TY - JOUR
T1 - Numerical simulation of broken pin effects on the flow field and cooling performance of a double-wall cooling configuration
AU - GAO, Wenjing
AU - LI, Honglin
AU - LI, Lei
AU - ZHAO, Zhe'nan
AU - YUE, Zhufeng
N1 - Publisher Copyright:
© 2020 Chinese Society of Aeronautics and Astronautics
PY - 2021/2
Y1 - 2021/2
N2 - In this paper, the flow characteristics of the double wall structure are presented and the effect of the broken pin size on the cooling performance and flow field of the double wall configuration is investigated. A periodic plate model with seven units is adopted, and there are an impingement hole and a film hole in each unit. Under five blowing ratios, six different sizes of the broken pin are compared, and the double wall configuration without broken pins is taken as the baseline. The results show that if the broken pins height is too small, the cooling effectiveness usually cannot be improved. With the presence of broken pins with a height of more than 0.4, the effectiveness is improved due to the enhancement of reattachment and recirculation of coolant. With the increase of the broken pin height, the cooling effectiveness increases. However, the increase of the diameter does not always improve the cooling performance, since the limiting effect of the wall jet. In this study, Case 6 with the largest broken pin always has the best cooling performance, but also the largest flow resistance. In Case 6 temperature is reduced by almost 15 K compared to the baseline, and more areas have relatively higher cooling effectiveness.
AB - In this paper, the flow characteristics of the double wall structure are presented and the effect of the broken pin size on the cooling performance and flow field of the double wall configuration is investigated. A periodic plate model with seven units is adopted, and there are an impingement hole and a film hole in each unit. Under five blowing ratios, six different sizes of the broken pin are compared, and the double wall configuration without broken pins is taken as the baseline. The results show that if the broken pins height is too small, the cooling effectiveness usually cannot be improved. With the presence of broken pins with a height of more than 0.4, the effectiveness is improved due to the enhancement of reattachment and recirculation of coolant. With the increase of the broken pin height, the cooling effectiveness increases. However, the increase of the diameter does not always improve the cooling performance, since the limiting effect of the wall jet. In this study, Case 6 with the largest broken pin always has the best cooling performance, but also the largest flow resistance. In Case 6 temperature is reduced by almost 15 K compared to the baseline, and more areas have relatively higher cooling effectiveness.
KW - Broken pin
KW - Computational Fluid Dynamics
KW - Cooling performance
KW - Double wall configuration
KW - Turbine blades
UR - http://www.scopus.com/inward/record.url?scp=85097092410&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2020.09.014
DO - 10.1016/j.cja.2020.09.014
M3 - 文章
AN - SCOPUS:85097092410
SN - 1000-9361
VL - 34
SP - 358
EP - 375
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 2
ER -