩИЕ ДОРОЖКИ ЗАЗЕМЛЕНИЯ
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