玻璃钢/复合材料 ›› 2020, Vol. 0 ›› Issue (1): 5-11.

• 基础研究 •    下一篇

不同对流换热条件下复合材料层合板固化温度场与热应力分析

顾威, 陈淑仙*   

  1. 中国民用航空飞行学院航空工程学院,广汉 618307
  • 收稿日期:2019-03-18 出版日期:2020-01-28 发布日期:2020-01-28
  • 通讯作者: 陈淑仙(1975-),女,博士,教授,主要从事复合材料热固化方面的研究,bellesavana@163.com。
  • 作者简介:顾威(1995-),男,硕士研究生,研究方向为复合材料热固化方法优化。
  • 基金资助:
    国家自然科学基金资助项目(51306201);四川省科技厅项目(2019YJ0722);中国民用航空飞行学院项目(J2019-033);中国民用航空飞行学院研究生创新项目(X2019-007)

ANALYSIS OF CURING TEMPERATURE FIELD AND THERMAL STRESS OF COMPOSITE LAMINATES UNDER DIFFERENT CONVECTIVE HEAT TRANSFER CONDITIONS

GU Wei, CHEN Shu-xian*   

  1. Aviation Engineering institutee, Civil Aviation Flight University of China, Guanghan 618307, China
  • Received:2019-03-18 Online:2020-01-28 Published:2020-01-28

摘要: 采用有限元方法,构建了3234/T300B复合材料层合板固化过程的物理模型以及数学模型。对不同对流换热条件下层合板固化时的温度场及热应力场进行了数值模拟。分析了不同对流换热系数对层合板固化阶段的热应力以及固化后残余热应力的影响。结果表明:上表面施加的对流换热系数越大,固化过程升温阶段层合板内部的热应力越小,固化残余热应力显著减小。当施加的对流换热系数由5 W/(m2·K)增大到10 W/(m2·K)时,温度和热应力的下降幅度最大。研究表明通过引入对流换热条件来减小固化过程升温阶段层合板热应力以及固化残余应力是可行的,也为优化热风枪固化方法提供了参数依据。

关键词: 树脂基复合材料, 层合板, 对流换热系数, 热应力

Abstract: The physical model and mathematical model of the cure process of 3234/T300B composite laminates were constructed by finite element method. The solidification temperature field and thermal stress field of laminates under convective heat transfer conditions were numerically simulated. The effects of different convective heat transfer coefficient on the thermal stress during the cure process of the laminate and the residual thermal stress after curing were analyzed. The results show that the larger the convective heat transfer coefficient applied on the upper surface, the smaller the thermal stress inside the laminate during the heating process. And when the convective heat transfer coefficient increases from 5 W/(m2·K) to 10 W/(m2·K), the decline of the temperature and thermal stress is the largest. The research result shows that it is feasible to reduce the thermal stress and solidification residual stress of the laminate during the heating process by introducing convective heat transfer conditions, providing a parameter basis for optimizing the curing method using by air hot gun.

Key words: resin-based composite, laminated plate, convective heat transfer coefficient, thermal stress

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