Film cooling effectiveness from upstream purge slots of a turbine vane endwall: Experiment, modeling, and correlation

被引:7
|
作者
Yang, Xing [1 ]
Zhao, Qiang [2 ]
Wu, Hang [1 ]
Feng, Zhenping [1 ]
机构
[1] Xi An Jiao Tong Univ, Inst Turbomachinery, Shaanxi Engn Lab Turbomachinery & Power Equipment, Xian 710049, Peoples R China
[2] Xian Aerosp Prop Inst, Xian 710100, Peoples R China
关键词
Turbine endwall; Purge air; Film cooling; Geometry variation; Correlation; Pressure-sensitive paint; HEAT-TRANSFER; BOUNDARY-LAYER; FLOW-FIELD; CASCADE;
D O I
10.1016/j.ijheatmasstransfer.2023.124899
中图分类号
O414.1 [热力学];
学科分类号
摘要
The design of an efficient cavity slot between assembled components, where purge air is injected, is especially crucial to the durability and efficiency of an aero-engine, since the purge air is relevant to sealing and film cooling of the hot component. In this paper, film cooling for purge flow injected from slots upstream the endwall of a turbine vane is systematically investigated in a linear cascade using Pressure-Sensitive Paint (PSP). The influence of the slot width (0.020-0.044 times vane axial chord length), position (0.11-0.24 times vane axial chord length in front of turbine passage inlets), and inclination angle (20- 45 degrees) is examined for coolant injection ratios of 0.3-2.0 %, with an attempt to develop a new correlation specifically for purge flow film cooling over a turbine endwall, since existing correlations in literature only work for slot injection on flat plates. The experimental tests are undertaken in extensive ranges of the slot geometry and the injection rate that are typically seen in a modern engine. For better understanding the impacts of the affecting parameters, five-hole probe and thermocouple measurements and numerical simulations were carried out as well to visualize the coolant-withmainstream mixing flows. The measured local film coverage, pitchwise- and area-averaged cooling effectiveness are presented and discussed, in combination with the probe-detected and numerically-modeled flow structures to elaborate the experimental observations. The current results sufficiently reveal the changing tendency of purge flow film cooling caused by the variations of the slot geometry. Additionally, the newlydeveloped correlation is well validated using own experimental data and datasets in literature, proving the capability of the correlation to predict film cooling for purge flow injected from slots with such geometrical parameter ranges. The correlation can be a helpful tool to support the selection of an efficient slot in its preliminary design stage.
引用
收藏
页数:13
相关论文
共 50 条
  • [31] TURBINE VANE ENDWALL FILM COOLING WITH SLASHFACE LEAKAGE AND DISCRETE HOLE CONFIGURATION
    Chowdhury, Nafiz H. K.
    Shiau, Chao-Cheng
    Han, Je-Chin
    Zhang, Luzeng
    Moon, Hee-Koo
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5C, 2016,
  • [32] Computational study of a midpassage gap and upstream slot on vane endwall film-cooling
    Hada, Satoshi
    Thole, Karen A.
    PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 3, PTS A AND B: HEAT TRANSFER: GENERAL INTEREST, 2006, : 839 - 848
  • [33] APPLICATION OF THE TRANSIENT HEATER FOIL TECHNIQUE FOR HEAT TRANSFER AND FILM COOLING EFFECTIVENESS MEASUREMENTS ON A TURBINE VANE ENDWALL
    Jonsson, M.
    Charbonnier, D.
    Ott, P.
    von Wolfersdorf, J.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 4, PTS A AND B, 2008, : 443 - 453
  • [34] Numerical investigation of blowing ratio, density ratio and axial position of film holes on the vane endwall film cooling effectiveness with upstream step
    Xu, Qingzong
    Du, Qiang
    Wang, Pei
    Xiao, Xiangtao
    Liu, Jun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (03) : 541 - 553
  • [35] Transient simulation of pulsed purge film cooling on flow and thermal characteristics of a turbine endwall
    Liu, Youhong
    Luo, Yifu
    APPLIED THERMAL ENGINEERING, 2019, 161
  • [36] Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring
    Rezasoltani, M.
    Schobeiri, M. T.
    Han, J. C.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,
  • [37] Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall
    Zhang, Jie
    Liu, Cunliang
    Niu, Xiying
    Xu, Weijiang
    Zhang, Li
    Liu, Xuyang
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2023, 145 (11):
  • [38] Experimental and numerical investigations of overall cooling effectiveness on a vane endwall with jet impingement and film cooling
    Yang, Xing
    Liu, Zhansheng
    Zhao, Qiang
    Liu, Zhao
    Feng, Zhenping
    Guo, Fushui
    Ding, Liang
    Simon, Terrence W.
    APPLIED THERMAL ENGINEERING, 2019, 148 : 1148 - 1163
  • [39] Influence of hole shape on the performance of a turbine vane endwall film-cooling scheme
    Colban, W.
    Thole, K.
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2007, 28 (03) : 341 - 356
  • [40] Influences of large fillets on endwall flows in a vane cascade with upstream slot film-cooling
    Shote, Adeola S.
    Mahmood, Gazi, I
    Meyer, Josua P.
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2020, 112