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Journal of Inorganic Materials, Volume. 39, Issue 10, 1077(2024)

Thermal Spray Coatings for Aircraft CMC Hot-end Components: Opportunities and Challenges

Shunyan TAO1... Jiasheng YANG1, Fang SHAO1, Yingchen WU1,2, Huayu ZHAO1, Shaoming DONG3, Xiangyu ZHANG3 and Ying XIONG4 |Show fewer author(s)
Author Affiliations
  • 11. Key Laboratory of Inorganic Coating Materials CAS, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 201899, China
  • 22. University of Chinese Academy of Sciences, Beijing 100049, China
  • 33. State Key Laboratory of High Performance Ceramics and Superfine Microstructure, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 200050, China
  • 44. AECC Shenyang Liming Aero-Engine Co., Ltd., Shenyang 110043, China
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    Figures & Tables(10)
    Inlet gas temperatures corresponding to aero-engines with different thrust-weight ratios
    1. Inlet gas temperatures corresponding to aero-engines with different thrust-weight ratios

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    Contribution of changes in high temperature alloy process to engine performance improvement [1]
    2. Contribution of changes in high temperature alloy process to engine performance improvement [1]

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    Relationship between NOx emission and combustion chamber outlet temperature[2]
    3. Relationship between NOx emission and combustion chamber outlet temperature[2]

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    Material selection scheme and its corresponding temperature bearing characteristics of engine hot-end components[5-6]
    4. Material selection scheme and its corresponding temperature bearing characteristics of engine hot-end components[5-6]

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    Shroud ring coating components of CMC turbine for CFM Leap-1A and Leap-1B engines[1]
    5. Shroud ring coating components of CMC turbine for CFM Leap-1A and Leap-1B engines[1]

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    Near-infrared spectral reflectance of APS-EBCs and APS-TBCs
    6. Near-infrared spectral reflectance of APS-EBCs and APS-TBCs

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    Designed TEBCs with multi-layer structure of functional partition
    7. Designed TEBCs with multi-layer structure of functional partition

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    Relationship between the water-oxygen corrosion rate and the thermal expansion coefficient of ceramic materials[24]
    8. Relationship between the water-oxygen corrosion rate and the thermal expansion coefficient of ceramic materials[24]

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    TBC-ASCs for shroud ring of the first stage turbine of high temperature alloy material[40]
    9. TBC-ASCs for shroud ring of the first stage turbine of high temperature alloy material[40]

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    Schematic drawing of the Sulzer Innotec abradability test rig [44]
    10. Schematic drawing of the Sulzer Innotec abradability test rig [44]

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    Shunyan TAO, Jiasheng YANG, Fang SHAO, Yingchen WU, Huayu ZHAO, Shaoming DONG, Xiangyu ZHANG, Ying XIONG. Thermal Spray Coatings for Aircraft CMC Hot-end Components: Opportunities and Challenges[J]. Journal of Inorganic Materials, 2024, 39(10): 1077

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    Paper Information

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    Received: Mar. 25, 2024

    Accepted: --

    Published Online: Dec. 13, 2024

    The Author Email:

    DOI:10.15541/jim20230565

    Topics

    laser devices and laser physics
    Lasers and Laser Optics
    Laser physics
    laser manufacturing
    Instrumentation, Measurement and Metrology