Wing arrangement comprising an adjustable flap and fairing element for covering a flap adjustment mechanism of a wing
AssigneeAirbus Operations GmbH
InventorKarsten Schroeder
Life of this patent
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Abstract
A wing arrangement includes, but is not limited to an adjustable flap, which is adjustable between a retracted position and at least one extended position, has at least one fairing element for covering a flap adjustment mechanism and at least one cover element. The fairing element extends downstream at least as far as the flap and has, in a surface facing the flap, a cutout which correlates with an intended adjustment movement of the flap. The cover element is movably arranged with respect to the fairing element and adapted such to cover the cutout in the fairing element in the retracted position of the flap and expose at least part of said cutout in an extended position.
Claims15
A wing arrangement, comprising:
- an adjustable flap that is adjustable between a retracted position and at least one extended position, the adjustable flap comprising:
- at least one fairing element that is configured to cover a flap adjustment mechanism, the at least one fairing element extending downstream at least as far as the adjustable flap and comprises, in a surface facing the adjustable flap, a cutout that correlates with an intended adjustment movement of the adjustable flap;
- and
- at least one cover element that is movably arrangeable with respect to the at least one fairing element and configured to cover the cutout in the at least one fairing element in the retracted position of the adjustable flap and expose at least part of said cutout in an extended position.
A fairing element for covering a flap adjustment mechanism on a wing, comprising:
- two walls for fixing to the wing and a base element;
- a circular-segment-shaped cutout within the two walls on a side opposite the base element, the circular-segment-shaped cutout is configured to receive a flap that is pivotally arranged on the wing.
A cover element, comprising:
- a first circle-segment-shaped wall;
- a second circle-segment-shaped wall that is configured with the first circle-segment-shaped wall to pivot with respect to a fairing element that is fixed to a wing of an aircraft,
- wherein the first circle-segment-shaped wall and the second circle-segment-shaped wall are further configured to cover a circle-segment-shaped cutout in at least one fairing element when there is movement of a flap pivotally arranged on the wing.
Dependencies are inferred from the claim text.