Embodiments of the present invention provide a composite skin that can be used on a curved sweepback wing. The combined skin of the bending variable sweepback wing comprises a first skin part and a second skin part. The first skin part is mounted at a part from a wing main beam to a wing leading edge; the second skin portion is mounted at a portion from the wing girder to the wing trailing edge. The first skin portion is of an integral structure. The second skin part comprises a plurality of belts; the length directions of the plurality of belts are along the direction of the machine body; the plurality of belts are stacked in the spanwise direction. The combined skin provided by the embodiment of the invention is high in deformability and wide in application range.
本发明的实施例提供一种可以用在弯曲变后掠机翼上的组合蒙皮。弯曲变后掠机翼的组合蒙皮包括:第一蒙皮部分,第二蒙皮部分。所述第一蒙皮部分安装在从机翼主梁到机翼前缘的部分;所述第二蒙皮部分安装在从所述机翼主梁到机翼后缘的部分。所述第一蒙皮部分是一体的结构。所述第二蒙皮部分包括多个带;所述多个带的长度方向沿着机身方向;所述多个带在翼展方向上层叠设置。本发明的实施例提供的组合蒙皮变形能力强,适用范围广。
Combined skin of bending variable-sweepback wing
一种弯曲变后掠机翼的组合蒙皮
2022-11-11
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Flexible main beam of bending variable sweepback wing
Europäisches Patentamt | 2022
|Variable wing sweepback bell X-5
Engineering Index Backfile | 1951
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