Modeling and Simulation of a Bonding Process for Space Solar Cells  

作　　者：赵辉 李培波 付庄 赵言正 

机构地区：[1]School of Mechanical Engineering,Shanghai Jiaotong University

出　　处：《Journal of Beijing Institute of Technology》2008年第3期259-263,共5页北京理工大学学报（英文版）

基　　金：the National Natural Science Foundation of China(60675040);the Specialized Researth Fund for the Doctoral Program of Higher Education(20070248021)

摘　　要：A bonding process for space solar cells implemented by an automated coating and bonding system was theoretically investigated for future parametric studies to achieve better bonding quality. First, the mechanical properties of silicone adhesive and the vacuum suction cup were experimentally analyzed. Based on the constitutive relationship of four parts in the bonding process, the dynamic bonding process was modeled systematically, and numerically simulated by a commercial finite element analysis code, Adina. The final bonding edge-alignment error and the thickness and uniformity of the adhesive layer were obtained from simulation and validated by experiments. A simulation platform was created for predicting the final bonding quality via adjusting bonding parameters when dimensions of the solar cells and adhesive were changed.A bonding process for space solar cells implemented by an automated coating and bonding system was theoretically investigated for future parametric studies to achieve better bonding quality. First, the mechanical properties of silicone adhesive and the vacuum suction cup were experimentally analyzed. Based on the constitutive relationship of four parts in the bonding process, the dynamic bonding process was modeled systematically, and numerically simulated by a commercial finite element analysis code, Adina. The final bonding edge-alignment error and the thickness and uniformity of the adhesive layer were obtained from simulation and validated by experiments. A simulation platform was created for predicting the final bonding quality via adjusting bonding parameters when dimensions of the solar cells and adhesive were changed.

关 键 词：space solar cell adhesive bond vacuum suction cup VISCOELASTIC CONTACT finite element analysis 

分 类 号：TG491[金属学及工艺—焊接]