Correlation of solidity, aspect ratio and compound lean blade in compressor cascade design

被引:11
|
作者
Xu, Wenjuan [1 ]
Du, Xin [1 ]
Tao, Chuansijia [1 ]
Wang, Songtao [1 ]
Wang, Zhongqi [1 ]
机构
[1] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China
关键词
Solidity; Aspect ratio; Compound lean blade; Diffusion factor; Total pressure loss; Compressor cascade design; FLOW; DEVIATION;
D O I
10.1016/j.applthermaleng.2018.12.167
中图分类号
O414.1 [热力学];
学科分类号
摘要
Compressor one-dimensional design prediction models provide match basis of cascade design parameters. Solidity and aspect ratio are two primary prediction parameters. Compound lean blade is a three-dimensional blade technology generally applied in compressor redesign. This paper analyzes the correlations of solidity, aspect ratio and compound lean blade in order to find compound lean blade effect on cascade design. Abundant cascade cases have been computed by proved numerical method. Characteristics of compound lean blade effect on diffusion and loss are discussed. To exploit the dependence of geometry and performance parameters under min-loss working condition, a minimum loss incidence (i(o)) model, a diffusion factor (D-o) model and a total pressure loss (omega(o)) model are built up, and dependence map of parameters is analyzed. It suggests that compound lean blade changes constraint relations between parameters and enriches the choices of design case. Finally, a minimum loss model (omega(theta),(Do))(min) and a minimum blade count model (h/t(theta),(Do))(min) are studied, providing new parameter match principles and selection range, which breaks through traditional parameters balance relationship established based on straight blade. So, there is reasonable prediction that introducing compound lean blade to prediction models could broaden compressor one-dimensional design view and contribute to compressor optimal design.
引用
收藏
页码:175 / 192
页数:18
相关论文
共 34 条
  • [1] Correlation of solidity and curved blade in compressor cascade design
    Xu, Wenjuan
    Du, Xin
    Wang, Songtao
    Wang, Zhongqi
    APPLIED THERMAL ENGINEERING, 2018, 131 : 244 - 259
  • [2] Effects of solidity on characteristics of compressor cascade with curved-blade
    Zhong, Jingjun
    Wang, Wei
    Su, Jiexian
    Wang, Zhongqi
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 1997, 12 (02): : 163 - 166
  • [3] Relationship of optimum curved blade stack line and aspect ratio in linear compressor cascade
    Ling, Jing
    Du, Xin
    Wang, Songtao
    Wang, Zhongqi
    Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering, 2014, 34 : 153 - 159
  • [4] Solidity effect on corner separation and its control in a high-speed low aspect ratio compressor cascade
    Tang, Yumeng
    Liu, Yangwei
    Lu, Lipeng
    INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2018, 142 : 304 - 321
  • [5] Relationship between optimum curved blade generate line and cascade solidity in linear compressor cascade
    School of Energy Science and Engineering, Harbin Institute of Technology, Harbin
    150001, China
    Jixie Gongcheng Xuebao, 8 (144-150):
  • [6] Optimization Design of Aspect Ratio and Solidity of a Heavy-Duty Gas Turbine Transonic Compressor Rotor
    Liu, Shuaipeng
    Geng, Shaojuan
    Li, Xinlong
    Jin, Yun
    Zhang, Hongwu
    MACHINES, 2023, 11 (01)
  • [7] Full blended blade and endwall design of a compressor cascade
    Meng, Tongtong
    Yang, Guang
    Zhou, Ling
    Ji, Lucheng
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (11) : 79 - 93
  • [8] Full blended blade and endwall design of a compressor cascade
    Tongtong MENG
    Guang YANG
    Ling ZHOU
    Lucheng JI
    Chinese Journal of Aeronautics, 2021, 34 (11) : 79 - 93
  • [9] Full blended blade and endwall design of a compressor cascade
    Tongtong MENG
    Guang YANG
    Ling ZHOU
    Lucheng JI
    Chinese Journal of Aeronautics , 2021, (11) : 79 - 93
  • [10] Design Optimization of a Blended Blade and Endwall in a Compressor Cascade
    Li, Jiabin
    Ji, Lucheng
    Zhou, Ling
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2020, 142 (02):