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等离子涂层典型界面损伤与破坏的数值模拟

魏洪亮 杨晓光 齐红宇

魏洪亮, 杨晓光, 齐红宇等 . 等离子涂层典型界面损伤与破坏的数值模拟[J]. 北京航空航天大学学报, 2007, 33(10): 1141-1145.
引用本文: 魏洪亮, 杨晓光, 齐红宇等 . 等离子涂层典型界面损伤与破坏的数值模拟[J]. 北京航空航天大学学报, 2007, 33(10): 1141-1145.
Wei Hongliang, Yang Xiaoguang, Qi Hongyuet al. Numerical simulation of damage and fracture on typical interfaces of plasma sprayed thermal barrier coatings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1141-1145. (in Chinese)
Citation: Wei Hongliang, Yang Xiaoguang, Qi Hongyuet al. Numerical simulation of damage and fracture on typical interfaces of plasma sprayed thermal barrier coatings[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1141-1145. (in Chinese)

等离子涂层典型界面损伤与破坏的数值模拟

详细信息
    作者简介:

    魏洪亮(1978-),男,辽宁阜新人,博士生,buaawhl@163.com.

  • 中图分类号: V 254.2; TB 125

Numerical simulation of damage and fracture on typical interfaces of plasma sprayed thermal barrier coatings

  • 摘要: 基于界面损伤力学思想,提出了三结点界面单元的概念,和传统界面单元相比,具有能够表征任意形状界面法线方向的优点,将改进的单元通过ABAQUS的用户子程序UEL与有限元软件进行了结合.考虑等离子涂层界面粗糙度的影响,模拟了余弦形界面在热循环载荷下的损伤以及在拉伸载荷下的破坏过程.计算结果表明,界面单元结点间位移出现不连续现象,体现了裂纹的逐渐张开过程,界面损伤随热循环次数的增加而增加,其中第一个循环造成的损伤最大,波峰处是界面断裂的危险位置,法向分离起主导作用;等离子涂层粗糙界面承受法向拉伸载荷的能力较平直界面显著增加.采用改进的界面单元模拟异质材料复杂形状界面的损伤与破坏是可行的,结果是合理的.

     

  • [1] Gang Qian. Fracture analysis and microstructural modeling of thermal spray coatings . New York: School of Mechanical Engineering, State University of New York, USA, 1999 [2] Chaboche J L, Feyel F, Monerie Y. Interface debonding models: a viscous regularization with a limited rate dependency[J]. International Journal of Solids and Structures, 2001, 38: 3127-3160 [3] Needleman A. A continuum model for void nucleation by inclusion debonding[J]. J Appl Mech, 1987, 54: 525-531 [4] Tvergaard V. Effect of fibre debonding in a whisker-reinforced metal[J]. Mater Sci Engng A , 1990a, 125: 203-213 [5] Lemaitre J. A course on damage mechanics[M]. Berlin: Springer, 1992 [6] Chandra N, Li H, Shet C, et al. Some issues in the application of cohesive zone models for metal-ceramic interfaces[J]. International Journal of Solids and Structures, 2002, 39: 2827-2855 [7] 牛鑫瑞, 余寿文, 冯西桥. 含圆形夹杂两相材料界面变形与损伤特性的数值模拟[J]. 机械强度, 2005, 27(5): 681-686 Niu Xinrui, Yu Shouwen, Feng Xiqiao. Numerical simulation of interfacial deformation and damage for a dual-phase composite with a circular cylindrical inclusion[J]. Journal of Mechanical Strength, 2005, 27(5): 681-686(in Chinese) [8] 周储伟, 杨卫, 方岱宁. 内聚力界面单元与复合材料的界面损伤分析[J]. 力学学报, 1999, 31(3): 372-377 Zhou Chuwei, Yang Wei, Fang Daining. Cohesive interface element and interfacial damage analysis of composites[J]. Acta Mechanica Sinica, 1999, 31(3): 372-377 (in Chinese) [9] Chaboche J L, Girard R, Levasseur P. On the interface debonding models[J]. International Journal of Damage Mechanics, 1997b, 6: 220-257 [10] Xie Wangang, Walker K P, Jordan E H, et al. Implementation of a viscoplastic model for a plasma sprayed ceramic thermal barrier coating[J]. J Eng Mater Technol, 2003, 125: 200-207 [11] 耿瑞. 热障涂层强度分析及寿命预测研究 . 北京: 北京航空航天大学能源与动力工程学院, 2001 Geng Rui. Strength analysis and life prediction study on thermal barrier coatings . Beijing : School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, 2001 ( in Chinese) [12] Evans A G, Mumm D R, Hutchinson J W, et al. Mechanisms controlling the durability of thermal barrier coatings[J]. Progress in Materials Science, 2001, 46: 505-553 [13] Caliez M, Chaboche J L, Feyel F, et al. Numerical simulation of EBPVD thermal barrier coatings spallation[J]. Acta Materialia, 2003, 51: 1133-1141
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出版历程
  • 收稿日期:  2006-10-13
  • 刊出日期:  2007-10-31

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