The invention discloses an aircraft wing capable of loading a solar cell, which comprises a wing shell, a solar storage cell and a cell frame, wherein the bottom of the inner cavity of the wing shellis fixedly connected with a corrugated fixed underframe. According to the aircraft wing capable of loading a solar cell, which relates to the technical field of aircraft wings, the wavy edge of the corrugated fixed underframe is used to increase the perimeter, namely, the welding length with the surfaces of the wing shell and the annular plate is increased; the material increment is not large; meanwhile, the connection strength is improved; a hoop is matched with a first fixing block and a second fixing block; the mounting plate for mounting the cell frame and the annular plate can be firmly fixed together; by utilizing the contact between the hoop and the inclined surfaces of the first fixing block and the second fixing block, the stress can be decomposed into two directions to be matchedwith bolts for use, and the fixing strength is far greater than that of the bolt for fixing, so that the cell is firmer to install, and the cell can be prevented from loosening due to the breakage ofthe bolt.
本发明公开了一种能够装载太阳能电池的飞机机翼,包括机翼壳体、太阳能蓄电池和电池框架,所述机翼壳体内腔的底部固定连接有波纹固定底架,本发明涉及飞机机翼技术领域。该能够装载太阳能电池的飞机机翼,利用波纹固定底架的波浪形边缘,增大了周长,即增大了与机翼壳体和环形板表面的焊接长度,材料增加量不大的同时增加了连接强度,而利用抱箍与第一固定块、第二固定块的配合,可将用于安装电池框架的安装板与环形板牢牢固定在一起,利用抱箍与第一固定块、第二固定块斜面的接触,可将受力分解成两个方向,配合螺栓使用,其固定强度远远大于仅用螺柱固定,使电池的安装更牢固,即可避免应螺柱断裂而使电池松动。
Aircraft wing capable of loading solar cell
一种能够装载太阳能电池的飞机机翼
2020-05-01
Patent
Electronic Resource
Chinese