脉动来流下燃氢涡轮叶栅端壁气膜冷却特性

张昊; 白波; 李志刚; 李军

doi:10.7652/xjtuxb202510007

您当前的位置：

首页 >

文章列表页 >

脉动来流下燃氢涡轮叶栅端壁气膜冷却特性

更新时间：2025-09-28

- 脉动来流下燃氢涡轮叶栅端壁气膜冷却特性
- Film Cooling Characteristics of Hydrogen-Fueled Turbine Cascade Endwall under Pulsating Inflow Conditions
- 西安交通大学学报 2025年59卷第10期页码：75-86
- 作者机构：
- 作者简介：
  
  作者简介：张昊（2001—），男，博士生；
  白波（通信作者），男，助理教授。
- 基金信息：
  
  国家自然科学基金资助项目。(52406054)
- DOI：10.7652/xjtuxb202510007
  中图分类号： TK474.4
- 收稿：2025-03-17，
  
  纸质出版：2025-10-10
- 稿件说明：
移动端阅览
张昊, 白波, 李志刚, 等. 脉动来流下燃氢涡轮叶栅端壁气膜冷却特性[J]. 西安交通大学学报, 2025,59(10):75-86.

ZHANG Hao, BAI Bo, LI Zhigang, et al. Film Cooling Characteristics of Hydrogen-Fueled Turbine Cascade Endwall under Pulsating Inflow Conditions[J]. Journal of Xi'an Jiaotong University, 2025, 59(10): 75-86.
张昊, 白波, 李志刚, 等. 脉动来流下燃氢涡轮叶栅端壁气膜冷却特性[J]. 西安交通大学学报, 2025,59(10):75-86. DOI： 10.7652/xjtuxb202510007.

ZHANG Hao, BAI Bo, LI Zhigang, et al. Film Cooling Characteristics of Hydrogen-Fueled Turbine Cascade Endwall under Pulsating Inflow Conditions[J]. Journal of Xi'an Jiaotong University, 2025, 59(10): 75-86. DOI： 10.7652/xjtuxb202510007.

摘要

为厘清掺氢/全氢燃烧诱发的燃气脉动对下游涡轮叶栅流动传热和冷却特性的影响，基于某研究所真实掺氢/全氢燃烧脉动测量数据和跨声速风洞试验数据，采用非定常数值方法，系统研究了设计运行工况下，燃气脉动频率（1、3、5kHz）对涡轮叶栅端区流动和端壁气膜冷却的影响。研究结果表明：脉动来流显著降低了端壁气膜冷却效率，其影响呈非单调频率依赖性，当频率为3kHz时气膜冷却效率降幅最小，约为4.02%，当5kHz时降幅最大，约为11.28%；端壁气膜冷却效率波动幅度随频率增加呈现先减小后增加趋势，气膜孔下游及叶栅喉部区域波动幅值最大；气膜冷却效率波动频率与进口脉动频率严格同步，即叶栅通道中脉动频率不发生衰减；随着脉动频率的增加，台阶下游空腔涡逐渐向端壁下游扩张，高频（5kHz）脉动下空腔涡和马蹄涡强度显著增强，诱发端区二次流结构失稳，导致端壁气膜冷却性能下降和波动幅值增加。研究揭示了脉动来流下涡轮叶栅端区流动冷却耦合机制和脉动特性，为燃氢涡轮叶栅端区高效冷却布局设计提供了参考。

Abstract

To clarify the effects of hydrogen-blended/full-hydrogen combustion-induced gas pulsation on the convective heat transfer and cooling characteristics of downstream turbine cascades

based on real hydrogen-blended/full-hydrogen combustion pulsation measurement data and transonic wind tunnel test data from a research institute and employing unsteady numerical methods

the influence of gas pulsation frequencies (1

and 5kHz) on the endwall flow and film cooling performance of a turbine cascade under design operating conditions is investigated. The results show that pulsating inflow significantly reduces the endwall film cooling effectiveness

exhibiting non-monotonic frequency dependence. The smallest reduction in film cooling effectiveness (approximately 4.02%) occurs at 3kHz

while the largest reduction (approximately 11.28%) occurs at 5kHz. The fluctuation amplitude of film cooling effectiveness initially decreases and then increases with rising frequency

with the largest fluctuations observed downstream of the film cooling holes and near the cascade throat. The fluctuation frequency of film cooling effectiveness strictly synchronizes with the inlet pulsation frequency

indicating no attenuation of pulsation frequency within the cascade passage. As the pulsation frequency increases

the cavity vortex downstream of the step gradually expands toward the endwall. Under high-frequency (5kHz) pulsation

the intensities of the cavity vortex and horseshoe vortex significantly strengthen

destabilizing the secondary flow structures in the endwall region and leading to degraded film cooling performance and increased fluctuation amplitudes. This study reveals the coupled mechanism of flow and cooling as well as the pulsation characteristics in the endwall region of hydrogen-fueled turbine cascades

providing insights for the design of high-efficiency cooling configurations in endwall region.

