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
  • [1] Upstream and Passage Endwall Film Cooling of a Transonic Turbine Vane
    Burdett, Timothy A. A.
    Ullah, Izhar
    Wright, Lesley M. M.
    Han, Je-Chin
    McClintic, John W. W.
    Crites, Daniel C. C.
    Riahi, Ardeshir
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2023, 37 (02) : 394 - 403
  • [2] Turbine Vane Endwall Film Cooling Effectiveness of Different Purge Slot Configurations in a Linear Cascade
    Mueller, Gunther
    Landfester, Christian
    Boehle, Martin
    Krewinkel, Robert
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2020, 142 (03):
  • [3] TURBINE VANE ENDWALL FILM COOLING EFFECTIVENESS OF DIFFERENT PURGE SLOT CONFIGURATIONS IN A LINEAR CASCADE
    Mueller, Gunther
    Landfester, Christian
    Boehle, Martin
    Krewinkel, Robert
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5B, 2019,
  • [4] Endwall film-cooling in a cascade with filleted vane, upstream discrete slots, and holes
    Shote, Adeola S.
    Huyssen, Barbara B.
    Mahmood, Gazi I.
    EXPERIMENTAL HEAT TRANSFER, 2024,
  • [5] UPSTREAM FILM COOLING ON THE CONTOURED ENDWALL OF A TRANSONIC TURBINE VANE IN AN ANNULAR CASCADE
    Salinas, Daniel A.
    Ullah, Izhar
    Wright, Lesley M.
    Han, Je-Chin
    McClintic, John W.
    Crites, Daniel C.
    Riahi, Ardeshir
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 7B, PT II, 2020,
  • [6] Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade
    Salinas, Daniel A.
    Ullah, Izhar
    Wright, Lesley M.
    Han, Je-Chin
    McClintic, John W.
    Crites, Daniel C.
    Riahi, Ardeshir
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 143 (06):
  • [7] Endwall film cooling holes design upstream of the leading edge of a turbine vane
    Liu, Jian
    Du, Wei
    Hussain, Safeer
    Xie, Gongnan
    Sunden, Bengt
    NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2020, 79 (03) : 222 - 245
  • [8] TURBINE VANE ENDWALL FILM COOLING CONSIDERING FLOW NONUNIFORMITIES AND COOLANT INJECTION FROM UPSTREAM COMBUSTORS
    Yang, Xing
    Zhao, Qiang
    Feng, Zhenping
    HEAT TRANSFER RESEARCH, 2021, 52 (13) : 11 - 31
  • [9] Effects of Upstream Step Geometries on Endwall Film Cooling and Phantom Cooling Performances of a Transonic Turbine Vane
    Bai, Bo
    Li, Zhigang
    Li, Jun
    Mao, Shuo
    Ng, Wing F.
    JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS, 2022, 14 (12)
  • [10] Effects of Upstream Endwall Film Cooling on a Vane Cascade Flowfield
    Mahmood, Gazi I.
    Arnachellan, Keenesh
    JOURNAL OF PROPULSION AND POWER, 2018, 34 (02) : 460 - 468