组合机匣处理对跨音压气机流动特性的影响

刘家璇; 杨福胜; 邓建强; 张早校

doi:10.7652/xjtuxb202004021

您当前的位置：

首页 >

文章列表页 >

组合机匣处理对跨音压气机流动特性的影响

更新时间：2025-07-09

- 组合机匣处理对跨音压气机流动特性的影响
- Influence of Combined Casing Treatment on Flow Characteristics of Transonic Compressor
- 西安交通大学学报 2020年54卷第4期页码：173-178
- 作者机构：
  
  西安交通大学化学工程与技术学院,西安,710049
- 作者简介：
- 基金信息：
  
  : 2019-07-31.作者简介: 刘家璇(1996-),男,硕士生;杨福胜(通信作者),男,副教授.基金项目: 国家重点研发计划资助项目(2017YFB0903600)
- DOI：10.7652/xjtuxb202004021
  中图分类号： V235.12
- 网络首发：2020-04-10，
  
  纸质出版：2020
- 稿件说明：
移动端阅览
刘家璇, 杨福胜, 邓建强, 等. 组合机匣处理对跨音压气机流动特性的影响[J]. 西安交通大学学报, 2020,54(4):173-178.

Influence of Combined Casing Treatment on Flow Characteristics of Transonic Compressor[J]. 2020, 54(4): 173-178.
刘家璇, 杨福胜, 邓建强, 等. 组合机匣处理对跨音压气机流动特性的影响[J]. 西安交通大学学报, 2020,54(4):173-178. DOI： 10.7652/xjtuxb202004021.

Influence of Combined Casing Treatment on Flow Characteristics of Transonic Compressor[J]. 2020, 54(4): 173-178. DOI： 10.7652/xjtuxb202004021.

摘要

针对当前单一流动控制技术在压气机优化方面存在影响范围不大、性能提升有限的不足

提出了一种轴向倾斜缝和抽吸槽相结合的组合机匣处理结构

采用定常数值模拟研究了两种流动控制技术的结合对跨音压气机流场特性及性能的影响。模拟结果表明:应用该组合机匣处理结构后

转子在峰值效率下降2.5%的前提下使失速裕度提高了5.52%

明显改善了转子的性能; 组合机匣处理除了能同时改善叶顶和端壁的流动之外

两种结构的复合影响使激波强度降低、流体分离减弱

低速范围明显减小; 尽管两种结构的相互作用能为低能流体提供能量

但射流与主流流动发生的掺混带来了一定的掺混损失

增加了主流的切向动量及二次流损失

引起转子效率降低。

Abstract

To expand the influence range of flow control technology and further improve the performance of rotor

a combined casing structure with axial skewed slots and suction slots is presented

and the influences of the combination of two flow control technologies on the flow field characteristics and performance of the transonic compressor are investigated numerically by steady state simulation. The results show that the stall margin is increased by 5.52% while the peak efficiency reduces by 2.5%

which indicates the significantly improved performance of the rotor. In addition

the flows at both blade tip and end wall are ameliorated; the combined effect of the two structures weakens shock wave intensity and fluid separation

and reduces the area of low velocity region. Although the interaction between the two structures can provide energy for the low-energy fluid

the mixing of the jet flow and the mainstream flow causes a certain mixing loss and increases the tangential momentum and second

关键词

Keywords

references

WENNERSTROM A J. Highly loaded axial flow compressors: history and current developments [J]. Journal of Turbomachinery, 1990, 112(4): 567-578.

HERGT A, MEYER R, ENGEL K. Effects of vortex generator application on the performance of a compressor cascade [J]. Journal of Turbomachinery, 2013, 135(2): 21-26.

BENINI E, BIOLLO R, PONZA R. Efficiency enhancement in transonic compressor rotor blades using synthetic jets: a numerical investigation [J]. Applied Energy, 2011, 88(3): 953-962.

DING J, CHEN S W, XU H, et al. Control of flow separations in compressor cascade by boundary layer suction holes in suction surface [C]∥Proceedings of ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. New York, USA: ASME, 2013: V06AT35A012.

TANG M Z, JIN D H, GUI X M. Modeling and numerical investigation of the inlet circumferential fluctuations of swept and bowed blades [J]. Journal of Thermal Science, 2017, 26(1): 1-10.

HOUGHTON T, DAY I. Stability enhancement by casing grooves: the importance of stall inception mechanism and solidity [J]. Journal of Turbomachinery, 2012, 134(2): 021003.

CHU W L, LI X J, WU Y H, et al. Reduction of end wall loss in axial compressor by using non-axisymmetric profiled end wall: a new design approach based on end wall velocity modification [J]. Aerospace Science and Technology, 2016, 55: 76-91.

