TY - GEN
T1 - EXPERIMENTAL INVESTIGATION ON HEAT TRANSFER CHARACTERISTICS IN AN IMPINGEMENT/EFFUSION COOLING SYSTEM OF A RIBBED TURBINE CASING
AU - Li, Guodong
AU - Guo, Tao
AU - Qiu, Changbo
AU - Liu, Cunliang
AU - Zhu, Huiren
AU - Li, Jichen
N1 - Publisher Copyright:
Copyright © 2022 by ASME.
PY - 2022
Y1 - 2022
N2 - The present paper reports an impingement/effusion cooling structure applied to the turbine casing. The structure consists of three rows of jet holes and two rows of effusion holes, both of which are in a staggered arrangement. A high rib exists inside the impinging chamber for structural support, which is connected to the effusion plate and divides the impinging chamber into two interconnected small chambers, one of which is arranged with effusion holes and the other is not. Transient liquid crystal (TLC) experiments were conducted to investigate the influence of the Reynolds number based on the jet hole diameter (ReD), distance between impingement plate and effusion plate(H), hole pith in Y direction(A) and X direction(C), with a parameter range of 1100 ≤ ReD ≤ 5100, 2.5 ≤ H/D ≤ 7.5, 4.0 ≤ A/D ≤ 14.0 and 8.0 ≤ C/D ≤ 14.0, on the heat transfer characteristics of the effusion plate. The results show that the region averaged Nu increases with an increase in ReD for all studied cases and there is a linear relationship between the ReD and the region averaged Nu in the logarithmic coordinate. The change of H/D has an obvious effect on the heat transfer in the 2D-3D region from the stagnation point. As the H/D increases, the entrainment effect that makes the surrounding fluid continuously enter the jet, resulting in the velocity of the jet decreasing, and the enhanced heat transfer at the effusion plate becomes weaker. When 38
AB - The present paper reports an impingement/effusion cooling structure applied to the turbine casing. The structure consists of three rows of jet holes and two rows of effusion holes, both of which are in a staggered arrangement. A high rib exists inside the impinging chamber for structural support, which is connected to the effusion plate and divides the impinging chamber into two interconnected small chambers, one of which is arranged with effusion holes and the other is not. Transient liquid crystal (TLC) experiments were conducted to investigate the influence of the Reynolds number based on the jet hole diameter (ReD), distance between impingement plate and effusion plate(H), hole pith in Y direction(A) and X direction(C), with a parameter range of 1100 ≤ ReD ≤ 5100, 2.5 ≤ H/D ≤ 7.5, 4.0 ≤ A/D ≤ 14.0 and 8.0 ≤ C/D ≤ 14.0, on the heat transfer characteristics of the effusion plate. The results show that the region averaged Nu increases with an increase in ReD for all studied cases and there is a linear relationship between the ReD and the region averaged Nu in the logarithmic coordinate. The change of H/D has an obvious effect on the heat transfer in the 2D-3D region from the stagnation point. As the H/D increases, the entrainment effect that makes the surrounding fluid continuously enter the jet, resulting in the velocity of the jet decreasing, and the enhanced heat transfer at the effusion plate becomes weaker. When 38
KW - Heat transfer characteristics
KW - Impingement/effusion cooling system
KW - Low jet Reynolds numbers
KW - Transient liquid crystal Thermography
KW - Turbine casing
UR - http://www.scopus.com/inward/record.url?scp=85141219339&partnerID=8YFLogxK
U2 - 10.1115/GT2022-82346
DO - 10.1115/GT2022-82346
M3 - 会议稿件
AN - SCOPUS:85141219339
T3 - Proceedings of the ASME Turbo Expo
BT - Heat Transfer - General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, GT 2022
Y2 - 13 June 2022 through 17 June 2022
ER -