Comprehensive evaluations on performance and energy consumption of pre-swirl rotor-stator system in gas turbine engines

被引:20
|
作者
Lin, Aqiang [1 ,2 ]
Liu, Gaowen [1 ,2 ]
Wang, Xinxin [3 ]
Feng, Qing [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Peoples R China
[2] Northwestern Polytech Univ, Shaanxi Key Lab Thermal Sci Aeroengine Syst, Xian 710129, Peoples R China
[3] AECC Commercial Aircraft Engine Co LTD, Shanghai 200241, Peoples R China
关键词
Gas turbine engine; Turbine disc cavity; Pre-swirl system; Energy consumption; Performance prediction; Wall friction; Rotor-stator moment; Seal flow; AIR COOLING SYSTEM; HEAT-TRANSFER; CFD ANALYSIS;
D O I
10.1016/j.enconman.2021.114440
中图分类号
O414.1 [热力学];
学科分类号
摘要
Pre-swirl system has an indispensable role to supply enough cooling air with appropriate pressure, temperature, and mass flow rate to improve the life and the efficiency of turbine cooling blades and vanes. This study aimed to reveal the heat transfer mechanism and energy conversion characteristics of a multi-in and multi-out pre-swirl system. Subsequently, a novel modified prediction modeling was proposed to evaluate the system performance and energy conversion with complete consideration of multi-factors, especially for determining the influence of the seal flow, wall friction, work done by the rotating turbine disc, and rotor-stator moment. The results reveal that a high pre-swirl cooling performance and low-energy consumption can be obtained from the contribution of the airflow swirl ratio, whereas the swirl ratio was susceptible to the mixed seal flow. Thereafter, the seal outflow improved the system temperature-drop efficiency, whereas the seal inflow strongly influenced the heat transfer and energy consumption characteristics. The modified modeling resulted in a 56.89% increase in prediction accuracy relative to the Liu-model. Moreover, the nonlinear relationships between the seal flow and system performances can be comprehensively and accurately evaluated. In particular, a peak in a system temperature drop of 38.5 K can be realized with a low-energy consumption of -133 kW and a 64% enhancement in the airsupply flow rate based on a contribution of the seal flow on airflow swirl ratio. Thus, the implementation of the modified modeling can prove significant in theoretical guidance and engineering applications.
引用
收藏
页数:18
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共 35 条
  • [1] Effects of pre-swirl radius on cooling performance of a rotor-stator pre-swirl system in gas turbine engines
    Kong, Xiaozhi
    Huang, Tianshuo
    Liu, Yuxin
    Chen, Hua
    Lu, Huawei
    [J]. CASE STUDIES IN THERMAL ENGINEERING, 2022, 37
  • [2] Numerical investigation of the pre-swirl rotor-stator system of the first stage in gas turbine
    Liao, Gaoliang
    Wang, Xinjun
    Li, Jun
    [J]. APPLIED THERMAL ENGINEERING, 2014, 73 (01) : 940 - 952
  • [3] Theoretical and experimental evaluations of pre-swirl rotor-stator system with inner seal bypass configuration for turbine performance improvement
    Lin, Aqiang
    Liu, Gaowen
    Li, Pengfei
    Zhang, Zhiyuan
    Feng, Qing
    [J]. ENERGY, 2022, 258
  • [4] Fluid dynamics of a pre-swirl rotor-stator system
    Yan, Y
    Gord, MF
    Lock, GD
    Wilson, M
    Owen, JM
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2003, 125 (04): : 641 - 647
  • [5] NUMERICAL INVESTIGATION OF THE EFFECT OF AN AXIAL PRE-SWIRL NOZZLE WITH A RADIAL ANGLE IN A PRE-SWIRL ROTOR-STATOR SYSTEM
    Zhao, Gang
    Ding, Shuiting
    Qiu, Tian
    Zhang, Shenghui
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 5B, 2021,
  • [6] Flow and heat transfer characteristics in a pre-swirl rotor-stator cavity
    Yang, Xiaoyu
    Ren, Zhong
    Li, Xueying
    Ren, Jing
    Ligrani, Phillip M.
    [J]. INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2022, 172
  • [7] Numerical and theoretical study of flow and heat transfer in a pre-swirl rotor-stator system
    Farzaneh-Gord, Mahmood
    Wilson, Mike
    Owen, J. Michael
    [J]. Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B, 2005, : 943 - 949
  • [8] Effect of Impellers on the Cooling Performance of a Radial Pre-Swirl System in Gas Turbine Engines
    Shen, Wenjie
    Wang, Suofang
    Liang, Xiaodi
    [J]. AEROSPACE, 2024, 11 (03)
  • [9] INFLUENCE OF A WEAK SUPERPOSED CENTRIPETAL FLOW IN A ROTOR-STATOR SYSTEM FOR SEVERAL PRE-SWIRL RATIO
    Abdel Nour, Fadi
    Debuchy, Roger
    Bois, Gerard
    [J]. PROCEEDINGS OF THE ASME/JSME/KSME JOINT FLUIDS ENGINEERING CONFERENCE 2011, VOL 1, PTS A-D, 2012, : 2915 - 2923
  • [10] Numerical investigation of the flow and heat transfer characteristics for a pre-swirl rotor-stator system with center inflow
    Zhang, Feng
    Wang, Xinjun
    Li, Jun
    [J]. APPLIED THERMAL ENGINEERING, 2016, 105 : 646 - 658