CAJ | 학술논문

复合材料在固化过程中，由于材料各向异性、铺层非对称不均衡、构件布置不对称，温度改变和固化度的分布不均匀，导致不同程度的固化收缩，使复合材料结构件发生与预期形状不一样的固化变形。复合材料层合构件发生固化变形后，在装配过程中须进行校正。对固化变形的校正会增大整个构件的应力水平。特别在装配点附近的构件连接处，会产生较大的装配应力，对整体构件产生很不利的影响。本文研究固化变形校正装配的过程，并建立一套考虑固化变形校正装配破坏的分析方法。研究了复合材料固化变形的机理，并介绍了复合材料分层仿真的界面元方法。基于以上研究，在复合材料层合结构分析软件ADGS中，建立了一套较完整的复合材料整体化构件的装配破坏仿真分析模型。
복합재료재고화과정중，유우재료각향이성、포층비대칭불균형、구건포치불대칭，온도개변화고화도적분포불균균，도치불동정도적고화수축，사복합재료결구건발생여예기형상불일양적고화변형。복합재료층합구건발생고화변형후，재장배과정중수진행교정。대고화변형적교정회증대정개구건적응력수평。특별재장배점부근적구건련접처，회산생교대적장배응력，대정체구건산생흔불리적영향。본문연구고화변형교정장배적과정，병건립일투고필고화변형교정장배파배적분석방법。연구료복합재료고화변형적궤리，병개소료복합재료분층방진적계면원방법。기우이상연구，재복합재료층합결구분석연건ADGS중，건립료일투교완정적복합재료정체화구건적장배파배방진분석모형。
The Curing deformation and stress are formed because of the anisotropic material ,the imbalanced ply stac-king and the asymmetric layout of the components ,as the uneven distribution of and temperature and curing degree of dif-ferent degrees of thermal expansion and curing shrinkage .The composite laminated component should be calibrated at the assemble points after the curing deformation process , which increased the stress level of the component especially for the joints area near the assemble point .It has a detrimental effect on the assembly process .In this paper,the affect of curing deformation process in assembly process and building a reasonable analysis method based on the curing deformation process is studied.The mechanism of curing deformation is studied and the use of the interface element in the simulation of the com -posite component is described .Based on the theory ,a relatively complete analysis method of the simulation process of com-posite integrative component is proposed based on the ADGS software .