Study on Mould Surface Revising of Composites Part Based on the Surface Node
HAN Zhiren1,2, YANG Pan2, TONG Gang3, XIANG Song3
(1. Key Laboratory of Fundamental Science for National Defense of Aeronautical Digital Manufacturing Process, Shenyang
110136, China;
2. Department of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China;
3.Liaoning General Aviation Academy, Shenyang 110136, China)
Abstract：Aiming at the problems in the aerospace industry for a long time that curing process causes the size error
of composite part prepared in autoclave, assembly with stress and fatigue life is reduced. It realizes the match between
the two surfaces by the location coordinates of fiducial points, and presents a arithmetic of deformation modification and
a feasible means of correction by the study on the factors and mechanism of composites curing deformation. In the design
process of the forming die, a compensation for the surface of the forming die has been carried out, which reduces the trial
and amendment work of the die. It can realize the effective control of composites curing deformation and achieve the goal
of composites precision manufacturing.
韩志仁1,2，杨 攀2，佟 刚3，项 松3. 基于型面节点的复合材料构件模具型面修正研究[J]. 航空制造技术, 2017, 60(4): 16-19.
HAN Zhiren1,2, YANG Pan2, TONG Gang3, XIANG Song3. Study on Mould Surface Revising of Composites Part Based on the Surface Node. Aeronautical Manufacturing Technology, 2017, 60(4): 16-19.
2017, 
