留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

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.

     

  • [1] Vargiu P,Firrone C M,Zucca S,et al.A reduced order model based on sector mistuning for the dynamic analysis of mistuned bladed disks[J].International Journal of Mechanical Sciences,2011,53(8):639-646.
    [2] 王建军,李其汉,朱梓根.失谐叶片-轮盘结构系统振动局部化问题的研究进展[J].力学进展,2000,30(4):517-528. WANG Jianjun,LI Qihan,ZHU Zigen.Vibratory localization of mistuned bladed disk assemblies a review[J].Advances in Mechanics,2000,30(4):517-528.(in Chinese)
    [3] 廖海涛,王建军,李其汉.随机失谐叶盘结构失谐特性分析[J].航空动力学报,2010,25(1):160-168. LIAO Haitao,WANG Jianjun,LI Qihan.Mistuning characteristics analysis of mistuned bladed disk assemblies[J].Journal of Aerospace Power,2010,25(1):160-168.(in Chinese)
    [4] 白斌,白广忱,童晓晨,等.整体叶盘结构失谐振动的国内外研究状况[J].航空动力学报,2014,29(1):91-103. BAI Bin,BAI Guangchen,TONG Xiaochen,et al.Research on vibration problem of integral mistuned balded disk assemblies at home and abroad[J].Journal of Aerospace Power,2014,29(1):91-103.(in Chinese)
    [5] 王红建.复杂耦合失谐叶片-轮盘系统振动局部化问题研究[D].西安:西北工业大学,2006. WANG Hongjian.Investigation of the vibration localization problem of the mistuned bladed disk with complicated coupling[D].Xi'an:Northwestern Polytechnical University,2006.(in Chinese)
    [6] Petrov E P,Haftka R T.Optimization of mistuned bladed discs using gradient-based response surface approximations[R].AIAA-2000-1522,2000.
    [7] Choi B K.Pattern optimization of intentional blade mistuning for the reduction of the forced response using genetic algorithm[J].Journal of Mechanical Science and Technology,2003,17(7):966-977.
    [8] Choi W,Storer R H.Heuristic algorithms for a turbine-blade-balancing problem[J].Computers and Operations Research,2004,31(8):1245-1258.
    [9] Bendiksen O O.Localization phenomena instructural dynamics[J].Chaos,Solitons and Fractals,2000,11(10):1621-1660.
    [10] Scarselli G,Lecce L,Castorini E.Mistuning effects evaluation on turbomachine dynamic behaviour using genetic algorithms[J].International Journal of Acoustics and Vibration,2011,16(4):191-196.
    [11] 袁惠群,张亮.基于蚁群算法的航空发动机失谐叶片减振排布优化分析[J].振动与冲击,2012,31(11):169-172. YUAN Huiqun,ZHANG Liang.Optimization of mistuning blades arrangement for vibration absorption in an aero-engine based on artificial ant colony algorithm[J].Journal of Vibration and Shock,2012,31(11):169-172.(in Chinese)
    [12] 袁惠群,杨少明.基于蚁群算法和模态局部化参数的失谐叶盘减振研究[J].东北大学学报:自然科学版,2010,31(11):1611-1614. YUAN Huiqun,YANG Shaoming.Vibration reduction of mistuned blade disc by ant colony algorithm and modal localization parameter[J].Journal of Northeastern University:Natural Science,2010,31(11):1611-1614.(in Chinese)
    [13] 袁惠群,张亮.航空发动机转子失谐叶片减振安装优化分析[J].振动、测试与诊断,2011,31(5):647-651. YUAN Huiqun,ZHANG Liang.Optimization analysis on mistuning blades of vibration absorption in aero-engine[J].Journal of Vibration,Measurement and Diagnosis,2011,31(5):647-651.(in Chinese)
    [14] 鞠鹏飞,宁方飞.GPU平台上的叶轮机械CFD加速计算[J].航空动力学报,2014,29(5):1154-1162. JU Pengfei,NING Fangfei.Accelerated CFD computing of turbomachinery on GPU platform[J].Journal of Aerospace Power,2014,29(5):1154-1162.(in Chinese)
    [15] 白洪涛.基于GPU的高性能并行算法研究[D].长春:吉林大学,2010. BAI Hongtao.Research on high performance parallel algorithms based on GPU[D].Changchun:Jilin University,2010.(in Chinese)
    [16] 王红建,贺尔铭,余仕侠.具有干摩擦散乱失谐的叶盘受迫响应特性[J].航空动力学报,2006,21(4):711-715. WANG Hongjian,HE Erming,YU Shixia.Forced response characteristics of bladed disks with disordered dry friction[J].Journal of Aerospace Power,200621(4):711-715.(in Chinese)
    [17] 徐自力,常东锋,上官博.微滑移离散模型及在干摩擦阻尼叶片振动分析中的应用[J].机械科学与技术,2007,26(10):1304-1307. XU Zili,CHANG Dongfeng,SHANGGUAN Bo.One barmicroslip discrete model and its application to vibration analysis of blade with dry friction damper[J].Mechanical Science and Technology for Aerospace Engineering,2007,26(10):1304-1307.(in Chinese)
    [18] 辛振铭.一种改进的模拟退火算法在TSP问题中的研究与应用[D].长春:东北师范大学,2010. XIN Zhenming.The imprived simulated annealing algorithm research and application based on TSP[D].Changchun:Northeast Normal University,2010.(in Chinese)
    [19] Kirkpatrick S.Optimization by simulated annealing[J].Science,1983,220(4598):671-680.
    [20] Czapiński M.An effective parallel multistart tabu search for quadratic assignment problem on CUDA platform[J].Journal of Parallel and Distributed Computing,2013,73(11):1461-1468.
  • 加载中
计量
  • 文章访问数:  918
  • HTML浏览量:  2
  • PDF量:  647
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-07-30
  • 刊出日期:  2016-05-28

目录

    /

    返回文章
    返回