Excitation characteristics of rotor/stator-interaction flow field and resonant design of bladed disk

LI Lin; MA Hao-ran; WANG Pei-yi

doi:10.13224/j.cnki.jasp.2016.06.012

Chinese

您当前的位置：

首页 >

文章列表页 >

Excitation characteristics of rotor/stator-interaction flow field and resonant design of bladed disk

更新时间：2026-07-07

- Excitation characteristics of rotor/stator-interaction flow field and resonant design of bladed disk
- Vol. 31, Issue 6, Pages: 1368-1376(2016)
- 作者机构：
  
  1. 北京航空航天大学能源与动力工程学院,北京,100191
  2. 先进航空发动机协同创新中心,北京,100191
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2016.06.012
  CLC：
- Published：2016
- 稿件说明：
移动端阅览
李琳, 马浩然, 王培屹. 转静干涉流场的激励特征与叶盘结构的共振设计[J]. 航空动力学报, 2016, 31(6): 1368-1376.

doi: 10.13224/j.cnki.jasp.2016.06.012
李琳, 马浩然, 王培屹. 转静干涉流场的激励特征与叶盘结构的共振设计[J]. 航空动力学报, 2016, 31(6): 1368-1376. DOI： 10.13224/j.cnki.jasp.2016.06.012.

doi: 10.13224/j.cnki.jasp.2016.06.012 DOI：

摘要

在对三维非定常转静干涉流场进行计算与分析的基础上

研究了转静干涉流场对叶盘结构激励的特征

包括尾流激励中的频率成分和空间成分

以及这些特征成分的相对大小. 在此基础上

结合叶盘结构共振条件

总结并提出了从抑制共振的角度确定静子结构周期数的设计原则

即静子结构周期数的确定应使其产生的尾流激励的频率特征中不包含叶盘结构的频率成分

以及空间分布特征中不包含对应该频率模态节径的谐波成分.给出了基于转静干涉流场特征参数估算尾流激励主要频率成分和空间成分的公式

使这一确定静子结构周期数的原则在设计阶段可方便实施.数值分析结果对这种估算公式的合理性进行了验证.结果表明:该公式不需对转静干涉三维非定常流场进行数值模拟

即可对静子结构周期数的合理性(是否会引起共振)做出判断.

Abstract

Based on the computation and analysis of three-dimensional unsteady flow induced by rotor/stator-interaction

the characteristics of flow excitation to bladed disk were studied

including frequency-components and circumferential wave-components in the wake of stator. By combining the resonant condition of bladed disk

a design principle was given for determining the stator-structural period from the view of avoiding resonance

namely

the stator-structural period should ensure that in the wake excitation there was neither modal frequency-component of bladed disk nor circumferential wave-component corresponding to the nodal diameter of the bladed disk. The formula was given to predict frequency-components and circumferential wave-components in wake of stator

making it easier to determinate stator-structural period in design phase. It is shown by numerical analysis that this method can determinate the rationality (inducing the resonance or not) of stator-structural period without need of performing numerical simulation of three-dimensional unsteady flow induced by rotor/stator-interaction.

关键词

Keywords

references

Views

686

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Impact of bow shock on tip leakage flow in counter-rotating compressor

Unsteady aerodynamic characteristics of ducted coaxial propeller unmanned aerial vehicle

Topological optimization of piezoelectric materials on the blades for vibration reduction of bladed disks

Accuracy analysis of unsteady numerical simulation methods for axial flow compressor

Exploration of three-dimensional unsteady model for compressor post-stall under inlet distortion

Related Author

徐强仁

刘智远

项效镕

周小勇

赵庆军

蔡红明

马国梁

李忠新

Related Institution

中国科学院工程热物理研究所中国科学院轻型动力重点实验室

中国科学院大学航空宇航学院

中国科学院工程热物理研究所

南京航空航天大学航空学院

南京理工大学能源与动力工程学院

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