期刊文献+

基于非线性谐波法评估压气机转静干涉诱发的强迫响应 被引量:2

Evaluating of the Forcing Response under Compressor Stator-Rotor Interaction Using NLH
下载PDF
导出
摘要 针对压气机转静干涉诱发的强迫响应问题,对某型风扇试验件进口可变弯度导向叶片进行流固耦合数值模拟。基于NUMECA的非线性谐波法,求解在后排转子势流作用下可调导叶的非定常流场,从而获得谐波压力,并对其作用在前排可调导叶相应模态下的强迫响应进行了计算,与试验验证结果吻合。结果表明:基于非线性谐波法的流场计算以及强迫响应分析,为工程应用建立了转静干涉诱发强迫振动响应的数值评估方法。 Aiming at the forcing response of compressor stator-rotor interaction, the numerical fluid-solid coupling simulation of the fan pivoting-stator were performed. Based on the nonlinear harmonic method in NUMECA, the unsteady flow field of the variable guide vane was solved under the potential flow effect of back row rotors. With the achieved harmonic pressure on the variable guide vane, the forcing response under the corresponding model was predicted. These results are in agreement with those obtained from experiments. The results show that an engineering numerical method of evaluating the forcing response under stator-rotor interaction was achieved based on the nonlinear harmonic simulation in the flow field and forcing response analysis.
出处 《航空发动机》 2015年第2期40-44,共5页 Aeroengine
基金 国家重大基础研究项目资助
关键词 压气机 转静干涉 非线性谐波法 强迫响应 流固耦合 航空发动机 compressor stator-rotor interaction NLH forcing response fluid-solid coupling aeroengine
  • 相关文献

参考文献14

  • 1Sander A J, Fleeter S. Blading response to potential field interactions in axial and radial flow turbomachinery [J]. Journal of Propulsion and Power, 1998,14(2) : 199-207.
  • 2Le Y T, Feng J Z. Potential and viscous interactions for a muhi- blade row compressor[C]//ASME Turbo Expo 2003, Collocaled with the 2003 International Joint Power Generation Conference, USA: AmericanSociety of Mechanical Engineers, 2003.
  • 3Bjorn Laumert, Hans Marlensson. Investigation of unsteady aerodynamic blade excitation mechanisms in a transonic turbine stage, Part l:phe- nomenological identification and classification [J]. Journal of Turboma- chinery, 2002,124 ( 3 ) : 410-418.
  • 4Wei Ning, StuartM. Blade forced response prediction for industrial gas turbines-Part2: verification and application [C]//ASME Turho Expo 2003,Collatt with the 2003 International Joint Power Generation Conference, USA:American Society of Mechanical Engineers, 2003.
  • 5王梅,江和甫,吕文林.在尾流激振情况下叶片振动应力预估技术[J].航空动力学报,2007,22(4):608-613. 被引量:33
  • 6孟越,李琳,李其汉.尾流激振情况下叶片强迫响应瞬态分析方法[J].北京航空航天大学学报,2006,32(6):671-674. 被引量:22
  • 7孟越,李琳,李其汉.不对称静子尾迹流场激振力分析及计算方法[J].北京航空航天大学学报,2007,33(9):1005-1008. 被引量:6
  • 8李润泽,李琳.跨声速工况下流体诱发叶片振动研究[J].航空动力学报,2008,23(4):747-753. 被引量:7
  • 9Du Pengcheng,Ning Fangfei. Application of the harmonic balance method in simulating almost periodic turbomaehinery flows [R]. ASME 2014-GT-25457.
  • 10Ning F, Xu L. Numerical investigation of transonic compressor rotor flow using an implicit 3D flow solver with one-equation spalart-all- maras turbulence model[R]. ASME 2001-GT-0359.

二级参考文献17

  • 1孟越,李琳,李其汉.尾流激振情况下叶片强迫响应瞬态分析方法[J].北京航空航天大学学报,2006,32(6):671-674. 被引量:22
  • 2沈达宽,欧阳绍泽,陈群.燃气涡轮发动机不均匀导流叶栅及其尾迹对工作叶片的振动分析和计算[R].西安:西北工业大学,1985.
  • 3Stuart M,Li He.Blade forced response prediction for industrial gas turbines part 1:methodologies[C]//Proceedings of the ASME Turbo Expo 2003.Volume 4:Oil and Gas Applications,Structures and Dynamics.[S.L]:ASME,2003:407-414
  • 4Wei Ning,Stuart M,Li Yansheng,et al.Blade forced response prediction for industrial gas turbines part 2:verification and application[C]// Proceedings of the ASME Turbo Expo 2003.Volume 4:Oil and Gas Applications,Structures and Dynamics.[S.L]:ASME,2003:415-422
  • 5王梅,江和甫,吕文林,在尾流激振情况下叶片振动应力预估技术[C]//中国航空学会动力分会发动机结构强度与振动专业委员会第十二届学术会议论文集.四川:青城山,2004:484-490
  • 6祈明旭,丰镇平,KANG Shun,等,轴流透平级动静干涉的非定常效应及其对气动性能的影响[C]//工程热物理学会热机气动热力学学术会议论文集.中山:中国工程热物理学会,2002:395-401
  • 7Rivas-Guerra A J, Mignolet M P. Local/global effects of mistuning on the forced response of bladed disks [ J]. Journal of Engineering for Gas Turbines and Power, 2004, 126( 1 ) : 131 - 141.
  • 8Lim Sang-Ho, Christophe P, Castanier Matthew P. Predicting blade stress levels directly from reduced-order vibration models of mistuned bladed disks [J]. Journal of Turbo Machinery, 2006, 128(1): 206-210.
  • 9Gottfried Dana A, Fleeter S. Passive detuning for HCF reduction [ R ]. AIAA 2002-3634,2002.
  • 10夏邃勤,吕文林.尾迹激振与旋转失速航空发动机设计手册(第十八分册)[M].北京:航空工业出版社,1996.

共引文献49

同被引文献20

引证文献2

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部