The invention relates to the technical field of aircraft skin repairing, in particular to an aircraft skin repairing structure based on a self-piercing riveting technology, which comprises a base, an adjusting assembly is arranged on the base, a riveting assembly is arranged at the top of the adjusting assembly, a supporting assembly is arranged on one side of the riveting assembly, and a moving assembly is arranged at the bottom of the base. The adjusting assembly comprises a cavity formed in the base, a sliding plate is slidably connected into the cavity, and sliding rods are fixedly installed on the two sides of the top of the sliding plate. According to the aircraft skin repairing device, the adjusting assembly and the riveting assembly are arranged and matched with the stamping die and the female die, in the using process, the position of the aircraft skin repairing device can be conveniently adjusted and riveted according to the repairing requirement, and therefore the aircraft skin can be conveniently repaired, and the using convenience of the structure is improved.
本发明涉及飞机蒙皮修理技术领域,具体为基于自冲铆接技术的飞机蒙皮修理结构,包括底座,所述底座上设置有调节组件,调节组件的顶部设置有铆接组件,铆接组件的一侧设置有支撑组件,底座的底部设置有移动组件,调节组件包括开设在底座内部的腔体,腔体的内部滑动连接有滑板,滑板顶部的两侧均固定安装有滑杆。本发明通过设置的调节组件和铆接组件,配合冲压模和凹模,在使用的过程中,方便根据修复要求对其位置进行调节和铆接操作,从而方便对飞机蒙皮进行修复操作,提高了该结构的使用便捷度。
Aircraft skin repairing structure and rapid repairing method based on self-piercing riveting technology
基于自冲铆接技术的飞机蒙皮修理结构和快速修理方法
2025-03-18
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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|Self-piercing riveting advantages
British Library Online Contents | 1998
Dimensional Variation in Self-Piercing Riveting
SAE Technical Papers | 2006
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