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根据某型飞机中央翼端肋附近上壁板蒙皮局部腐蚀损伤情况,制定了合理的腐蚀修理方案,利用现有的修理条件,结合复合材料修理技术成果,完成了上壁板蒙皮局部腐蚀的现场原位修理,首次真正实现了复合材料高效原位修理技术在该型飞机上的推广应用,可为其他现役飞机的维修提供借鉴。
According to the local corrosion damage of upper wall skin near the central wing flank of a certain aircraft, a reasonable scheme of corrosion repair was established. By using the existing repair conditions and the technical achievements of composite material repair, the local corrosion of the upper wall skin Site repair in situ, for the first time really realized the efficient application of composite materials in situ repair technology in the type of aircraft on the promotion and application of other active aircraft maintenance can provide reference.