Changeable wing profile
First Claim
1. An aerodynamic structure for a wing or rudder arrangement of an aircraft, comprising:
- a support structure; and
an outer skin;
wherein the support structure comprises an adaptive surface support structure in the longitudinal direction, which extends in the longitudinal direction from a root area to an outer end area, and is formed by a support surface, which exhibits an adjustable periodic profiling that runs in a transverse direction, in which first and second flange areas are alternatingly formed, and joined together by web areas running in the direction of a profile height, wherein alternatingly aligned open profile segments running in the longitudinal direction are formed;
wherein, in the area of the open profile segments, the support structure comprises several connecting segments running in the transverse direction, which join together two adjacent first or second flange areas;
wherein at least a portion of the connecting segments are designed as adjustable-length connecting segments, so that the distance between the adjacent first or second flange areas can be adjusted;
wherein the width of the open profile segments can be varied by the adjustable connecting segments;
wherein the outer skin is attached to the support surface;
wherein an outer contour of the aerodynamic structure can be changed at least in the transverse direction by adjusting the distance between the adjacent first or second flange areas;
wherein the periodic profiling comprises a repeating sequence of flanges and webs and the alternatingly aligned opened profile segments; and
wherein the flange areas run on the two opposing outer sides of the profiling, with the first flange areas on one side and the second flange areas on the other side.
1 Assignment
0 Petitions
Accused Products
Abstract
This relates to changes in wing profiles. In order to provide an aerodynamic structure that can be variably adjusted and changed with respect to the wing profile, it is provided that an aerodynamic structure for a wing or rudder arrangement of an aircraft comprises a support structure and an outer skin. The support structure comprises an adaptive surface support structure in a longitudinal direction, which extends in a longitudinal direction from a root area to an outer end area, and is formed by a support surface, which comprises an adjustable periodic profiling that runs in the transverse direction, in which first flange areas and second flange areas are alternatingly formed, and joined together by web areas running in the direction of a profile height. Alternatingly aligned open profile segments running in the longitudinal direction are here formed.
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Citations
12 Claims
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1. An aerodynamic structure for a wing or rudder arrangement of an aircraft, comprising:
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a support structure; and an outer skin; wherein the support structure comprises an adaptive surface support structure in the longitudinal direction, which extends in the longitudinal direction from a root area to an outer end area, and is formed by a support surface, which exhibits an adjustable periodic profiling that runs in a transverse direction, in which first and second flange areas are alternatingly formed, and joined together by web areas running in the direction of a profile height, wherein alternatingly aligned open profile segments running in the longitudinal direction are formed; wherein, in the area of the open profile segments, the support structure comprises several connecting segments running in the transverse direction, which join together two adjacent first or second flange areas; wherein at least a portion of the connecting segments are designed as adjustable-length connecting segments, so that the distance between the adjacent first or second flange areas can be adjusted; wherein the width of the open profile segments can be varied by the adjustable connecting segments; wherein the outer skin is attached to the support surface; wherein an outer contour of the aerodynamic structure can be changed at least in the transverse direction by adjusting the distance between the adjacent first or second flange areas; wherein the periodic profiling comprises a repeating sequence of flanges and webs and the alternatingly aligned opened profile segments; and wherein the flange areas run on the two opposing outer sides of the profiling, with the first flange areas on one side and the second flange areas on the other side. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. An aircraft, comprising:
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a fuselage structure, a wing assembly with at least one wing surface; and a tail unit with at least one control surface; wherein the wing assembly and tail unit are held on the fuselage structure; and wherein at least one wing surface and/or one control surface is designed with an aerodynamic structure for a wing or rudder arrangement of an aircraft, comprising; a support structure; and an outer skin; wherein the support structure comprises an adaptive surface support structure in the longitudinal direction, which extends in the longitudinal direction from a root area to an outer end area, and is formed by a support surface, which exhibits an adjustable periodic profiling that runs in a transverse direction, in which first and second flange areas are alternatingly formed, and joined together by web areas running in the direction of a profile height, wherein alternatingly aligned open profile segments running in the longitudinal direction are formed; wherein, in the area of the open profile segments, the support structure comprises several connecting segments running in the transverse direction, which join together two adjacent first or second flange areas; wherein at least a portion of the connecting segments are designed as adjustable-length connecting segments, so that the distance between the adjacent first or second flange areas can be adjusted; wherein the width of the open profile segments can be varied by the adjustable connecting segments; wherein the outer skin is attached to the support surface; wherein an outer contour of the aerodynamic structure can be changed at least in the transverse direction by adjusting the distance between the adjacent first or second flange areas; wherein the periodic profiling comprises a repeating sequence of flanges and webs and the alternatingly aligned opened profile segments; and wherein the flange areas run on the two opposing outer sides of the profiling, with the first flange areas on one side and the second flange areas on the other side.
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12. A method for adjusting an outer contour of an aerodynamic structure for a wing or rudder arrangement, comprising:
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a) providing an aerodynamic structure for a wing or rudder arrangement of an aircraft;
wherein the aerodynamic structure exhibits a support structure and an outer skin; andwherein the support structure exhibits an adaptive surface support structure in the longitudinal direction, which extends in a longitudinal direction from a root area to an outer end area, and is formed by a supporting surface, which exhibits an adjustable periodic profiling that runs in a transverse direction, in which first and second flange areas are alternatingly formed, and joined together by web areas running in the direction of a profile height, wherein alternatingly aligned open profile segments running in the longitudinal direction are here formed;
wherein, in the area of the open profile segments, the support structure exhibits several connecting segments running in the transverse direction, which join together two adjacent first or second flange areas; and
wherein at least a portion of the connecting segments are designed as adjustable-length connecting segments; and
wherein the outer skin is attached to the supporting surface;wherein the periodic profiling comprises a repeating sequence of flanges and webs and the alternatingly aligned opened profile segments; and wherein the flange areas run on the two opposing outer sides of the profiling, with the first flange areas on one side and the second flange areas on the other side; b) adjusting the adjustable-length connecting segments, wherein a width of the open profile segments in varied by the adjustable connecting segments; and c) changing the outer contour of the aerodynamic structure at least in the transverse direction.
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Specification