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Improvement of Film Cooling Design for Turbine Vane Leading Edge Considering Combustor Outflow

WANG Xinyu LIU Cunliang FU Zhongyi LI Yang ZHU Huiren

热科学学报（英文版）2024，Vol.33Issue(1)：311-327,17.

热科学学报（英文版）2024，Vol.33Issue(1)：311-327,17.DOI:10.1007/s11630-023-1878-8

Improvement of Film Cooling Design for Turbine Vane Leading Edge Considering Combustor Outflow

WANG Xinyu ¹LIU Cunliang ¹FU Zhongyi ²LI Yang ²ZHU Huiren¹

作者信息

1. School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China
2. AECC Hunan Aviation Powerplant Research Institute,Zhuzhou 412002,China
折叠

摘要

关键词

turbine vane/showerhead cooling/swirling inflow/laid-back-fan-shaped hole/film hole inclination

Key words

turbine vane/showerhead cooling/swirling inflow/laid-back-fan-shaped hole/film hole inclination

引用本文复制引用

WANG Xinyu,LIU Cunliang,FU Zhongyi,LI Yang,ZHU Huiren..Improvement of Film Cooling Design for Turbine Vane Leading Edge Considering Combustor Outflow[J].热科学学报（英文版）,2024,33(1):311-327,17.

基金项目

The authors acknowledge gratefully the financial support from the National Natural Science Foundation of China(Grant No.U2241268),the Natural Science Foundation of Hunan Province(Grant No.2021JJ40646),the National Science and Technology Major Project(Grant No.J2019-Ⅲ-0019-0063),and the Innovation Capacity Support Plan in Shaanxi Province of China(Grant No.2023-CX-TD-19). （Grant No.U2241268）

热科学学报（英文版）

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ISSN：1003-2169

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