The invention relates to the technical field of aircrafts, and discloses a wing and fuselage connecting method. According to the wing and fuselage connecting method, a wing body, a fuselage body and a plurality of fixing assemblies are included, the wing body 1 comprises a first surface, and a pair of inserting parts is arranged on the first surface; the machine body comprises a second surface, the second surface is provided with plugging holes in one-to-one correspondence with the plugging parts, and the plugging holes extend into the machine body to form corresponding plugging channels; the connecting method comprises the steps that S1, the pair of inserting parts are inserted into the inserting channels through the corresponding inserting holes; and S2, limiting the movement of the inserting part in the corresponding inserting channel through a plurality of fixing assemblies, and enabling the first surface and the second surface to be attached to each other. By means of the wing and fuselage connecting method, rapid disassembly and assembly of the wing and fuselage can be achieved, time and labor are saved, and the transportation cost and the maintenance cost are reduced.
本申请涉及飞行器技术领域,公开了一种机翼机身连接方法。本申请机翼机身连接方法包括机翼本体、机身本体和多个固定组件,所述机翼本体1包括第一表面,第一表面上设有一对插接部;机身本体包括第二表面,第二表面设有与一对插接部一一对应的插接孔,并由一对插接孔分别延伸到机身本体内形成对应的插接通道;连接方法包括:S1:将一对插接部通过对应插接孔插入插接通道;S2:通过多个固定组件限定插接部在对应的插接通道内活动,且使第一表面和第二表面相互贴合。本申请的机翼机身连接方法可以实现机翼机身的快速拆装,省时省力,降低运输成本和维修成本。
Wing and fuselage connecting method
机翼机身连接方法
2024-06-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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