The invention discloses an aircraft body skin crack repairing and redundant object taking-out method, and relates to the technical field of airplanes, and the method comprises the following steps: carrying out nondestructive testing on an aircraft body skin crack area to determine a crack tip; digging the crack by using a milling tool to form a hole, wherein the hole covers the crack area of the airframe skin; carrying out nondestructive testing on the dug-out aircraft body skin crack area again; a suction tool penetrates through the hole to enter the machine body, redundant substances in the machine body are adsorbed, and the suction tool is moved out after adsorption is completed; manufacturing patch blocks made of the same material as the aircraft body, and filling the holes with the patch blocks; and the patch block is fixed on the airplane body by using a rivet. The method for repairing the aircraft body skin crack and taking out the redundant materials can be used for repairing the aircraft body skin crack area, and the redundant materials in the aircraft body can be taken out in the repairing process so as to prevent the redundant materials from influencing the work of the aircraft.
本发明公开了一种飞机机体蒙皮裂纹修复及多余物取出的方法,涉及飞机技术领域,包括如下步骤:对机体蒙皮裂纹区域进行无损检测,以确定裂纹尖端;使用铣切工具对裂纹进行挖除以形成孔洞,孔洞覆盖机体蒙皮裂纹区域;对挖除后的机体蒙皮裂纹区域再次进行无损检测;使用抽吸工具穿设孔洞进入机体的内部,吸附机体内部的多余物,吸附完成之后移出抽吸工具;制作和飞机机体同材质的补丁块,并将补丁块填补于孔洞;使用铆钉将补丁块固定于飞机机体上。本发明提供的飞机机体蒙皮裂纹修复及多余物取出的方法可用于对飞机机体蒙皮裂纹区域进行修复,还能在修复的过程中取出机体内部的多余物,以避免多余物影响飞机工作。
Aircraft body skin crack repairing and redundant object taking-out method
飞机机体蒙皮裂纹修复及多余物取出的方法
2024-04-02
Patent
Elektronische Ressource
Chinesisch
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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