The invention discloses an aircraft wing for aerospace. The aircraft wing comprises a wing body, an inserting groove is formed in the right end of the wing body, a turbine is arranged below an aircraft body, the top of the turbine is fixedly connected with the bottom of the wing body, and a connecting assembly is arranged at the right side of the wing body. According to the aircraft wing for the aerospace, through clearance fit of an inserting block and the inserting groove, the wing body and the aircraft body can be rapidly positioned, then the installation difficulty is reduced, the installation efficiency is improved, rapid disassembly and assembly between the wing body and the aircraft body can be achieved, the disassembly and assembly efficiency is improved, and follow-up overhaul andmaintenance of the wing body are facilitated; and through meshing connection of a first gear and a second gear at the left side and threaded connection of a threaded rod at the left side and a lantern ring, rotary opening and closing of a lower rotating plate can be controlled under the action of a supporting rod at the lower portion, then the angle above the wing body is increased, the lifting force of the wing body during high-speed movement is improved, and the rising efficiency of an aircraft is improved.
本发明公开了一种航空航天用飞机机翼,包括机翼,所述机翼的右端设有插槽,所述机体的下方设有涡轮,所述涡轮的顶部与机翼的底部固定连接,所述机翼的右侧设有连接组件。该航空航天用飞机机翼,可通过插块与插槽的间隙配合,使得机翼与机体之间可快速实现定位,进而降低安装难度,提升安装效率,进而使得机翼和机体之间可实现快速拆装,进而提升拆装效率,且便于后续对机翼的检修和维护,可通过左侧第一齿轮和第二齿轮的啮合连接,以及左侧螺纹杆与套环的螺纹连接,在下方支杆的作用下,可对下转板的转动开合进行控制,进而增大机翼上方角度,提升机翼在高速移动时的升力,提升飞机上升效率。
Aircraft wing for aerospace
一种航空航天用飞机机翼
2020-12-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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