The invention discloses a distributed driving mechanism capable of realizing variable camber and thickness of a wing. The distributed driving mechanism comprises a driving device, a metal flexible skin, a wing rib, a trailing edge wing rib, a ball pin and a worm nut strip, the metal flexible skin is laid on the integral structure of the wing ribs and the rear edge wing ribs and is fixedly hinged to the worm nut strip at the output end of the driving device through the ball pin. The invention provides a distributed driving mechanism capable of realizing variable camber and thickness of a wing, and the shape of the variable-thickness and variable-camber wing can be changed more smoothly and softly.
本发明公开了一种可实现机翼变弯度和厚度的分布式驱动机构,包括:驱动装置、金属柔性蒙皮、翼肋、后缘翼肋、球头销钉、蜗母条;金属柔性蒙皮铺设在翼肋和后缘翼肋的整体结构上,并通过球头销钉与驱动装置的输出端蜗母条固定铰连接。本发明提供一种可实现机翼变弯度和厚度的分布式驱动机构,可使变厚度和弯度机翼更加光滑柔顺的改变形状。
Distributed driving mechanism capable of realizing variable camber and thickness of wing
一种可实现机翼变弯度和厚度的分布式驱动机构
2024-02-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Deformation skin structure capable of realizing variable camber and thickness of wing
European Patent Office | 2024
|NTIS | 1973
NTIS | 1973
NTIS | 1973