不同叶顶间隙下压气机旋转不稳定性特性

doi:10.16183/j.cnki.jsjtu.2020.03.006

上海交通大学学报 ›› 2020, Vol. 54 ›› Issue (3): 265-276.doi: 10.16183/j.cnki.jsjtu.2020.03.006

不同叶顶间隙下压气机旋转不稳定性特性

赖生智a，吴亚东b,c，田杰b,c，欧阳华b,c

上海交通大学 a. 航空航天学院； b. 机械与动力工程学院; c. 燃气轮机与民用航空发动机教育部工程研究中心, 上海 200240

出版日期:2020-03-28 发布日期:2020-04-09
通讯作者: 吴亚东，副研究员，电话（Tel.）:13564311521；E-mail: yadongwu@sjtu.edu.cn.
作者简介:赖生智（1994-），男，四川省资阳市人，硕士生，主要从事压气机气动不稳定性研究.
基金资助:
国家自然科学基金（11202132），上海市自然科学基金(18ZR1418600)，国防基础科研计划(B1420110136)资助项目

Rotating Instability Characteristics in Compressor with Different Tip Clearances

LAI Shengzhi a，WU Yadong b,c，TIAN Jie b,c，OUYANG Hua b,c

a. School of Aeronautics and Astronautics; b. School of Mechanical Engineering; c. Engineering Research Center of Gas Turbine and Civil Aero Engine, Ministry of Education, Shanghai Jiao Tong University, Shanghai 200240, China

Online:2020-03-28 Published:2020-04-09

摘要/Abstract

摘要： 采用全通道数值计算方法对一台单级低速轴流压气机旋转不稳定性(RI)特性进行分析，研究了4种叶顶间隙条件下RI的频率特性、模态特性和流场特性的变化及原因.采用相干分析方法得到相邻叶片通道内同角度位置压力信号相干函数和互功率谱，显示产生RI流动的通道涡结构在周向的传播特性.空间模态分解和旋转源机理分析得到RI的周向模态特性，影响RI通道涡结构的脉动和旋转特性及其在绝对和相对坐标系下的关系.结果表明：随着叶顶间隙的减小，叶顶流动强度减弱，RI现象强度逐渐减弱，主模态阶数增大.

关键词: 旋转不稳定性（RI）；数值模拟；叶顶间隙流动；旋转源机理；周向模态

Abstract: Rotating instability (RI) characteristics of a single stage low speed compressor are analyzed by full channel numerical calculation method. Variations and the reasons of frequency characteristics, modes characteristics and flow characteristics of RI under four different tip clearances are investigated. The coherence analysis method is used to obtain the coherent function and the mutual power spectrum of the pressure signal at the same angle in the adjacent blade channel, which show the propagation characteristics of the channel vortex structure with flow in the circumferential direction. The circumferential modal characteristics of RI, the pulsating and rotating characteristics of channel vortex structures affecting RI as well as its relationship in absolute and relative coordinate systems are obtained by spatial mode decomposition and rotation source mechanism analysis. Results show that with the decrease of tip clearance, the flow intensity of tip clearance decreases, the intensity of RI gradually decreases, and the order of main modes increases.

Key words: rotating instability (RI); numerical simulation; tip clearance flow; rotating source mechanism; circumferential mode

中图分类号:

V 231.3

赖生智，吴亚东，田杰，欧阳华. 不同叶顶间隙下压气机旋转不稳定性特性[J]. 上海交通大学学报, 2020, 54(3): 265-276.

LAI Shengzhi，WU Yadong，TIAN Jie，OUYANG Hua. Rotating Instability Characteristics in Compressor with Different Tip Clearances[J]. Journal of Shanghai Jiaotong University, 2020, 54(3): 265-276.

参考文献

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不同叶顶间隙下压气机旋转不稳定性特性

Rotating Instability Characteristics in Compressor with Different Tip Clearances

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