The present invention relates to an aircraft slat skin repair structure comprising a repair piece shaped to fit to a damaged site of an aircraft slat skin, a plurality of split reinforcement tabs, each split reinforcement tab being secured under the aircraft slat skin at a first portion and each split reinforcement tab being secured to the repair piece at a second portion, after the plurality of separate reinforcement sheets are fixed to the aircraft slat skin, the second portion extends from the aircraft slat skin toward the damaged site and encloses an opening. According to the aircraft slat skin repairing structure, the problem that the whole reinforcing piece is difficult to put into the slat skin is solved, double-face operation can be achieved in the reinforcing structure mounting process, the reinforcing structure is mounted in place, and multiple rows of fasteners can be conveniently fixed. In addition, the invention further relates to an aircraft slat skin repairing method.
本发明涉及一种飞机缝翼蒙皮修理结构,包括:修理件,修理件成形为配合到飞机缝翼蒙皮的损伤部位,多个分离式加强片,每个分离式加强片在第一部分处固定到飞机缝翼蒙皮的下方,而每个分离式加强片在第二部分处固定到修理件,其中,多个分离式加强片在固定到飞机缝翼蒙皮后,第二部分从飞机缝翼蒙皮朝向损伤部位延伸并且封围形成开口。该飞机缝翼蒙皮修理结构解决了整块加强片难以放入缝翼蒙皮内部的问题,并且能够在加强结构安装过程中实现双面操作,使得加强结构安装到位并且能够便于固定多排紧固件。另外,本发明还涉及一种飞机缝翼蒙皮修理方法。
Aircraft slat skin repairing structure and repairing method
飞机缝翼蒙皮修理结构和修理方法
2023-04-25
Patent
Electronic Resource
Chinese
European Patent Office | 2025
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