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

基于接触状态分析的叶冠阻尼评估与改进设计

洪杰 杨鑫 陈璐璐 张大义

洪杰, 杨鑫, 陈璐璐, 等 . 基于接触状态分析的叶冠阻尼评估与改进设计[J]. 北京航空航天大学学报, 2012, 38(5): 681-687.
引用本文: 洪杰, 杨鑫, 陈璐璐, 等 . 基于接触状态分析的叶冠阻尼评估与改进设计[J]. 北京航空航天大学学报, 2012, 38(5): 681-687.
Hong Jie, Yang Xin, Chen Lulu, et al. Damping assessment and improving design of blade shrouds based on contact states[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(5): 681-687. (in Chinese)
Citation: Hong Jie, Yang Xin, Chen Lulu, et al. Damping assessment and improving design of blade shrouds based on contact states[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(5): 681-687. (in Chinese)

基于接触状态分析的叶冠阻尼评估与改进设计

基金项目: 国家自然科学基金资助项目(10577006)
详细信息
  • 中图分类号: V 231.92

Damping assessment and improving design of blade shrouds based on contact states

  • 摘要: 采用基于接触状态分析的干摩擦阻尼结构设计方法,针对某型带冠涡轮叶片进行了阻尼评估与改进设计.接触状态包括接触形式和接触参数,通过接触形式从结构上判断结构设计的合理性;通过接触参数从力学性能上评价叶冠的阻尼效果.对叶片的动力特性、接触状态和振动响应进行综合评估分析,找出叶冠结构设计不足之处,并指出具体的改进措施,使叶冠的接触状态及振动响应得到一定的改善,并找到叶冠弦宽稳定工作范围.接触状态能够细致反映出叶冠工作状态下真实的接触情况,为叶冠结构设计和阻尼效果判定提供了更准确、详尽的参考依据.

     

  • [1] 卢绪祥,黄树红,刘正强,等.汽轮机自带冠叶片碰撞减振的研究现状与发展[J].振动与冲击,2010,29(2):11-16 Lu Xuxiang,Huang Shuhong,Liu Zhengqiang,et al.Impact-damping studies for integral shroud blades of a turbine machinery[J].Journal of Vibration and Shock,2010,29(2):11-16(in Chinese)
    [2] 黄庆南,刘春华,杨养花,等.涡轮叶片锯齿冠结构设计的实践与思考[J].航空发动机,2008,34(2):13-16 Huang Qingnan,Liu Chunhua,Yang Yanghua,et al.Practice and reflection of serrated shroud structural design for turbine blade[J].Aeroengine,2008,34(2):13-16(in Chinese)
    [3] 丛配红,张连祥,刘延毅.航空发动机涡轮转子叶片锯齿形叶冠紧度的最佳选择[J].航空发动机,2000,4:9-12 Cong Peihong,Zhang Lianxiang,Liu Yanyi.The best tightness of serrated shroud for aero-engine turbine blade[J].Aeroengine,2000,4:9-12(in Chinese)
    [4] 黄庆南,申秀丽,田静.涡轮动叶锯齿冠的预扭设计[J].航空发动机,1999,4:1-3 Huang Qingnan,Shen Xiuli,Tian Jing.Pre-twist design of turbine blade serrated shroud[J].Aeroengine,1999,4:1-3(in Chinese)
    [5] 孙立业,王鸣,周柏卓.涡轮叶片叶冠的预扭设计分析[J].航空发动机,2005,31(3):20-22 Sun Liye,Wang Ming,Zhou Baizhuo.Pre-twist design analysis of turbine blade shroud[J].Aeroengine,2005,31(3):20-22(in Chinese)
    [6] Zmitrowicz A.A vibration analysis of a turbine blade system damped by dry friction force[J] .International Journal of Mechanical Science,1981,23(12):741-761
    [7] Yang B D ,Menq C H.Modeling of friction contact and it sapplication to the design of shroud contact[J].Transactions of ASME Journal of Engineering for Gas Turbines and Power,1997,119:958-963
    [8] Yang B D ,Chen J J ,Menq C H.Prediction of resonant response of shrouded blades with three-dimensional shroud constraint[J].Transactions of ASME Journal of Engineering for Gas Turbines and Power,1999,121:523-529
    [9] Shi Yajie,Hong Jie,Shan Yingchun,et al.Forced re-sponse analysis of shrouded blades by an alternating frequency/time domain method //Proceedings of GT2006 ASME Turbo Expo 2006: Power for Land,Sea and Air.Barcelona: ,2006:865-872
    [10] Hong Jie,Chen Lulu,Yang Xin,et al.Design method and experimental investigation based on dynamic response analysis of shrouded turbine blades //Proceedings of the ASME 2008 International Design Engineering Technical Conferences & Computers and Information in Engineering Conference.Berlin: ,2008
  • 加载中
计量
  • 文章访问数:  2444
  • HTML全文浏览量:  229
  • PDF下载量:  499
  • 被引次数: 0
出版历程
  • 收稿日期:  2011-03-07
  • 网络出版日期:  2012-05-30

目录

    /

    返回文章
    返回
    常见问答