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非线性摩擦失谐叶片排序并行退火算法

赵天宇 袁惠群 杨文军 张宏远

赵天宇, 袁惠群, 杨文军, 张宏远. 非线性摩擦失谐叶片排序并行退火算法[J]. 航空动力学报, 2016, 31(5): 1053-1064. doi: 10.13224/j.cnki.jasp.2016.05.005
引用本文: 赵天宇, 袁惠群, 杨文军, 张宏远. 非线性摩擦失谐叶片排序并行退火算法[J]. 航空动力学报, 2016, 31(5): 1053-1064. doi: 10.13224/j.cnki.jasp.2016.05.005
ZHAO Tian-yu, YUAN Hui-qun, YANG Wen-jun, ZHANG Hong-yuan. Mistuned blade arrangement with non-linear friction based on parallel annealing algorithm[J]. Journal of Aerospace Power, 2016, 31(5): 1053-1064. doi: 10.13224/j.cnki.jasp.2016.05.005
Citation: ZHAO Tian-yu, YUAN Hui-qun, YANG Wen-jun, ZHANG Hong-yuan. Mistuned blade arrangement with non-linear friction based on parallel annealing algorithm[J]. Journal of Aerospace Power, 2016, 31(5): 1053-1064. doi: 10.13224/j.cnki.jasp.2016.05.005

非线性摩擦失谐叶片排序并行退火算法

doi: 10.13224/j.cnki.jasp.2016.05.005
基金项目: 

国家自然科学基金重点项目(51335003)

国家自然科学基金(51275081)

辽宁省科技创新重大专项课题(201303004)

沈阳市科技计划高新技术产业发展与科技攻关计划项目(F13-01-21-00)

详细信息
    作者简介:

    赵天宇(1989-),男,辽宁鞍山人,博士生,主要研究方向为转子动力学.

  • 中图分类号: V23

Mistuned blade arrangement with non-linear friction based on parallel annealing algorithm

  • 摘要: 基于叶片模态实验获得的叶片失谐参数,基于非线性摩擦阻尼分析提出一种失谐叶盘结构的集中参数模型.综合模拟退火算法的局部搜索能力和遗传算法的全局搜索能力,并引入禁忌表作为搜索记忆表,提出了一种应用模拟退火进化算法附加禁忌表的叶片排序优化方法.同时结合图形处理器运算设计了基于compute unified device architecture(CUDA)的并行算法并且分析其算法性能.研究表明:基于并行框架寻优可以获得4.5倍的加速,同时按照优化后方案安装,可以明显降低叶盘系统振动响应幅值与方差.

     

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出版历程
  • 收稿日期:  2014-07-30
  • 刊出日期:  2016-05-28

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