Study on Humid Air Turbine Cooling Technique

Hua ZHU; Biao YAN; Yusong LIU; Liang LI

doi:10.12096/j.2096-4528.pgt.21050

English Version Reader LoginJournal Login

您当前的位置：

首页 >

文章列表页 >

Study on Humid Air Turbine Cooling Technique

Intelligent Turbine Power Generation Technology | 更新时间：2025-07-04

- Study on Humid Air Turbine Cooling Technique
- Power Generation Technology Vol. 42, Issue 4, Pages: 412-421(2021)
- 作者机构：
  
  1.西安交通大学叶轮机械研究所, 陕西省西安市 710049
  2.陕西省叶轮机械及动力装备工程实验室, 陕西省西安市 710049
- 作者简介：
- 基金信息：
  
  National Science and Technology Major Project(2017-I-0009-0010)
- DOI：10.12096/j.2096-4528.pgt.21050
  CLC： TK14
- Received：29 April 2021，
  
  Published：31 August 2021
- 稿件说明：
移动端阅览
Hua ZHU, Biao YAN, Yusong LIU, et al. Study on Humid Air Turbine Cooling Technique[J]. Power Generation Technology, 2021, 42(4): 412-421.
DOI：

Hua ZHU, Biao YAN, Yusong LIU, et al. Study on Humid Air Turbine Cooling Technique[J]. Power Generation Technology, 2021, 42(4): 412-421. DOI： 10.12096/j.2096-4528.pgt.21050.

摘要

为了研究湿空气对透平叶片冷却的影响特性，构建湿空气透平冷却性能预测模型，建立了常压透平叶片冷却实验平台，开展了以湿空气为冷却工质的实验研究。在湿空气含湿量为15~80g/kg、温度为200℃的条件下，对叶片前缘冲击冷却、肋片扰流U型通道冷却和叶片尾缘柱肋冷却进行了实验研究，探究了不同雷诺数下3种冷却方式的靶面换热性能随含湿量和温度的变化规律。研究结果表明：靶面换热强度随冷气含湿量的提高而增强，随冷气温度的提高而减弱，随冷气雷诺数的提高而增强。在含湿量约为180g/kg时，相对于干空气，冲击冷却、肋片扰流U型通道冷却、柱肋冷却的靶面平均努塞尔数最大分别提高了6.5%、10.0%、9.2%。

Abstract

In order to study the influence of humid air on the cooling performance of turbine blade and build the cooling performance prediction model of humid air turbine

the experimental platform of normal pressure turbine blade cooling was established

and the experimental study of humid air as coolant medium was carried out. Under the condition of humid air moisture content of 15-80g/kg and temperature of 200℃

the impingement cooling of blade leading edge

the U-channel cooling of fin disturbing flow and the pin-fin cooling of blade trailing edge were experimentally studied. The variation of heat transfer performance of the target wall with moisture content and temperature under different Reynolds numbers was explored. The results indicate that the heat transfer intensity of the target wall increases with the increasing coolant humid ratio

the decreasing coolant temperature and the increasing coolant Reynolds number. When using the humid air with moisture content of 180g/kg

the area-averaged Nussult number of target wall for impingement cooling

U-channel cooling and pin-fin cooling increases by 6.5%

10.0% and 9.2% respectively

compared with the case using dry air.

关键词

Keywords

references

薛晓东, 韩巍, 王晓东, 等. 适合分布式冷热电联供系统的中小型发电装置[J]. 发电技术, 2020, 41(3): 252-260.

XUE X D, HAN W, WANG X D, et al. Small and medium-scale power generation devices suiting for distributed combined cooling, heating and power system[J]. Power Generation Technology, 2020, 41(3): 252-260.

苏烨, 丁俊宏,丁宁, 等. 全国燃气轮机联合循环机组热控系统典型故障分析及预控措施建议[J]. 浙江电力, 2020, 39(8): 95-102.

SU Y, DING J H, DING N, et al. Typical fault analysis and proposals of pre-control measures for thermal control system of national gas turbine combined cycle units[J]. Zhejiang Electric Power, 2020, 39(8): 95-102.

朱俊杰, 王晓维, 董玉亮, 等. 基于工况辨识的重型燃气轮机性能评价方法研究[J]. 智慧电力, 2020, 48(7): 24-29.

ZHU J J, WANG X W, DONG Y L, et al. Performance evaluation method of heavy duty gas turbine based on condition identification[J]. Smart Power, 2020, 48(7): 24-29.

翁史烈, 陈汉平. 湿空气透平循环的基础研究[M]. 上海: 上海交通大学出版社, 2008: 2-5.

