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针对某型飞机机翼吻合性超差的问题,从副翼的检查数据、结构、制造过程及下壁板成型等方面分析了其根本原因,提出了改进措施,并对改进措施进行了效果评估,结果表明,该措施能够大幅降低超差。
Aiming at the problem of over-tolerance of wing of a certain type of aircraft, this paper analyzes the root cause of aileron inspection data, structure, manufacturing process and forming of the lower panel, puts forward the improvement measures, and evaluates the improvement measures , The results show that this measure can significantly reduce over-tolerance.