The invention aims to provide an assembly method for assembling an aircraft fuselage panel, a fuselage part and an aircraft. The aircraft panel is assembled by welding, so that the flexibility of the aircraft panel can be improved. The panels (26, 28) are docked together along the longitudinal tie lines and secured to each other by welding the longitudinal edges (30, 32) of the panels without joining the longitudinal ends (30A, 30B, 32A, 32B) of the welded edges (30, 32) of the panels to each other. According to the invention, the longitudinal shroud rings (38, 40) are fixed in such a way that the concave surfaces of the panels (26, 28) are partially covered at least partially at the ends (30A, 30B, 32A, 32B). No welding at the end introduces the desired flexibility.
本发明旨在提供一种用于组装飞行器机身面板的组装方法、机身部分和飞行器。本发明通过焊接来组装飞行器面板,使得可以提高其柔性。沿着纵向连结线将面板(26,28)对接在一起并且通过面板的纵向边缘(30,32)焊接彼此固定,而不将面板的焊接边缘(30,32)的纵向端部(30A,30B,32A,32B)彼此连接。对纵向箍环(38,40)进行固定,其方式为使得至少部分地在所述端部(30A,30B,32A,32B)处部分地覆盖面板(26,28)的凹表面。不在端部处进行焊接引入了所期望的柔性。
Assembly method for assembling aircraft fuselage panel, fuselage part and aircraft
用于组装飞行器机身面板的组装方法、机身部分和飞行器
2024-03-29
Patent
Electronic Resource
Chinese
AIRCRAFT FUSELAGE ASSEMBLING JIG AND METHOD OF HANDLING AIRCRAFT FUSELAGE PANEL
European Patent Office | 2019
|Aircraft fuselage assembling jig and method of handling aircraft fuselage panel
European Patent Office | 2022
|AIRCRAFT FUSELAGE ASSEMBLY JIG AND METHOD FOR HANDLING AIRCRAFT FUSELAGE PANEL
European Patent Office | 2017
|