玻璃钢/复合材料 ›› 2018, Vol. 0 ›› Issue (10): 39-46.

• 基础研究 • 上一篇    下一篇

不同修补工艺下的大厚度树脂基复合材料修补片热应力

陈淑仙, 田秋实, 包正弢, 顾威   

  1. 中国民用航空飞行学院航空工程学院,广汉618307
  • 收稿日期:2018-04-18 出版日期:2018-10-28 发布日期:2018-10-28
  • 作者简介:陈淑仙(1975-),女,博士,教授,主要从事复合材料固化过程工艺方面的研究,bellesavana@163.com。
  • 基金资助:
    国家自然科学基金民航联合基金重点项目(U1233202,U1333201);国家自然科学基金(51306201)

THE THERMAL STRESS OF THICK-SECTIONED RESIN MATRIX COMPOSITES PATCHES AT DIFFERENT REPAIRING PARAMETERS

CHEN Shu-xian, TIAN Qiu-shi, BAO Zheng-tao, GU Wei   

  1. Aviation Engineering Institute, Civil Aviation Flight University of China, Guanghan 618307, China
  • Received:2018-04-18 Online:2018-10-28 Published:2018-10-28

摘要: 建立了大厚度碳纤维复合材料修补片与母板共固化的有限元数学模型和计算方法,并采用已有实验结果验证了数学模型和计算方法的正确性。计算了修补片与母板共固化过程中的温度、固化度及热应力变化过程,研究了挖补斜度、纤维铺层方向、纤维铺层顺序等修补工艺参数对修补片固化过程中不同阶段温度及热应力场分布的影响。研究结果表明,挖补斜度对于升温和保温阶段修补片内的热应力影响较大,对于降温结束后的修补片热应力影响较弱。增大挖补斜度,可减小大厚度修补片升温和保温过程的热应力,也可避免较大的热应力集中。在整个固化过程中,0°铺层角对应的修补片内的残余热应力最小,90°铺层角对应的修补片内的残余热应力最大,且在修补片顶部中心有较强的应力集中。为了减小残余热应力,纤维的排布方向应平行于修补片与母板接触面,即母板的铺层方向。对称铺层的修补片在整个固化过程中的热应力较小,而顺序间隔铺层和反对称铺层的修补片内热应力较大,大厚度树脂基复合材料修补片应采用对称的铺层设计原则。

关键词: 挖补修理, 工艺参数, 大厚度树脂基复合材料, 温度场, 热应力

Abstract: The finite element method is used to simulate the varying process of temperature, curing degree and thermal stress in the co-curing process of thick-sectioned resin matrix composite patch with mother board, and the correctness of the numerical methodology is verified by comparison with the experimental results. The effects of scarf slope, fiber orientation and fiber layup order on distributions of temperature and thermal stress field in patch at different stages during curing process are studied. The results show that the slope of scarf has a great influence on the thermal stress in the patch during the heating and isothermal stages, and has little effect on the thermal stress of the patch at the end of cooling. Increasing the scarf slope can reduce the thermal stress of the patch during the heating and isothermal stages, and can also avoid large thermal stress concentration. During the whole curing process, the residual thermal stress in the patches is the smallest with 0° fiber orientation while the value is the largest with 90° fiber orientation, and there is a strong stress concentration at the center of the top of the patches corresponding to the latter one. In order to reduce the residual thermal stress, the orientation of the fibers should be parallel to the contact surface of the patch with the motherboard, i.e. perpendicular to the direction constrained by the motherboard. Symmetric ply patches have less thermal stress throughout the curing process, while thermal stresses are greater in the patches with sequential spacer plies and anti-symmetric plies. Symmetry ply design principles should be used for resin matrix composites patch plies.

Key words: scarf repair, process parameters, thick-sectioned resin matrix composites, temperature field, thermal stress

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