关键词

Keywords

references

生态环境部 . 发布《中国应对气候变化的政策与行动2023年度报告》 [J ] . 节能与环保 , 2023 ( 11 ): 5 .

Ministry of Ecology and Environment . Release of the 2023 annual report on China's policies and actions to address climate change [J ] . Energy Conservation &Environmental Protection , 2023 ( 11 ): 5 .

李苏辉 , 张归华 , 吴玉新 . 面向未来燃气轮机的先进燃烧技术综述 [J ] . 清华大学学报(自然科学版) , 2021 , 61 ( 12 ): 1423 - 1437 .

LI Suhui , ZHANG Guihua , WU Yuxin . Advanced combustion technologies for future gas turbines [J ] . Journal of Tsinghua University (Science and Technology) , 2021 , 61 ( 12 ): 1423 - 1437 .

PATEL V , SHAH R . Effect of hydrogen enrichment on combustion characteristics of methane swirling and non-swirling inverse diffusion flame [J ] . International Journal of Hydrogen Energy , 2019 , 44 ( 52 ): 28316 - 28329 .

吕光普 , 刘潇 , 张志浩 , 等 . 氢燃气轮机燃烧技术研究进展 [J ] . 燃气轮机技术 , 2022 , 35 ( 1 ): 1 - 15 .

LÜ Guangpu , LIU Xiao , ZHANG Zhihao , et al . Research progress of combustion technology in hydrogen gas turbine [J ] . Gas Turbine Technology , 2022 , 35 ( 1 ): 1 - 15 .

BUNKER R S . Gas turbine heat transfer:ten remaining hot gas path challenges [J ] . Journal of Turbomachinery , 2007 , 129 ( 2 ): 193 - 201 .

HAN J C . Fundamental gas turbine heat transfer [J ] . Journal of Thermal Science and Engineering Applications , 2013 , 5 ( 2 ): 021007 .

OLCZAK D , JAWORSKI M . Review of turbine cooling technologies [J ] . Journal of Engineering for Gas Turbines and Power , 2023 , 145 ( 9 ): 090801 .

CHOWDHURY N H K , SHIAU C C , HAN J C , et al . Film cooling effectiveness comparison on turbine vane endwall with cluster configurations using PSP measurement technique [C ] // ASME 2017 International Mechanical Engineering Congress and Exposition . New York,NY,USA : ASME , 2017 : V008T10A039 .

SHIAU C C , SAHIN I , WANG Nian , et al . Turbine vane endwall film cooling comparison from five filmhole design patterns and three upstream injection angles [J ] . Journal of Thermal Science and Engineering Applications , 2019 , 11 ( 3 ): 031012 .

HU Jianjun , AN Baitao . Film-cooling effectiveness on a turbine blade platform with various hole shapes and layouts [J ] . ASME Journal of Heat and Mass Transfer , 2024 , 146 ( 11 ): 113801 .

刘钊 , 丁玉强 , 谢晔航 , 等 . 气膜孔布置对透平端壁冷却和气动性能影响的研究 [J ] . 西安交通大学学报 , 2023 , 57 ( 8 ): 22 - 33 .

LIU Zhao , DING Yuqiang , XIE Yehang , et al . Study on effects of film hole arrangements on film cooling and aerodynamic characteristics of turbine endwall [J ] . Journal of Xi'an Jiaotong University , 2023 , 57 ( 8 ): 22 - 33 .

苏杭 . 优化气膜布局的导叶端壁冷却特性的实验研究 [D ] . 合肥 : 中国科学技术大学 , 2018 .

YANG Xing , LIU Zhansheng , ZHAO Qiang , et al . Comparisons of endwall overall effectiveness from two film hole distribution patterns at low and high exit Mach numbers [J ] . Journal of Turbomachinery , 2020 , 142 ( 10 ): 101007 .

薛兴旭 . 亚音速高负荷涡轮叶栅二次流动特征与控制研究 [D ] . 哈尔滨 : 哈尔滨工业大学 , 2021 .

THRIFT A A , THOLE K A , HADA S . Effects of an axisymmetric contoured endwall on a nozzle guide vane: convective heat transfer measurements [J ] . Journal of Turbomachinery , 2011 , 133 ( 4 ): 041008 .

KALIYAPERUMAL A , GOVARDHAN M . Reduction of secondary flow losses in transonic nozzle guide vane through axisymmetric endwall profile optimization [C ] // ASME 2017 Gas Turbine India Conference . New York,NY,USA : ASME , 2017 : V001T02A008 .

