Enhancing heat transfer in a rotating droplet-shaped pin-fins channel: Investigating the influence of rotational radius ratio and temperature ratio

被引:4
作者
Zhang, Xuejiao [1 ,2 ]
You, Ruquan [1 ,2 ,4 ]
Li, Haiwang [1 ,2 ]
Liu, Song [1 ,3 ]
机构
[1] Beihang Univ, Res Inst Aeroengine, Beijing 100191, Peoples R China
[2] Beihang Univ, Natl Key Lab Sci & Technol Aero Engines Aerothermo, Beijing 100191, Peoples R China
[3] China AECC Sichuan Gas Turbine Estab, Chengdu 610599, Sichuan, Peoples R China
[4] Adv Jet Prop Innovat Ctr AEAC, Beijing 101304, Peoples R China
关键词
Heat transfer; Droplet-shaped pin-fins; Rotational radius ratio; Temperature ratio; Turbine blade;
D O I
10.1016/j.applthermaleng.2024.122839
中图分类号
O414.1 [热力学];
学科分类号
摘要
A droplet -shaped pin -fins array is designed to optimize the heat transfer coefficient (HTC) in the trailing edge channel of turbine blades. Experimental testing was conducted under a wide range of conditions, including varying inlet Reynolds numbers (Re) ranging from 10,000 to 70,000, rotation numbers (Ro) from 0 to 1.0, temperature ratios (TR) from 0.04 to 0.22, rotational radius ratios (r/D) from 25.67 to 52.33, and Buoyancy numbers (Buo) from 0 to 2.55. The study reveals a significant increase in convective heat transfer on the trailing surface (TS) under rotational conditions, indicating enhanced heat transfer characteristics. Conversely, rotation negatively affects heat transfer on the leading surface (LS), reducing its effectiveness. Rotation accelerates fluid velocity near the TS of the radial outflow channel due to the Coriolis force, and causes cooler secondary flow fluid to impact the TS. HTC gradually decreases with rising TR at different dimensionless positions. The impact of r/D on HTC is also analyzed, showing a 10 % increase in average Nusselt numbe at a r/D of 52.33 compared to 25.67 at Re of 5,000. When Re, Ro, and Buo are kept constant, there is a significant approximately 20.8 % variation in the level of heat transfer, despite changes in TR and r/D. Maintaining consistent dimensionless parameters such as Re, Ro, Buo, TR, r/D, D is crucial for accurate HTC. These findings provide valuable insights for optimizing the understanding of HTC in internal cooling channels.
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页数:12
相关论文
共 31 条
[1]   Numerical and Experimental Investigation of Turning Flow Effects on Innovative Pin Fin Arrangements for Trailing Edge Cooling Configurations [J].
Bianchini, C. ;
Facchini, B. ;
Simonetti, F. ;
Tarchi, L. ;
Zecchi, S. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2012, 134 (02)
[2]   Dimensionless analysis of flow and heat transfer characteristics in a high-speed rotor-stator disk cavity based on similarity criteria [J].
Chang, Ran ;
Zhao, Yizhen ;
Guo, Miaoxin ;
Lin, Aqiang ;
Wang, Yangang ;
Liu, Gaowen .
APPLIED THERMAL ENGINEERING, 2024, 238
[3]   Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs [J].
Chen, I-Lun ;
Sahin, Izzet ;
Wright, Lesley M. ;
Han, Je-Chin ;
Krewinkel, Robert .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2021, 143 (08)
[4]   Pin-fin Shape and Orientation Effects on Wall Heat Transfer Predictions of Gas Turbine Blade [J].
Effendy, Marwan ;
Yao, Yufeng ;
Yao, Jun ;
Marchan, Denis R. .
EXPLORING RESOURCES, PROCESS AND DESIGN FOR SUSTAINABLE URBAN DEVELOPMENT, 2019, 2114
[5]  
Fu WL, 2005, PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 3 PTS A AND B, P453
[6]   Turbine blade cooling studies at Texas A&M University: 1980-2004 [J].
Han, JC .
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2006, 20 (02) :161-187
[7]   Experimental and numerical investigation on the film-cooling a gas turbine vane pressure side with various internal rib angles [J].
Huang, Kun ;
Cheng, Xiang ;
Yang, Xi ;
Lei, Jiang ;
Ji, Wen-Tao ;
Tao, Wen-Quan .
APPLIED THERMAL ENGINEERING, 2024, 239
[8]   Channel orientation effect on endwall heat transfer in rotating cooling passages with pin-fins [J].
Huang, Szu-Chi ;
Wang, Chen-Chih ;
Liu, Yao-Hsien .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 136 :1115-1126
[9]   Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers [J].
Huh, Michael ;
Lei, Jiang ;
Han, Je-Chin .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2012, 134 (01)
[10]   Comparison of Pin Surface Heat Transfer in Arrays of Oblong and Cylindrical Pin Fins [J].
Kirsch, Kathryn L. ;
Ostanek, Jason K. ;
Thole, Karen A. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2014, 136 (04)