ALONE D B, KUMAR S S, THIMMAIAH S, et al. Performance characterization of the effect of axial positioning of bend skewed casing treatment retrofitted to a transonic axial flow compressor [C]∥Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. New York, USA: ASME, 2014: GT2014-26099.

ROSS M H, CAMERON J D, MORRIS S C, et al. Axial compressor stall, circumferential groove casing treatment, and the tip-clearance momentum flux [J]. Journal of Propulsion and Power, 2018, 34(1): 146-152.

卢新根, 楚武利, 张燕峰. 跨音速压气机间隙流与处理机匣相互作用分析 [J]. 西安交通大学学报, 2006, 40(11): 1357-1360, 1364.

LU Xingen, CHU Wuli, ZHANG Yanfeng. Numerical investigation of interaction between casing treatment and tip leakage flow in a transonic compressor rotor [J]. Journal of Xi’an Jiaotong University, 2006, 40(11): 1357-1360, 1364.

党春宁. 周向槽机匣处理对跨声速轴流压气机影响分析 [J]. 燃气涡轮试验与研究, 2008, 21(3): 18-25, 12.

DANG Chunning. Analysis of the effects of circumferential groove casing treatment on a transonic axial flow compressor [J]. Gas Turbine Experiment and Research, 2008, 21(3): 18-25, 12.

MERCHANT A, KERREBROCK J L, ADAMCZYK J J, et al. Experimental investigation of a high pressure ratio aspirated fan stage [J]. Journal of Turbomachinery, 2005, 127(1): 43-51.

李勇, 王如根, 夏钦斌. 对跨音速转子附面层发展控制研究 [J]. 汽轮机技术, 2010(1): 32-34.

LI Yong, WANG Rugen, XIA Qinbin. Research on boundary development control at transonic compressor rotor [J]. Turbine Technology, 2010(1): 32-34.

张皓光, 王云鹏, 吴俊, 等. 组合型机匣处理提高轴流压气机稳定性的机理 [J]. 航空动力学报, 2015, 30(1): 228-236.

ZHANG Haoguang, WANG Yunpeng, WU Jun, et al. Mechanism of improvement on axial-flow compressor stability with assembled casing treatment [J]. Journal of Aerospace Power, 2015, 30(1): 228-236.

CHIMA R V, STRAZISAR A J. Comparison of two-and three-dimensional flow computations with laser anemometer measurements in a transonic compressor rotor [J]. Journal of Engineering for Power, 1983, 105(3): 596-605.

刘志伟, 张长生, 时静珣, 等. 倾斜缝机匣处理轴向位置对压气机性能影响的研究 [J]. 工程热物理学报, 1987, 8(1): 52-54.

LIU Zhiwei, ZHANG Changsheng, SHI Jingxun, et al. A study on effects of axial positions of skewed slots casing treatment on compressor performance [J]. Journal of Engineering Thermophysics, 1987, 8(1): 52-54.

杨宵毅, 宁方飞. 飞轴流压气机失速点流场特性数值研究 [J]. 燃气涡轮试验与研究, 2011, 24(1): 29-34, 41.

YANG Xiaoyi, NING Fangfei. Numerical investigation of flow field characteristics at near stall condition in axial compressor [J]. Gas Turbine Experiment and Research, 2011, 24(1): 29-34, 41.

张皓光, 楚武利, 吴艳辉. 缝式处理机匣轴向位置对压气机特性影响的机理 [J]. 航空动力学报, 2011, 26(1): 92-98.

ZHANG Haoguang, CHU Wuli, WU Yanhui. Mechanism of influences of axial positions of axial skewed slot casing treatment on a compressor performance [J]. Journal of Aerospace Power, 2011, 26(1): 92-98.

郑覃, 卢少鹏, 羌晓青, 等. 动叶局部弯曲对压气机流场和性能的影响 [J]. 流体机械, 2015, 43(7): 27-31, 21.

ZHENG Tan, LU Shaopeng, QIANG Xiaoqing, et al. Influence of partially bowed rotor blades on the flow field and performance in a compressor [J]. Fluid Machinery, 2015, 43(7): 27-31, 21.

张皓光, 谭锋, 安康, 等. 跨音速轴流压气机逆角向缝机匣处理及其轴向位置的研究 [C]∥中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议论文集. 北京: 中国航天第三专业信息网, 2017: 302-313.

安鑫. 跨音压气机边界层抽吸控制方法研究 [D]. 北京: 中国科学院研究生院(工程热物理研究所), 2015: 40-42.

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

语义区分和子图整合驱动的知识图谱表示学习方法

EBSILON软件在热电联产系统优化中的应用综述

水蒸气掺混对氨裂解气旋流燃烧与排放特性的影响研究

结构-语义-残差协同的图像压缩框架：面向隐私保护与高保真重建

混合电解槽阵列协同的风光耦合制氢系统双层多目标优化