EXPERIMENTAL INVESTIGATION ON HEAT TRANSFER CHARACTERISTICS IN AN IMPINGEMENT/EFFUSION COOLING SYSTEM OF A RIBBED TURBINE CASING

被引:0
作者
Li, Guodong [1 ]
Guo, Tao [1 ]
Qiu, Changbo [3 ]
Liu, Cunliang [1 ,2 ]
Zhu, Huiren [1 ]
Li, Jichen [1 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, Xian, Shaanxi, Peoples R China
[2] Shaanxi Key Lab Thermal Sci Aeroengine Syst, Xian, Shaanxi, Peoples R China
[3] AECC Hunan Aviat Powerplant Res Inst, Zhuzhou, Hunan, Peoples R China
来源
PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 6B | 2022年
基金
中国国家自然科学基金;
关键词
Impingement/effusion cooling system; Turbine casing; Transient liquid crystal Thermography; Heat transfer characteristics; Low jet Reynolds numbers; JET IMPINGEMENT; UNCERTAINTIES;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The present paper reports an impingement/effusion cooling structure applied to the turbine casing. The structure consists of three rows of jet holes and two rows of effusion holes, both of which are in a staggered arrangement. A high rib exists inside the impinging chamber for structural support, which is connected to the effusion plate and divides the impinging chamber into two interconnected small chambers, one of which is arranged with effusion holes and the other is not. Transient liquid crystal (TLC) experiments were conducted to investigate the influence of the Reynolds number based on the jet hole diameter (ReD), distance between impingement plate and effusion plate(H), hole pith in Y direction(A) and X direction(C), with a parameter range of 1100 <= Re-D <= 5100, 2.5 <= H/D <= 7.5, 4.0 <= A/D <= 14.0 and 8.0 <= C/D <= 14.0, on the heat transfer characteristics of the effusion plate. The results show that the region averaged Nu increases with an increase in ReD for all studied cases and there is a linear relationship between the ReD and the region averaged Nu in the logarithmic coordinate. The change of H/D has an obvious effect on the heat transfer in the 2D-3D region from the stagnation point. As the H/D increases, the entrainment effect that makes the surrounding fluid continuously enter the jet, resulting in the velocity of the jet decreasing, and the enhanced heat transfer at the effusion plate becomes weaker. When 38<Y/D<42 and 0<Y/D<1, the Nu increases with the increase of H/D due to the weakening of the flow separation of the wall jet. The variation of A/D has little effect on the enhanced heat transfer in Region1 (surface without effusion hole), but for Regions2-4 (surface with effusion holes), decreasing or increasing A/D is unfavorable to the uniformity of the Nu distribution. The heat transfer enhancement is mainly influenced by C/D. As C/D decreases, the proportion occupied by the stagnation region gradually increases, thus the surface Nu increases significantly.
引用
收藏
页数:14
相关论文
共 45 条
  • [1] Experimental and numerical investigation on the role of holes arrangement on the heat transfer in impingement/effusion cooling schemes
    Andreini, Antonio
    Cocchi, Lorenzo
    Facchini, Bruno
    Mazzei, Lorenzo
    Picchi, Alessio
    [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2018, 127 : 645 - 659
  • [2] LIQUID-CRYSTAL METHODS FOR STUDYING TURBULENT HEAT-TRANSFER
    BAUGHN, JW
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 1995, 16 (05) : 365 - 375
  • [3] Ben Ahmed F, 2010, PROCEEDINGS OF THE ASME INTERNATIONAL HEAT TRANSFER CONFERENCE - 2010, VOL 5, P199
  • [4] Ben Ahmed F, 2011, Turbo Expo: Power for Land, Sea, and Air, V54655, P1095
  • [5] Bunker R. S., 2013, Turbo Expo: Power for Land, Sea, and Air, V55164
  • [6] Cho H.H., 1996, KSMEJSME THERMAL FLU, P71
  • [7] Cho H H, 2004, Turbo Expo: Power for Land, Sea, and Air, V41685, P643
  • [8] Cho H H, 2000, Turbo Expo: Power for Land, Sea, and Air, V78569
  • [9] The Effect of External Casing Impingement Cooling Manifold Standoff Distance on Casing Contraction for Thermal Control of Blade Tip Clearance
    Choi, Myeonggeun
    Gillespie, David R. H.
    Lewis, Leo V.
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 140 (02):
  • [10] Da Soghe R, 2012, PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, P301