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Optimization and Evaluation of Cooling Structure of Stage 1 Blade of Heavy-Duty Gas Turbine
Power Generation Technology Vol. 45, Issue 5, Pages: 838-846(2024)
Gas Turbine Power Generation Technology|Updated：2025-06-15
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Optimization and Evaluation of Cooling Structure of Stage 1 Blade of Heavy-Duty Gas Turbine
- “In the field of localization of core components of heavy-duty gas turbines, experts have significantly improved the reliability of blades in high-temperature environments by optimizing the structure of the first stage moving blades, providing theoretical basis for the localization of gas turbines.”
DOI：10.12096/j.2096-4528.pgt.24101
Revised：2024-08-12
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Related Author
ZHANG Chao
ZHANG Haichuan
FU Jinglun
TONG Zhiting
ZHU Junqiang
LI Shihan
BAI Bo
CHENG Guoqiang
Related Institution
Advanced Gas Turbine Laboratory (Institute of Engineering Thermophysics, Chinese Academy of Sciences), Haidian District
University of Chinese Academy of Sciences, Haidian District
National Demonstration Center for Experimental Mechanical and Electrical Engineering Education (Tianjin University of Technology), Xiqing District
Tianjin Key Laboratory for Advanced Mechatronic System Design and Intelligent Control (School of Mechanical Engineering, Tianjin University of Technology), Xiqing District
State Key Laboratory of Clean and Efficient Turbomachinery Power Equipment
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