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Review of Advanced Effusive Cooling for Gas Turbine Blades

Author

Listed:
  • Wen Wang

    (School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310007, China
    ZJUI Institute, Zhejiang University, Haining 314400, China)

  • Yan Yan

    (School of Advanced Technology, Xi’an Jiaotong-Liverpool University, Suzhou 215123, China)

  • Yeqi Zhou

    (ZJUI Institute, Zhejiang University, Haining 314400, China)

  • Jiahuan Cui

    (School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310007, China
    ZJUI Institute, Zhejiang University, Haining 314400, China)

Abstract

Turbine inlet temperature has continuously increased to improve gas turbine performance during the past few decades. Although internal convection cooling and traditional film cooling have contributed significantly to the current achievement, advanced cooling schemes are needed to minimize the coolant consumption and maximize the cooling efficiency for future gas turbines. This paper conducts a comprehensive review of advanced effusive cooling schemes for gas turbine blades. First, the background and the history of turbine blade cooling are introduced. Then, the metrics of effusive cooling efficiency are defined. Next, effusion cooling, impingement/effusion cooling, and transpiration cooling are reviewed. The flow and heat transfer mechanisms of the cooling schemes are emphasized, and the design trends of the cooling schemes are revealed. Finally, the conclusions and future research perspectives are summarized.

Suggested Citation

  • Wen Wang & Yan Yan & Yeqi Zhou & Jiahuan Cui, 2022. "Review of Advanced Effusive Cooling for Gas Turbine Blades," Energies, MDPI, vol. 15(22), pages 1-28, November.
    • Handle: RePEc:gam:jeners:v:15:y:2022:i:22:p:8568-:d:974501
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    References listed on IDEAS

    as
    1. Sandip Dutta & Prashant Singh, 2021. "Opportunities in Jet-Impingement Cooling for Gas-Turbine Engines," Energies, MDPI, vol. 14(20), pages 1-29, October.
    2. Ke Tian & Zicheng Tang & Jin Wang & Milan Vujanović & Min Zeng & Qiuwang Wang, 2021. "Numerical Investigations of Film Cooling and Particle Impact on the Blade Leading Edge," Energies, MDPI, vol. 14(4), pages 1-14, February.
    3. Maghrabie, Hussein M., 2021. "Heat transfer intensification of jet impingement using exciting jets - A comprehensive review," Renewable and Sustainable Energy Reviews, Elsevier, vol. 139(C).
    4. Liaqat Hussain & Muhammad Mahabat Khan & Manzar Masud & Fawad Ahmed & Zabdur Rehman & Łukasz Amanowicz & Krzysztof Rajski, 2021. "Heat Transfer Augmentation through Different Jet Impingement Techniques: A State-of-the-Art Review," Energies, MDPI, vol. 14(20), pages 1-40, October.
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    Cited by:

    1. Chen, Zhimin & Chen, Xuejiao & Yang, XuFei & Yu, Bo & Wang, Bohong & Zhu, Jianqin & Chen, Yujie & Cai, Weihua, 2024. "Numerical study on cooling characteristics of turbine blade based on laminated cooling configuration with clapboards," Energy, Elsevier, vol. 299(C).
    2. Hao Xia & Xiaosheng Chen & Christopher D. Ellis, 2024. "Modelling and Simulation of Effusion Cooling—A Review of Recent Progress," Energies, MDPI, vol. 17(17), pages 1-30, September.

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