Abstract：With increasing of the application amount and range of composite in the new generation airframe, composite
structures put forward higher demands on assembly quality and methods. The research and application of stress-less
assembly methods for composite airframe are systematically summarized and elaborated. The shortcomings & gaps, as well
as development direction of assembly stress control technology for composite airframe in domestic are pointed out.
作者简介: 李东升，北京航空航天大学教授、博士生导师，长期从事飞机制造工艺与装备、精密/ 超精密成形制造方面的教学科研工作。主持完成了国家自然科学基金、国家863、国防预研、企业合作项目等40 余项；获国家科技进步二等奖1 项，国防科学技术一等奖2 项、二等奖1 项，国家发明专利20 余项。发表S C I / E I论文50 余篇，出版教材专著2 部。
引用本文:
李东升，翟雨农，李小强. 飞机复合材料结构少无应力装配方法研究与应用进展*[J]. 航空制造技术, 2017, 60(9): 30-34.
LI Dongsheng, ZHAI Yunong, LI Xiaoqiang. Research and Application Advances of Stress-Less Assembly Methods for Composite Airframe[J]. Aeronautical Manufacturing Technology, 2017, 60(9): 30-34.
2017, 
