The invention discloses a variable-thickness wing, and relates to the technical field of deformation wings, the variable-thickness wing comprises a wing outer frame, a power input module, a thickness deformation module and a flap deformation module, the power input module is installed in the wing outer frame, and the output end of the power input module is connected with the thickness deformation module and the flap deformation module; the thickness deformation modules are arranged close to the front edge of the wing outer frame, the thickness deformation modules are installed on the two sides of the wing outer frame, the thickness deformation modules can be driven by the power input module to adjust the thickness of the wing outer frame, and one end of the flap deformation module extends to a rear edge flap connected with the wing outer frame. And the flap deformation module can be driven by the power input module to adjust the angle of the trailing edge flap. The device is simple in overall structure, easy to operate and high in control precision.
本发明公开了一种变厚度机翼,涉及变形机翼技术领域,包括机翼外框、动力输入模块、厚度变形模块和襟翼变形模块,动力输入模块安装于机翼外框内,且动力输入模块的输出端分别连接厚度变形模块和襟翼变形模块,厚度变形模块靠近机翼外框的前缘设置,且厚度变形模块安装于机翼外框的两侧,且厚度变形模块能够在动力输入模块的带动下对机翼外框的厚度调节,襟翼变形模块的一端延伸至连接机翼外框的后缘襟翼,且襟翼变形模块能够在动力输入模块的带动下对后缘襟翼的角度调节。本发明整体结构简单、易于操作,且控制精度高。
Variable-thickness wing
一种变厚度机翼
2024-08-13
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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