The invention provides an intelligent airfoil profile and a rotor wing, the intelligent airfoil profile comprises an I-shaped pipe 6, a U-shaped pipe 5, a cross beam 7, a flexible skin 4 and a fuel oil medium 9, the cross beam 7 is located in the middle of the whole airfoil profile, and the center of the cross beam 7 is matched with the gravity center of the whole airfoil profile; the flexible skin 4 is arranged on the outer contour of the whole intelligent airfoil; the wing-shaped space inside the flexible skin 4 and the first-layer concave pipe 5 on the flexible skin 4 and outside the cross-shaped beam 7 and the first-layer concave pipe 5 on the cross-shaped beam 7 is filled with the I-shaped pipe 6 in a combined mode, and the gap space outside the I-shaped pipe 6 is filled with the fuel oil medium 9; the I-shaped pipe 6 comprises an I-shaped beam 1 and two flexible half pipes 2; the N I-shaped pipes form three combination types, namely a crisscross uniform distribution combination 8, a longitudinal arrangement combination 10 and a transverse arrangement combination 11; the concave pipe 5 comprises a concave beam 3 and a flexible half pipe 2; the flexible half pipes of the I-shaped pipe and the U-shaped pipe are filled with fuel oil media. The flexible half pipe 2 comprises an arc-shaped edge and a right-angle edge.
本申请提供一种智能翼型及旋翼,所述智能翼型包括:工字管6、凹字管5、十字梁7、柔性蒙皮4、燃油介质9,其中:十字梁7位于整个翼型的中间位置,十字梁7中心与整个翼型的重心吻合;柔性蒙皮4布置在整个智能翼型的外轮廓;柔性蒙皮4及其上的第一层凹字管5以内,十字梁7及其上的第一层凹字管5以外的翼型空间,使用工字管6进行组合填充,工字管6外的间隙空间,使用燃油介质9填充;工字管6包括工字梁1和2个柔性半管2;N个工字管构成三种组合类型,即纵横交叉均布组合8、纵列排布组合10、横列排布组合11;凹字管5包括凹字梁3和1个柔性半管2;工字管和凹字管的柔性半管内部均填充燃油介质;柔性半管2包括弧形边和直角边。
Intelligent airfoil profile and rotor wing
一种智能翼型及旋翼
17.12.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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