Research on Modular Assembly Technology of Aircraft Wing
WANG Shouchuan1, HAO Ju1, LI Xining2, GUO Feng1, WANG Yonghong1, WANG Zhanfeng1
1. Tooling Design Institute, AVIC Xi’an Aircraft Industrial (Group) Company Ltd., Xi’an 710089, China;
2. Key Laboratory of Contemporary Design and Integrated Manufacturing Technology, Ministry of Education, School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China
In view of the engineering realization of the modular assembly of a large aircraft wing, the technical background and the modular features of the aircraft components module are analyzed, and the module assembly process and the influencing factors are combed. The engineering design of wing assembly process, wing integration / flexible assembly and active airfoil unit is carried out. The integrated flexible working platform and rail mounting vehicle are designed. The design and analysis of control logic structure, test method and test equipment planning for aircraft active airfoil are finished. Finally, the application of wing module assembly and its effect are introduced.
王守川1,郝巨1,李西宁2,郭峰1,王永宏1,王战峰1. 飞机机翼模块化装配技术研究[J]. 航空制造技术, 2018, 61(13): 68-73.
WANG Shouchuan1, HAO Ju1, LI Xining2, GUO Feng1, WANG Yonghong1, WANG Zhanfeng1. Research on Modular Assembly Technology of Aircraft Wing. Aeronautical Manufacturing Technology, 2018, 61(13): 68-73.