The invention belongs to a structure butt joint method, and provides an aircraft wing body butt joint adjusting method aiming at the technical problems that when a digital attitude adjusting technology is adopted for aircraft wing body butt joint at present, the requirements for the manufacturing and assembling process are high, and the measuring efficiency is low. After a fuselage and wings are pre-leveled, the wings and the fuselage are connected through process bolts, the relative positions of the fuselage and the wings are adjusted by replacing the process bolts between wing bodies, the wing mounting angle, the wing dihedral angle and the wing body symmetry are evaluated through a relative coordinate measurement method, and then whether the relative positions of the wing bodies are correct or not is judged. According to the docking adjustment method, the problems of high requirements on human operation skills and low docking operation efficiency are solved, and the measurement accuracy and the measurement efficiency are effectively improved.
本申请属于一种结构对接方法,针对目前采用数字化姿态调整技术进行飞机翼身对接时,存在制造和装配过程要求高,测量效率低的技术问题,提供一种飞机翼身对接调整方法,通过机身调姿工装上的多个基准点转换坐标系,在机身和机翼均预调平后,先用工艺插销连接机翼和机身,通过更换翼身之间的工艺插销调整机身和机翼之间相对位置,并通过相对坐标测量法评价机翼安装角、机翼上反角和翼身对称性,进而判断翼身相对位置是否正确。本申请的对接调整方法解决了对人操作技能要求高,对接操作效率低的问题,有效提高了测量准确性和测量效率。
Aircraft wing body butt joint adjusting method
一种飞机翼身对接调整方法
2024-07-09
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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