The invention provides a variable-camber wing trailing edge structure. The variable-camber wing trailing edge structure is composed of a flexible skin, a variant structure and a driving system. The driving system consists of a driving steering engine, a steering wheel, a screw, a bolt, a nut and a variable cross-section eccentric lever; the variant structure is composed of a corrugated lattice structure control surface and filling foam. The flexible skin is a composite material flexible skin; the flexible skin and the variant structure are connected in a glue joint mode. According to the wing, smooth and continuous bending of the wing can be achieved.
本发明提供一种可变弯度机翼后缘结构,可变弯度机翼后缘结构由柔性蒙皮、变体结构和驱动系统三部分组成;驱动系统由驱动舵机、舵盘、螺钉、螺栓、螺母和变截面偏心杠杆组成;变体结构由波纹点阵结构舵面和填充泡沫组成;柔性蒙皮为复合材料柔性蒙皮;柔性蒙皮和变体结构连接方式为胶接,本发明能够实现机翼光滑连续变弯度。
Variable-camber wing trailing edge structure
一种可变弯度机翼后缘结构
2024-09-03
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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