双叉排气膜孔交互作用对气膜冷却效率影响Effect of double rows of film holes interaction on film cooling efficiency
林泽钦,温涛,王宇清
摘要(Abstract):
采用高精度红外热像仪测量了平板气膜冷却效率,比较了双叉排孔和单排孔气膜冷却效率,分析了孔间的相互作用,以及吹风比(M=0.65、1.00、1.50)和密度比(DR=1.0,1.5)对气膜冷却效率的影响;同时还采用数值计算方法比较了气膜冷却下的流场。结果表明:单排气膜孔冷却效率随着吹风比的增加而降低,但是双叉排气膜孔冷却效率大大提高,且随着吹风比的增加而增加,但是在展向气膜覆盖效果变差;增加密度比可以提高气膜冷却效率,但是双叉排孔和吹风比的影响相对密度比更大;双叉排孔相比于单排孔,冷却气流在孔下游形成了反肾形涡,较好抑制了气膜吹离。
关键词(KeyWords): 涡轮叶片;气膜冷却;冷却效率;双叉排气膜孔;流动与传热
基金项目(Foundation): 国家重点研发计划项目(2018YFE0206900)~~
作者(Author): 林泽钦,温涛,王宇清
DOI: 10.19666/j.rlfd.202307117
参考文献(References):
- [1] WANG W, GAO J, SHI X, et al. Cooling performance analysis of steam cooled gas turbine nozzle guide vane[J].International Journal of Heat and Mass Transfer, 2013, 62:668-679.
- [2] BUNKER R S. A review of shaped hole turbine film cooling technology[J]. ASME Journal of Heat Transfer,2005, 127:441-453.
- [3] ANDERSON J B, WINKA J R, BOGARD D G, et al.Evaluation of superposition predictions for showerhead film cooling on a vane[J]. Journal of Turbomachinery,2015, 137(4):041010.
- [4] ZHANG J Z, ZHANG S C,WANG C H, et al. Recent advances in film cooling enhancement:a review[J].Chinese Journal of Aeronautics 2020, 33(4):1119-1136.
- [5]张魏,李广超,寇志海,等.冷气横流对单入口和双出口孔射流冷却效率影响[J].热力发电, 2016, 45(3):64-69.ZHANG Wei, LI Guangchao, KOU Zhihai, et al. Influence of coolant crossflow on film cooling effectiveness of oneinlet and double-outlet injection holes[J]. Thermal Power Generation, 2016, 45(3):64-69.
- [6]于飞龙,肖俊峰,高松,等.猫耳气膜孔冷却性能数值模拟[J].热力发电, 2018, 47(9):48-55.YU Feilong, XIAO Junfeng, GAO Song, et al. Numerical study on cooling performance of Nekomimi film holes[J].Thermal Power Generation, 2018, 47(9):48-55.
- [7]李广超,陈钰恺,张魏,等.宽口扇形孔射流气膜冷却效率研究[J].热力发电, 2016, 45(4):60-64.LI Guangchao, CHEN Yukai, ZHANG Wei, et al. Investigation on film cooling effectiveness of fanned hole with broad outlet[J]. Thermal Power Generation, 2016, 45(4):60-64.
- [8] YU Y, YEN C H, SHIH T I P. Film cooling effectiveness and heat transfer coefficient distributions around diffusion shaped holes[J]. Journal of Heat Transfer, 2002, 124(5):820-827.
- [9]张玲,祝健,石景开,等.多因素影响下平板气膜冷却效果的数值模拟[J].热力发电, 2015, 44(6):68-71.ZHANG Ling, ZHU Jian, SHI Jingkai, et al. Orthogonal simulation of multi-factor influenced film cooling efficiency[J]. Thermal Power Generation, 2015, 44(6):68-71.
- [10] HAN J C, MEHENDALE A B. Flat plate film cooling with steam injection through one row and two rows of inclined holes[J]. Journal of Turbomachinery, 1986, 108(1):137-144.
- [11] ZHU H, GUO T, XU D. Investigation of film cooling and superposition method for double row dustpan-shaped holes[J].Heat Transfer-Asian Research, 2008, 37(4):208-217.
