高压比离心压气机串列叶轮内部流动机理研究

推进技术 ›› 2017, Vol. 38 ›› Issue (10): 2393-2400.

• 研究论文 • 上一篇

高压比离心压气机串列叶轮内部流动机理研究

李紫良^1,2,卢新根¹,张燕峰¹,韩戈¹,韩建涛^1,2,朱俊强¹

中国科学院工程热物理研究所/轻型动力重点实验室，北京 100190; 中国科学院大学，北京 100049,中国科学院工程热物理研究所/轻型动力重点实验室，北京 100190,中国科学院工程热物理研究所/轻型动力重点实验室，北京 100190,中国科学院工程热物理研究所/轻型动力重点实验室，北京 100190,中国科学院工程热物理研究所/轻型动力重点实验室，北京 100190; 中国科学院大学，北京 100049,中国科学院工程热物理研究所/轻型动力重点实验室，北京 100190

发布日期:2021-08-15
作者简介:李紫良，男，博士生，研究领域为叶轮机械气动热力学。
基金资助:
国家自然科学基金(51476166)。

Mechanism of Highly-Loaded Centrifugal Compressor Stage with Tandem Impeller

Key Laboratory of Light-Duty Gas-Turbine，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China; University of Chinese Academy of Sciences，Beijing 100049，China,Key Laboratory of Light-Duty Gas-Turbine，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China,Key Laboratory of Light-Duty Gas-Turbine，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China,Key Laboratory of Light-Duty Gas-Turbine，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China,Key Laboratory of Light-Duty Gas-Turbine，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China; University of Chinese Academy of Sciences，Beijing 100049，China and Key Laboratory of Light-Duty Gas-Turbine，Institute of Engineering Thermophysics， Chinese Academy of Sciences，Beijing 100190，China

Published:2021-08-15

摘要/Abstract

摘要： 为了探索串列叶轮的设计方法和实际应用，在常规离心叶轮的基础上，利用轴流压气机和离心叶片设计方法实现了串列叶轮设计，借助经过校核的数值模拟手段，对带串列叶轮的离心压气机内部流动进行了详细数值模拟，研究了诱导轮和导风轮之间相对周向位置对串列叶轮内部流场及气动性能的影响。研究表明:串列叶轮的引入能够不同程度改善离心压气机性能，且诱导轮与导风轮之间的相对周向位置对气动性能具有较大的影响，在[λs]=25%周向相对位置下，串列叶轮的引入使得压气机级综合裕度和峰值效率分别提高了1.3%和1.4%。与常规叶轮相比，合理布局的串列叶轮能够有效控制离心叶轮内部附面层的发展并改善离心叶轮内部流场特性以及离心叶轮出口流场品质，从而有效提高高压比离心压气机的性能和稳定工作裕度。

关键词: 高压比离心压气机；串列叶轮；周向相对位置；数值模拟

Abstract: In order to advance the understanding of the fundamental mechanism of tandem impeller， a highly loaded centrifugal compressor stage with impeller of conventional design and various tandem clocking designs was investigated at design speed numerically. The tandem impeller was designed using advanced axial compressor cascade and ruled surface impeller design methods based on a conventional impeller. Comparison and analysis for the performance and flow field between different impeller configurations showed that tandem design and clocking position had great influence on the performance of compressor. The tandem-impeller compressor with 25% clocking fraction increases the stall margin and peak efficiency by 1.3% and 1.4%， respectively. Appropriate tandem design can inhibit the boundary layer development and improve of the non-uniform flow field at impeller outlet， both of which contributed to the gain of the efficiency and stall margin of centrifugal compressor.

Key words: Highly-loaded centrifugal compressor；Tandem impeller；Clocking arrangement；Numerical simulation

李紫良,卢新根,张燕峰,韩戈,韩建涛,朱俊强. 高压比离心压气机串列叶轮内部流动机理研究[J]. 推进技术, 2017, 38(10): 2393-2400.

LI Zi-liang^1,2,LU Xin-gen¹,ZHANG Yan-feng¹,HAN Ge¹,HAN Jian-tao^1,2,ZHU Jun-qiang¹. Mechanism of Highly-Loaded Centrifugal Compressor Stage with Tandem Impeller[J]. Journal of Propulsion Technology, 2017, 38(10): 2393-2400.

