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

基于接触状态分析的叶冠阻尼评估与改进设计

北京航空航天大学能源与动力工程学院, 北京 100191

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
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出版历程
- 收稿日期: 2011-03-07
- 网络出版日期: 2012-05-30

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

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

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.
- 干摩擦阻尼 /
- 锯齿形叶冠 /
- 接触状态 /
- 阻尼评估 /
- 改进设计
Abstract: Damping assessment and improving design of a certain type of shrouded blades were conducted by applying the damping design method of sawtooth shroud based on contact states. Contact states included contact forms and contact parameters, in which contact forms could be used to judge the rationality of structure design; while contact parameters could be applied to evaluate the damping effect according to their mechanical properties. By generally assessing and analyzing the dynamic characteristics, contact states and dynamic response of the blade, the deficiencies of shroud structure design were found, and then the optimization measures which contributed to improve the contact states and dynamic response of the shroud were also proposed, also the stable operation range of chord width was obtained. The contact states could reflect the real contact conditions of shrouds when they are working, which can be regarded as a more accurate and detailed criterion for designing shroud structure and judging damping effects.
- dry friction damping /
- sawtooth shroud /
- contact states /
- damping assessment /
- improving design

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参考文献(10)

[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