- [12] LIGRANI P M, RAMSEY A E. Film cooling from span wise-oriented holes in two staggered rows[J]. Journal of Turbomachinery, 1997, 119(3):V004T09A028.
- [13] LIU Y, RAO Y, YANG L, et al. Flow and heat transfer characteristics of double-wall cooling with multi-row short film cooling hole arrangements[J]. International Journal of Thermal Sciences, 2021, 165:106878.
- [14] SAUMWEBER C, SCHULZ A. Interaction of film cooling rows:effects of hole geometry and row spacing on the cooling performance downstream of the second row of holes[J].Journal of Turbomachinery, 2004, 126(2):237-246.
- [15]张鸣远,陈学俊,邹福康,等.双排叉排孔气膜冷却特性研究(二)绝热有效温比[J].航空动力学报, 1990, 5(1):6-10.ZHANG Mingyuan, CHEN Xuejun, ZHOU Fukang, et al.Study on the cooling characteristics of double row fork vent air membrane(Ⅱ)adiabatic effective temperature ratio[J]. Journal of Aerospace Power, 1990, 5(1):6-10.
- [16]宋波,林宇震,刘高恩,等.不同排列方式多斜孔壁气膜冷却绝热温比研究[J].航空动力学报, 1999, 14(1):91-94.SONG Bo, LIN Yuzhen, LIU Gaoen, et al. Study on the adiabatic temperature ratio of polyoblique pore wall air film cooling in different arrangements[J]. Journal of Aerospace Power, 1999, 14(1):91-94.
- [17] JUBRAN B A, MAITEH B Y. Film cooling and heat transfer from a combination of two rows of simple and/or compound angle holes in inline and/or staggered configuration[J]. Heat and Mass Transfer, 1999, 34(6):495-502.
- [18]王浪,李雪英,任静,等.两排圆孔的气膜冷却特性[J].工程热物理学报, 2017, 38(5):1082-1086.WANG Lang, LI Xueying, REN Jing, et al. Flow characteristics and superposition rule of two rows of round holes[J].Journal of Engineering Thermophysics, 2017, 38(5):1082-1086.
- [19] KIROLLOS B, POVEY T. An energy-based method for predicting the additive effect of multiple film cooling rows[J]. Journal of Engineering for Gas Turbines and Power, 2015, 137(12):122607.
- [20] FOROUTAN H, YAVUZKURT S. Numerical simulations of the near-field region of film cooling jets under high free stream turbulence:applications of RANS and hybrid URANS/LES[J].Journal of Heat Transfer, 2015, 137:011701.
- [21] XU Zhipeng, ZHU Huiren, LIU Cunliang, et al. Film cooling effectiveness superposition calculation of doublerow injection holes on turbine vane[J]. Journal of Thermal Science, 2022, 31(6):2424-2437.
- [22] LYNCH S P, THOLE K A, KOHLI A, et al. Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring[J]. Journal of Turbomachinery, 2011, 133(4):041003.
- [23] LEE K D, KIM K Y. Numerical study on film-cooling performance of a novel shaped hole[C]//International Symposium on Fluid Machinery and Fluids Engineering(ISFMFE 2012), 2012.
- [24] SELLERS J P. Gaseous film cooling with multiple injection stations[J]. AIAA Journal, 1963, 1(9):2154-2156.
- [25]李彬,胡正义,林宇震,等. Sellers叠加模型在多孔阵冷却方式中的应用研究[J].燃气涡轮试验与研究,1999, 12(2):39-42.LI Bin, HU Zhengyi, LIN Yuzhen, et al. Application of Sellers superposition model in multi holes cooling[J]. Gas Turbine Experiment and Research, 1999, 12(2):39-42.
- [26]朱惠人,郭涛,许都纯.双排簸箕形孔气膜冷却效率及其叠加算法[J].航空动力学报, 2006, 21(5):814-819.ZHU Huiren, GUO Tao, XU Duchun. Film cooling and superposition method for double row dust-pan shaped holes[J]. Journal of Aerospace Power, 2006, 21(5):814-819.