Analysis of Circumferential Groove Casing Treatment on Axial Compressor

被引:0
|
作者
Yi, Tao [1 ]
Xie, Fang [1 ]
Liu, De-Jun [1 ]
Ji, Tian-Ye [1 ]
机构
[1] Xian Inst High Technol, Xian 710025, Peoples R China
关键词
axial compressor; casing treatment; circumferential groove; leakage flow;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
As an effective method to extend the stability range of axial compressor, circumferential groove casing treatment has always been the focus of researchers. This paper analyze the stall margin improvement of casing treatment and the flow field in axial compressor. Slot type and circumferential casing treatment are compared to conduct the development situation of optimized casing structure. We introduce a new casing treatment which can extend the stability range and improve efficiency of axial compressor. It turned out that keeping both pressure ratio and efficiency and improving the stall margin of compressor is the most important goal via designing reasonable tip clearance and circumferential groove casing treatment. The design principles can be used as a reference for the industrial sector.
引用
收藏
页码:482 / 486
页数:5
相关论文
共 50 条
  • [1] The stall inceptions in an axial compressor with single circumferential groove casing treatment at different axial locations
    Liu, Le
    Li, Jichao
    Nan, Xi
    Lin, Feng
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 59 : 145 - 154
  • [2] A Computational Fluid Dynamics Study of Circumferential Groove Casing Treatment in a Transonic Axial Compressor
    Chen, Haixin
    Huang, Xudong
    Shi, Ke
    Fu, Song
    Ross, Mark
    Bennington, Matthew A.
    Cameron, Joshua D.
    Morris, Scott C.
    McNulty, Scott
    Wadia, Aspi
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2014, 136 (03):
  • [3] A CFD STUDY OF CIRCUMFERENTIAL GROOVE CASING TREATMENTS IN A TRANSONIC AXIAL COMPRESSOR
    Chen, Haixin
    Huang, Xudong
    Shi, Ke
    Fu, Song
    Bennington, Matthew A.
    Morris, Scott C.
    Ross, Mark
    McNulty, Scott
    Wadia, Aspi
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 513 - 523
  • [4] Numerical Investigation of Inlet Distortion on an Axial Flow Compressor Rotor with Circumferential Groove Casing Treatment
    Jian, Huang
    Hu, Wu
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2008, 21 (06) : 496 - 505
  • [5] Numerical Investigation of Inlet Distortion on an Axial Flow Compressor Rotor with Circumferential Groove Casing Treatment
    Huang JianWu Hu School of Power and EnergyNorthwestern Polytechnical UniversityXi an China
    [J]. Chinese Journal of Aeronautics, 2008, 21 (06) : 496 - 505
  • [7] An Optimization Study of Circumferential Groove Casing Treatment in a High-Speed Axial Flow Compressor
    Liu, Wenhao
    Chu, Wuli
    Zhang, Haoguang
    Wang, Hao
    [J]. AEROSPACE, 2024, 11 (07)
  • [8] Axial Compressor Stall, Circumferential Groove Casing Treatment, and the Tip-Clearance Momentum Flux
    Ross, Mark H.
    Cameron, Joshua D.
    Morris, Scott C.
    Chen, Haixin
    Shi, Ke
    [J]. JOURNAL OF PROPULSION AND POWER, 2018, 34 (01) : 146 - 152
  • [9] Effect of circumferential groove casing on the response to distortion of an axial flow compressor rotor
    School of Power and Energy, Northwestern Polytechnical Univ., Xi'an 710072, China
    不详
    [J]. Tuijin Jishu, 2008, 3 (334-338+366):
  • [10] Experimental investigation of stability enhancement with single circumferential groove casing treatment on a low speed axial compressor
    Key Laboratory of Advanced Energy and Power, Institute of Engineering Thermophysics, Chineses Academy of Sciences, Beijing
    100190, China
    不详
    100190, China
    [J]. Hangkong Xuebao, 5 (1422-1431):