The invention discloses a variable trailing edge camber wing, and relates to the technical field of aircraft wing structures, the variable trailing edge camber wing comprises a wing body, the wing body comprises a front section, a first adjusting section, a second adjusting section and a third adjusting section, the front section and the first adjusting section are connected through flexible connecting pieces, and the adjusting sections are connected through flexible connecting pieces; the first flexible part covers the surfaces of the two sides of the wing body; the second flexible parts are connected between the front section and the first adjusting section and between the adjusting sections, and the second flexible parts are attached to the first flexible part; the driving part is arranged on the wing body and comprises a driving structure, and the driving structure comprises a first-stage driving piece, a second-stage driving piece and a third-stage driving piece. According to the variable trailing edge camber wing, multi-stage posture adjustment can be achieved so that the wing can reach different deformation states, and meanwhile, in the adjustment process, surface deformation of the wing is smoother and more stable.
本发明公开了一种变后缘弯度机翼,涉及飞机机翼结构技术领域,包括翼身,翼身包括前置段、第一调整段、第二调整段以及第三调整段,前置段与第一调整段之间以及各调整段之间均通过柔性连接件连接;第一柔性件,包覆于翼身的两侧表面;第二柔性件,前置段与第一调整段之间以及各调整段之间均连接有第二柔性件,第二柔性件贴合第一柔性件;以及设置于翼身的驱动部,包括驱动结构,驱动结构包括一级驱动件、二级驱动件以及三级驱动件。本申请的变后缘弯度机翼能够实现多级的姿态调整,以使机翼达到不同的变形状态,同时,调整过程中,机翼的表面变形更加平滑稳定。
Variable trailing edge camber wing
一种变后缘弯度机翼
2024-03-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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