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轴流压气机叶排干扰所引起转子叶片的振动应力
引用本文:夏邃勤,吕文林,刘志伟. 轴流压气机叶排干扰所引起转子叶片的振动应力[J]. 工程设计学报, 2001, 28(3): 152-156
作者姓名:夏邃勤  吕文林  刘志伟
作者单位:1. 浙江工业大学机电工程学院
2. 西北工业大学航空发动机与热能动力工程系
摘    要: 轴流压气机中上游导叶排与下游转子叶排相互干扰,这一非定常流动诱发了叶片振动.由此,利用有限元法,对所造成的振动应力进行了数值分析.建立了轴流压气机工程设计中求解作用于叶片非定常气动力的近似方法.讨论了叶型几何和静叶数对叶片振动应力的影响.给出由此所造成的叶片动应力分布图,与实验结果基本接近,得到了有益的结论.

关 键 词:叶排干扰  振动  振动应力  非定常流动  动叶  导叶  尾迹  位流场
文章编号:1006-754(2001)03-0152-05
修稿时间:2001-01-10

Dynamic Stress on Rotor Blades from Row Interactions in an Axial Flow Compressor
XIA Sui-Qin,L,Uuml,Wen-Lin,LIU Zhi-Wei. Dynamic Stress on Rotor Blades from Row Interactions in an Axial Flow Compressor[J]. Journal of Engineering Design, 2001, 28(3): 152-156
Authors:XIA Sui-Qin    Wen-Lin  LIU Zhi-Wei
Affiliation:1.Department of Electromechanical Engineering, Zhejiang University of Technology,Hangzhou 310014, China;
 2.Department of Aeroengine and Thermopower Engineering,Northwestern Polytechnical University, Xi' an 710072, China
Abstract:We investigated the impact of interaction of downstream rotor blade row with upstream guided vane row, i.e., interactions of wake and potential flow field, in a single stage axial flow compressor, on vibrations of rotor blades due to the unsteady flow induced by the interaction. With the help of FEM, numerical simulations have been carried out with some correlated factors, such as the geometry of vane profile, the number of guided vanes and so on, in affecting dynamic stress distributions in the rotor blades. An approximate method was given out to compute unsteady flow forces, acting on the rotor blades for compressor designers. Finally, dynamic stress distribution diagrams were illustrated for an example case. The comparison between the computed results and the measurement qualitatively came closer. Some useful conclusions have been obtained.
Keywords:interaction of blades rows  vibrations  dynamic stress  unsteady flow  guided vane  rotor blade  wake  potential flow field
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