CONCURRENT EFFECTS OF HOT STREAK AND GAS SPECIES CONCENTRATION ON AEROTHERMAL CHARACTERISTICS IN A TURBINE STAGE

被引:0
|
作者
Wang, Zhong-Nan [1 ]
Yuan, Xin [1 ]
机构
[1] Tsinghua Univ, Minist Educ, Key Lab Thermal Sci & Power Engn, Beijing 100084, Peoples R China
来源
PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 8, PTS A-C | 2012年
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Hydrogen or syngas derivative turbines in IGCC power plant promise increased efficiency with exceptional low NOx and CO2 emission. On one hand, the working flow in hydrogen turbines will be primarily water steam mixed with nitrogen, which leads to special aero-thermal characteristics in the turbine. On the other hand, the diluting and cooling air in combustors forms a cushion around the hot combustion gas, which results in both temperature and gas species non-uniformity at the turbine inlet. The goal of this paper is to study the concurrent effect of the two non-uniform inlet conditions on aerodynamics and heat transfer characteristics of the downstream turbine. In this paper, three-dimensional unsteady Navier-Stokes simulation was performed primarily on two cases: one with both hot streak and a range of species concentrations, and the other with only hot streak at the turbine inlet. The hot streak and species concentration migration was investigated to reveal their interaction. The results indicated that the steam concentration, among the range of species concentration, have the influential impact on the streak migration. It will enhance radial hot streak migration and promote the hot gas accumulation the rotor pressure side. Also, the tip leakage flow was also increased by the species concentration. Based on the understanding of their migration behaviors, the adiabatic wall temperature distribution was discussed to reveal the inlet species concentration effects on the blade heat load. The maximum blade surface temperature increase, due to the inlet species concentration, is about 1.5% of inlet total temperature (about 25 K) on the pressure side. The research in this paper will provide a practical guideline for the cooling strategy design of hydrogen turbines in the future.
引用
收藏
页码:1431 / 1441
页数:11
相关论文
共 50 条
  • [41] CFD ANALYSES OF A SINGLE STAGE TURBINE WITH INLET HOT-STREAK AT DIFFERENT CIRCUMFERENTIAL LOCATIONS
    Murari, Sridhar
    Sathish, Sunnam
    Bommisetty, Ramakumar
    Liu, Jong S.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 6A, 2013,
  • [42] HOT STREAK MIGRATION IN A TURBINE STAGE: INTEGRATED DESIGN TO IMPROVE AERO-THERMAL PERFORMANCE
    Basol, A. M.
    Jenny, P.
    Ibrahim, M.
    Kalfas, A.
    Abhari, R. S.
    PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 4, PTS A AND B, 2010, : 847 - 860
  • [43] An aerothermal analysis of the effects of tip gap height and cavity depth of a gas turbine blade
    Li, Chenxi
    Xiang, Jiacheng
    Song, Liming
    Li, Jun
    INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2020, 158 (158)
  • [44] Turbine Airfoil Aerothermal Characteristics in Future Coal Gas-Based Power Generation Systems
    Chyu, Minking K.
    Alvin, Mary Anne
    HEAT TRANSFER RESEARCH, 2010, 41 (07) : 737 - 752
  • [45] Effects of radial location of inlet hot streak on temperature distribution in low pressure stage of a vaneless counter-rotating turbine
    Zhao, Qing-Jun
    Wang, Hui-She
    Zhao, Xiao-Lu
    Xu, Jian-Zhong
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2009, 30 (02): : 214 - 216
  • [46] Numerical analysis of three-dimensional unsteady hot streak migration and shock interaction in a turbine stage
    Saxer, AP
    Felici, HM
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1996, 118 (02): : 268 - 277
  • [47] Influence of hot streak temperature ratio on low pressure stage of a vaneless counter-rotating turbine
    Zhao Qingjun
    Tang Fei
    Wang Huishe
    Du Jianyi
    Zhao Xiaolu
    Xu Jianzhong
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2008, 130 (03):
  • [48] Influence of hot streak temperature ratio on low pressure stage of a Vaneless Counter-Rotating Turbine
    Zhao, Qingjun
    Tang, Fei
    Wang, Huishe
    Du, Jianyi
    Zhao, Xiaolu
    Xu, Jianzhong
    Proceedings of the ASME Turbo Expo 2007, Vol 6, Pts A and B, 2007, : 469 - 480
  • [49] Three-dimensional simulations of hot streak clocking in a 1-1/2 stage turbine
    Gundy-Burlet, K
    Dorney, DJ
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 1997, 14 (03) : 133 - 144
  • [50] Tip-Clearance Effects on Hot-Streak Migration in Low-Pressure Stage of Vaneless Counter-Rotating Turbine
    Zhao, Qingjun
    Wang, Huishe
    Zhao, Xiaolu
    Xu, Jianzhong
    JOURNAL OF PROPULSION AND POWER, 2009, 25 (04) : 940 - 948