Coupling characteristics and simplification analysis method of laminated cooling configuration between external and internal cooling

被引:6
作者
Li, Honglin [1 ]
Li, Lei [1 ]
Li, Qi [3 ]
Tang, Zhonghao [1 ,2 ]
Zhang, Zhenyuan [1 ]
Chen, Ruiqing [1 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Civil Engn & Architecture, Xian, Peoples R China
[2] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China
[3] ENN Energy Power Technol Shanghai Co Ltd, Shanghai, Peoples R China
基金
中国国家自然科学基金; 上海市自然科学基金;
关键词
Gas turbine cooling; Laminated cooling; Decoupled method; Simplification method; HEAT-TRANSFER; NUMERICAL-SIMULATION; IMPINGEMENT; JETS; FLOW;
D O I
10.1016/j.ijthermalsci.2023.108159
中图分类号
O414.1 [热力学];
学科分类号
摘要
This study presents a method to decouple the cooling process of laminated cooling configuration and analyze the coupling characteristics between internal and external cooling. Based on it, two simplification methods of external cooling are developed to predict the coupled cooling performance and its distribution. Employing verified numerical method, five series of cooling process simulations are conducted under different blowing ratios. Results show that, the similar vortices structure among coupled, internal, and external cooling demon-strate that the decoupled method can effectively decouple the internal and external cooling and keep the same flow pattern. In laminated cooling, internal cooling contributes most of cooling performance and heat transfer capacity, and external cooling mainly influences the distribution characteristics due to its intensively regional cooling performance. While coupled cooling presents superposition characteristics of internal and external cooling, they will counteract about 17.88% cooling performance. The almost same local and overall cooling effectiveness and distribution under different blowing ratios demonstrate that simplifying external cooling to convective boundary condition and replacing with external cooling correlation formulas can effectively capture cooling performance and heat transfer characteristics with an average error of 12.91%. Further, the presented prediction formula can effectively predict area-averaged cooling effectiveness with maximum deviation of 8.8%.
引用
收藏
页数:15
相关论文
共 40 条
[1]   Gas turbine film cooling [J].
Bogard, DG ;
Thole, KA .
JOURNAL OF PROPULSION AND POWER, 2006, 22 (02) :249-270
[2]  
Bradley A., 2009, PREDICTION VANE LM C
[3]  
Bunker RS, 2017, PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 1
[4]  
Colladay R.S., 1972, Analysis and comparison of wall cooling schemes for advanced gas turbine applications
[5]  
Deng Q., 2016, CONJUGATE HEAT TRA B, V49781
[6]  
Funazaki K., 2003, ASME TURBO EXPO 2003, V5, P185, DOI [10.1115/gt2003-38256, DOI 10.1115/GT2003-38256]
[7]  
Funazaki K., 2001, ASME TURBO EXPO 2001
[8]   Numerical simulation of broken pin effects on the flow field and cooling performance of a double-wall cooling configuration [J].
Gao, Wenjing ;
Li, Honglin ;
Li, Lei ;
Zhao, Zhe'nan ;
Yue, Zhufeng .
CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (02) :358-375
[9]  
Goldstein R.J., 1971, Film Cooling, Advances in Heat and Mass Transfer, V7, P321
[10]   Effect of impingement jet on the full-coverage film cooling system with double layered wall [J].
Jung, Eui Yeop ;
Oh, Sang Hyun ;
Lee, Dong Hyun ;
Kim, Kyung Min ;
Cho, Hyung Hee .
EXPERIMENTAL HEAT TRANSFER, 2017, 30 (06) :544-562