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基于晶体塑性的涡轮盘短裂纹扩展模拟方法

张凭 陆山 景鑫 杨茂 罗忠兵 周荣欣

张凭, 陆山, 景鑫, 杨茂, 罗忠兵, 周荣欣. 基于晶体塑性的涡轮盘短裂纹扩展模拟方法[J]. 航空动力学报, 2022, 37(4): 684-693. doi: 10.13224/j.cnki.jasp.20210230
引用本文: 张凭, 陆山, 景鑫, 杨茂, 罗忠兵, 周荣欣. 基于晶体塑性的涡轮盘短裂纹扩展模拟方法[J]. 航空动力学报, 2022, 37(4): 684-693. doi: 10.13224/j.cnki.jasp.20210230
ZHANG Ping, LU Shan, JING Xin, YANG Mao, LUO Zhongbing, ZHOU Rongxin. Simulation method of short crack propagation in turbine disks based on crystal plasticity[J]. Journal of Aerospace Power, 2022, 37(4): 684-693. doi: 10.13224/j.cnki.jasp.20210230
Citation: ZHANG Ping, LU Shan, JING Xin, YANG Mao, LUO Zhongbing, ZHOU Rongxin. Simulation method of short crack propagation in turbine disks based on crystal plasticity[J]. Journal of Aerospace Power, 2022, 37(4): 684-693. doi: 10.13224/j.cnki.jasp.20210230

基于晶体塑性的涡轮盘短裂纹扩展模拟方法

doi: 10.13224/j.cnki.jasp.20210230
基金项目: 国家留学基金委(201806290092)
详细信息
    作者简介:

    张凭(1993-),男,博士,主要从事镍基高温合金裂纹模拟及晶体塑性理论研究。E-mail:pzhang@mail.nwpu.edu.cn

    通讯作者:

    陆山(1955-),男,教授、博士生导师,博士,主要从事航空发动机结构强度、振动及可靠性研究。E-mail:shanlu@nwpu.edu.cn

  • 中图分类号: V232.3

Simulation method of short crack propagation in turbine disks based on crystal plasticity

  • 摘要: 针对低周疲劳载荷下发动机涡轮盘早期短裂纹扩展行为,提出适用于工程结构的耦合晶体塑性(CP)理论和扩展有限元方法(XFEM)的多晶短裂纹模拟方法。该方法采用晶体内总累积分解切应变作为裂纹扩展判据并使裂纹沿最活跃滑移系对应的滑移平面传播。框架采用子模型技术/分区域网格细化以及宏-介观本构结合的方法解决真实工程结构和微观模型尺度不匹配的问题,在可接受的计算代价下预测了涡轮盘危险截面处的短裂纹扩展路径及速率。结果表明该结构内早期裂纹生长路径及速率受到晶体取向的影响而出现较大分散性,同时验证了基于CP-XFEM的框架在预测工程结构短裂纹扩展寿命及分散性上的可行性。

     

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出版历程
  • 收稿日期:  2021-05-11
  • 刊出日期:  2022-04-28

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