| 摘要 |
The invention relates to changes to wing profiles. In order to provide an aerodynamic structure that can be adapted and changed in many ways in terms of the wing profile, an aerodynamic structure (10) for a wing device or control surface device of an aircraft according to the invention has a supporting structure (12) and an outer skin (14). The supporting structure has a stationary spar (16) in the longitudinal direction, which spar extends from a root region to an outer end region. The supporting structure also has a plurality of adaptive framework segments (18) in the transverse direction, which each consist of a plurality of triangular compartments (20), which are arranged next to each other and are formed by control elements (22) of stationary length and control elements (24) of adjustable length. The framework segments are connected to the stationary spar. At least some of the triangular compartments have one of the adjustable control elements, at least on one side, such that the framework segments are adjustable in shape. The outer skin is fastened to the framework segments. An outer contour (26) of the aerodynamic structure can be changed at least in the transverse direction by adjusting the shape of the frameworks. |
