B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 9/18 (2006.01) B64C 3/28 (2006.01)
Patent
CA 2522553
An aircraft wing comprises a main wing (301) with a pivotable trailing edge (304) and a lift-assisting flap (302) on the rear of the wing, wherein the lift-assisting flap (302) is coupled to the main wing (301) and is designed in such a way that in its retracted state (300) it rests against the main wing (301) and in an extended state (310) it forms an air gap (311) with the main wing (301). The pivotable trailing edge (304) is pivotable in such a way that by using pivoting the pivotable trailing edge (304) the shape and the width of the air gap (311) are adjustable.
Aile d'aéronef composée d'une aile principale (301) munie d'un bord de fuite pivotant (304) et d'un volet hypersustentateur (302) placé à l'arrière de l'aile et accouplé à l'aile principale (301). Le volet sustentateur (302) est conçu pour s'appuyer contre l'aile principale (301) lorsqu'il est rétracté (300) et pour former un espace d'air (311) par rapport à l'aile principale (301) lorsqu'il est sorti (310). Le bord de fuite (304) peut pivoter, ce qui permet de modifier la forme et la largeur de l'espace d'air (311).
Dyke Adrian R.
Reckzeh Daniel
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Borden Ladner Gervais Llp
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