HUSSAIN S , LIU Jian , SUNDÉN B . Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane [J ] . Applied Thermal Engineering , 2020 , 168 : 114844 .

孙皓 , 宋立明 , 李军 . 透平叶栅非轴对称端壁优化设计 [J ] . 西安交通大学学报 , 2013 , 47 ( 9 ): 35 - 40 .

SUN Hao , SONG Liming , LI Jun . Optimization design of nonaxisymmetrical end wall profiling for turbine cascade [J ] . Journal of Xi'an Jiaotong University , 2013 , 47 ( 9 ): 35 - 40 .

沈鹏 , 刘洋 , 戴韧 . 非轴对称端壁抑制叶栅二次流分离的实验研究 [J ] . 热能动力工程 , 2021 , 36 ( 7 ): 32 - 38 .

SHEN Peng , LIU Yang , DAI Ren . Experimental research on contoured endwall depressing cascade secondary flow separation [J ] . Journal of Engineering for Thermal Energy and Power , 2021 , 36 ( 7 ): 32 - 38 .

张垲垣 , 李志刚 , 李军 . 透平端壁冷却及泛冷却最优的端壁造型设计研究 [J ] . 西安交通大学学报 , 2021 , 55 ( 5 ): 1 - 9 .

ZHANG Kaiyuan , LI Zhigang , LI Jun . Endwall contour design targeting on optimum turbine endwall cooling and phantom cooling effectiveness [J ] . Journal of Xi'an Jiaotong University , 2021 , 55 ( 5 ): 1 - 9 .

CHEN Pingting , LI Xueying , REN Jing , et al . Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance [J ] . International Journal of Heat and Mass Transfer , 2019 , 137 : 690 - 702 .

白波 , 李志刚 , 李军 . 轴向收敛造型对燃气涡轮叶栅端壁气膜冷却性能的影响 [J ] . 航空动力学报 , 2022 , 37 ( 5 ): 1042 - 1053 .

BAI Bo , LI Zhigang , LI Jun . Influence of axially-convergent contouring on cascade end wall film cooling characteristics in gas turbine [J ] . Journal of Aerospace Power , 2022 , 37 ( 5 ): 1042 - 1053 .

CHIESA P , LOZZA G , MAZZOCCHI L . Using hydrogen as gas turbine fuel [J ] . Journal of Engineering for Gas Turbines and Power , 2005 , 127 ( 1 ): 73 - 80 .

KIM B , MAI T D , VO D T , et al . Hydrogen combustion in two-stage high-pressure gas turbine—thermal and flow simulations for performance comparison with fossil fuels [J ] . International Journal of Engine Research , 2024 , 25 ( 3 ): 513 - 526 .

任静 , 李雪英 , 黄新宇 , 等 . 燃氢燃机高温高湿透平耦合传热和冷却特性 [J ] . 动力工程学报 , 2024 , 44 ( 9 ): 1416 - 1423 .

REN Jing , LI Xueying , HUANG Xinyu , et al . Coupled heat transfer and cooling characteristics of high temperature and high humidity turbine for hydrogenfired gas turbine [J ] . Journal of Chinese Society of Power Engineering , 2024 , 44 ( 9 ): 1416 - 1423 .

刘志敏 , 丁阳 , 徐婷婷 , 等 . 燃气轮机燃烧压力脉动与测量关键技术研究 [J ] . 华电技术 , 2019 , 41 ( 9 ): 1 - 5 .

LIU Zhimin , DING Yang , XU Tingting , et al . Research on gas turbine combustion pressure fluctuation and the key technologies for its measurement [J ] . Huadian Technology , 2019 , 41 ( 9 ): 1 - 5 .

吉冰 , 李军 , 王志多 . 脉动来流对涡轮非定常气动性能影响机理 [J ] . 航空动力学报 , 2020 , 35 ( 2 ): 410 - 421 .

JI Bing , LI Jun , WANG Zhiduo . Effect mechanism of pulsating flow on unsteady aerodynamic performance of turbine [J ] . Journal of Aerospace Power , 2020 , 35 ( 2 ): 410 - 421 .

LI Zhigang , BAI Bo , LI Jun , et al . Endwall heat transfer and cooling performance of a transonic turbine vane with upstream injection flow [J ] . Journal of Turbomachinery , 2022 , 144 ( 4 ): 041004 .

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

自适应采样涡轮叶顶气热性能不确定性量化与敏感性分析研究

尾迹影响下有复合角扇形孔涡轮叶片表面的气膜冷却效率实验研究

融合物理信息与深度算子网络的变压器绕组热-流场快速计算方法

语义区分和子图整合驱动的知识图谱表示学习方法

结构-语义-残差协同的图像压缩框架：面向隐私保护与高保真重建