Abstract：Assembly deviation analysis and control of aircraft complaint structure is always a difficulty in aircraft assembly. With the extensive application of composite materials in aircraft structure, this problem is exposed more and more obviously. As the composite parts manufactured by prepreg curing process have the characteristics of large manufacturing deviation and easy damage in non-principal stress direction in the assembly process, so higher requirements are put forward for the deviation analysis and control in the assembly of flexible parts. It is a difficult problem for assembly of composite complaint parts at present, that how to carry out tolerance allocating, technological compensation and over-constrained assembly reasonably to meet the performance requirements after assembly. This paper expounded and summarized the research progress of the deviation analysis and control of flexible parts assembly in aircraft structure, and provided a reference for assembly of aircraft flexible parts.
杨浩然，安鲁陵，黎雪婷. 飞机结构中柔性件装配偏差分析与控制研究进展[J]. 航空制造技术, 2021, 64(4): 30-37.
YANG Haoran, AN Luling, LI Xueting. Research Progress on Analysis and Control of Assembly Deviation of Flexible Parts in Aircraft Structures. Aeronautical Manufacturing Technology, 2021, 64(4): 30-37.
2021, 