参考文献

[1] 方昌德. 高性能涡轮发动机技术综合计划(IHPTET)跟踪研究[C]. 北京:第四代背景机技术研讨会,1996.
[2] 梁春华. 通用的,可承担起的先进涡轮发动机 (VAATE) 计划[J]. 航空发动机, 1996, 27(3): 42-42.
[3] Josuhn-Kadner B, Hoffmann B. Investigations on a Radial Compressor Tandem-Rotor Stage with Adjustable Geometry [R]. ASME 92-GT-218.
[4] Josuhn-Kadner B. Flow Field and Performance of a Centrifugal Compressor Rotor with Tandem Blades of Adjustable Geometry[R]. ASME 94-GT-13.
[5] Roberts D A, Kacker S C. Numerical Investigation of Tandem-Impeller Designs for a Gas Turbine Compressor [R]. ASME 2001-GT-324.
[6] Rodrigo R Erdmenger, Vittorio Michelassi. Influence of Tandem Inducers on the Performance of High Pressure Ratio Centrifugal Compressor[R]. ASME 2015-GT-43001.
[7] 季路成, 陈江. 从IHPTET到VAATE的技术方向探析[C]. 杭州:中国工程热物理学会年会热机气动热力学学术会议, 2005.
[8] Bammert K, Staude R. New Features in the Design of Axial Flow Compressors with Tandem Blades[R]. ASME Paper, 81-GT-113, 1981.
[9] Japikse D, Garcia R. Overview of Industrial and Rocket Turbopump Inducer Design[EB/OL]. http://resolver.caltech.edu/cav 2001: sessionB7.001., 2001.
[10] Klassen H A, Wood J R, Schumann L F. Experimental Performance of a 13.65cm-Tip-Diameter Tandem Bladed Sweptback Centrifugal Compressor Designed for a Pressure Ratio of 6 [R]. NASA TP-1091. 1977.
[11] 卢新根. 轴流压气机内部流动失稳及被动控制策略研究[D]. 西安:西北工业大学, 2007.
[12] 韩戈. 管式扩压器内部复杂流动机理及设计方法研究[D]. 北京:中国科学院大学, 2016.
[13] 张学锋. 高压比离心压气机高性能设计关键技术研究[D]. 北京:中国科学院大学, 2014.
[14] Rochunon N. Analyse de l’écoulement Tridimensionnel et Instationnaire Dans un Compresseur Centrifuge à Fort Taux de Pression[D]. Lyon: EcoleCentrale de Lyon, 2007.
[15] 周健, 赵庆军, 杜建一. 超声速串列转子三维流场数值分析[J]. 推进技术, 2012, 33(5): 719-725. (ZHOU Jian, ZHAO Qing-jun, DU Jian-yi. Three-Dimentional Numerical Investigation on Aerodynamic Performance in a Supersonic Tandem Rotor[J]. Journal of Propulsion Technology, 2012, 33(5): 719-725.)
[16] 赵斌, 刘宝杰. 前、后排叶片相对位置对串列转子性能的影响[J]. 推进技术, 2012, 33(1): 26-36. (ZHAO Bin, LIU Bao-jie. Effects of Relative Geometry Position of Forward and Aft Blades on Performance of Tandem Rotor[J]. Journal of Propulsion Technology, 2012, 33(1): 26-36.)
[17] 初雷哲. 高转速高压比离心压气机内部流动研究[D]. 北京:中国科学院研究生院, 2008.(编辑:史亚红)　　　　　　　　　　　　　*　收稿日期:2017-03-06；修订日期:2017-05-10。基金项目:国家自然科学基金(51476166)。作者简介:李紫良,男,博士生,研究领域为叶轮机械气动热力学。E-mail: liziliang@iet.cn

高压比离心压气机串列叶轮内部流动机理研究

Mechanism of Highly-Loaded Centrifugal Compressor Stage with Tandem Impeller

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 0

编辑推荐

Metrics

本文评价