WENG S L, CHEN H P. The basic research of humid air turbine cycle[M]. Shanghai: Shanghai Jiaotong University Press, 2008: 2-5.

HIGUCHI S, KOGANEZAWA T, HORIUCHI Y, et al. Test results from the advanced humid air turbine system pilot plant: part 1: overall performance[C]//Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air. Berlin, Germany, June 9-13, 2008: 691-700.

YAGI M, ARAKI H, TAGAWA H, et al. Progress of the 40 MW-classadvanced humid air turbine tests[J]. Journal of Engineering for Gas Turbine and Power, 2013, 135(11): 112002.

TRINH X T, FÉNOT M, DORIGNAC E. The Effect of nozzle geometry on local convective heat transfer to unconfined impinging air jets[J]. Experimental Thermal and Fluid Science, 2016, 70: 1-16.

XING Y, SPRING S, WEIGAND B. Experimental and numerical investigation of heat transfer characteristics of inline and staggered arrays of impinging jets[J]. Journal of Heat Transfer, 2010, 132(9): 1-9.

XING Y, WEIGAND B. Experimental investigation of impingement heat transfer on a flat and dimpled plate with different crossflow schemes[J]. International Journal of Heat and Mass Transfer, 2010, 53(19/20): 3874-3886.

TASLIM M E, BETHKA D. Experimental and numerical impingement heat transfer in an airfoil leading-edge cooling channel with cross-flow[J]. Journal of Turbomachinery, 2009, 131(1): 939-947.

BU X, PENG L, LIN G, et al. Experimental study of jet impingement heat transfer on a variable-curvature concave surface in a wing leading edge[J]. International Journal of Heat and Mass Transfer, 2015, 90: 92-101.

韩旭军. 涡轮叶片内部冷却结构参数化及带肋通道优化设计[D]. 哈尔滨: 哈尔滨工业大学, 2011.

HAN X J. Parametric expression of cooling structure of turbine blade and the optimization design of channels with ribs[D]. Harbin: Harbin Institute of Technology, 2011.

刘传凯, 丁水汀, 陶智. 旋转附加力对方通道内流动与换热的影响机理[J]. 北京航空航天大学学报, 2009, 35(3): 276-279.

LIU C K, DING S T, TAO Z. Effects of rotating induced forces on fluid flow and heat transfer in square channel[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(3): 276-279.

CHANG S W, HU Y W. Endwall thermal performances of radially rotating rectangular channel with pin-fins on skewed rib lands[J]. International Journal of Heat and Mass Transfer, 2014, 69: 173-190.

LIGRANI P M, OLIVEIRA M M, BLASKOVICH T. Comparison ofheat transfer augmentation techniques[J]. AIAA Journal, 2003, 41(3): 337-362.

张丽, 张书华, 朱惠人, 等. 小间距梯形扰流柱通道内的流动换热数值计算[J]. 航空动力学报, 2009, 24(1): 13-17.

ZHANG L, ZHANG S H, ZHU H R, et al. Numerical simulation on flow and heat transferin channel with small spacing short pin-fin arrays[J]. Journal of Aerospace Power, 2009, 24(1): 13-17.

吴江波, 王新军. 扰流肋柱在流动方向排列密度对矩形通道表面传热影响的数值研究[J]. 热科学与技术, 2010, 9(4): 308-311.

WU J B, WANG X J. Numerical study of effects of pin-fin array density at flow direction on heat transfer[J]. Journal of Thermal Science and Technology, 2010, 9(4): 308-311.

CLEETON J, KAVANAGH R M, PARKS G T. Blade cooling optimization in humid-air and steam-injected gas turbines[J]. Applied Thermal Engineering, 2010, 29: 3274-3283.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Effects of Variable-Flow Water Distribution on Cooling Performance of Wet Cooling Towers and Its Optimization

Uncertainty Analysis of Gas Turbine Overall Performance Based on Monte Carlo Method

Research Progress on Film Cooling Fed by Crossflow Ribbed Passage of Gas Turbine Blades

Research Status and Development Trend of Rotating Internal Cooling Channel in Gas Turbine Blade

Review of Research on Swirl Cooling Technology of Gas Turbine Blades

Related Author

LUO Cheng

WANG Lei

LI Yang

MENG Qingming

ZHANG Guibin

ZHAO Yuanbin

LU Wenqiang

CHEN Yan

Related Institution

School of Nuclear Science, Energy and Power Engineering, Shandong University

China Grid Energy Hami Coal Power Company Limited, Hami 839000, Xinjiang Uygur Autonomous Region

China Energy Baoqing Coal Power & Chemical Company Limited

Jiangsu Yanhai Chemical Co., Ltd.

Nanjing Institute of Future Energy System, IET, CAS

AI问答

⁰