宇航材料工艺2024，Vol.54Issue(3)：22-29,8.DOI:10.12044/j.issn.1007-2330.2024.03.003
基于实测数据的复合材料构件装配干涉与间隙计算
Interference and Gap Calculation for Composite Component Assembly Based on Measured Data
王琦 1张聘 1仲钰 1衡兴波 2张德伟2
作者信息
- 1. 航空工业济南特种结构研究所,高性能电磁窗航空科技重点实验室,济南 250023
- 2. 南京航空航天大学,南京 210016
- 折叠
摘要
Abstract
For the composite component assembly interference problem caused by molding errors,this paper proposed a method of dimensional reduction of composite component assembly interference and clearance based on point cloud data obtained from laser equipment,it converts the interference and clearance calculation of the three-dimensional assembly into the calculation of the two-dimensional boundary distance.Taking a certain type of aircraft random assembly as an example,the feasibility of the proposed method and algorithm is verified through experiments,and the assembly accuracy and efficiency are improved compared with the original assembly process.关键词
复合材料/装配/刚性变换/边界提取/干涉计算/点云Key words
Composites/Assembly/Rigid transformation/Boundary extraction/Interference calculation/Point cloud分类
信息技术与安全科学引用本文复制引用
王琦,张聘,仲钰,衡兴波,张德伟..基于实测数据的复合材料构件装配干涉与间隙计算[J].宇航材料工艺,2024,54(3):22-29,8.
