大型科学装置在航空发动机高温结构材料和涂层上的研究与应用

doi:10.7527/S1000-6893.2022.27481

材料工程与机械制造

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大型科学装置在航空发动机高温结构材料和涂层上的研究与应用

尚勇¹, 冯阳¹, 刘巧沐^1,2, 王君武^3,4, 杨惠君¹, 茹毅¹, 张恒¹, 赵文月¹, 裴延玲¹, 李树索³, 宫声凯¹

1. 北京航空航天大学前沿科学技术创新研究院, 北京 100191;
2. 中国航发四川燃气涡轮研究院, 成都 610599;
3. 北京航空航天大学航空发动机研究院, 北京 100191;
4. 贵阳航发精密铸造有限公司, 贵阳 550000

收稿日期:2022-05-20 修回日期:2022-06-05 发布日期:2022-07-14
通讯作者: 宫声凯,E-mail:gongks@buaa.edu.cn E-mail:gongks@buaa.edu.cn
基金资助:
北京市自然科学基金（2222060）；国家科技重大专项（2017-VI-0016-0088）

Research and application of large scientific facility on high-temperature structural materials and coatings of aero-engine

SHANG Yong¹, FENG Yang¹, LIU Qiaomu^1,2, WANG Junwu^3,4, YANG Huijun¹, RU Yi¹, ZHANG Heng¹, ZHAO Wenyue¹, PEI Yanling¹, LI Shusuo³, GONG Shengkai¹

1. Research Institute for Frontier Science, Beihang University, Beijing 100191, China;
2. AECC Sichuan Gas Turbine Research Institute, Chengdu 610599, China;
3. Research Institute of Aero-Engine, Beihang University, Beijing 100191, China;
4. Guiyang Aero-engine Precision Casting Co. LTD, Guiyang 550000, China

Received:2022-05-20 Revised:2022-06-05 Published:2022-07-14
Supported by:
Beijing Municipal Natural Science Foundation (2222060); National Science and Technology Major Project (2017-VI-0016-0088)

摘要/Abstract

摘要： 航空发动机用热端部件及其防护涂层具有密度高、结构复杂、服役环境恶劣、承受载荷复杂等特点，采用传统的分析测试方法对其进行损伤演变、质量评估和寿命预测研究存在极大挑战，无法满足航空发动机更高温度、更高速度、更高可靠性的需求。大型科学装置中的同步辐射技术和中子衍射技术具有高穿透性、高精度、高耦合度和高通量等特点，较传统检测技术更适用于未来航空航天领域高温结构材料的研发和测试，但上述两种技术在中国相关领域的基础研究和工程应用方面仍需进一步开展工作。本文着重介绍近年来国内外采用同步辐射和中子衍射技术进行航空发动机热端部件及其防护涂层基础科学研究与实际工程应用方面的进展与现状。

关键词: 高温合金, 热障涂层, 同步辐射, 中子衍射, 无损检测, 残余应力

Abstract: The characteristic of high temperature structural materials and coatings of aero-engine exhibit as high density, complex structure, extremely condition, complex load. It is a great challenge of traditional testing technology for high temperature structural materials and coatings on its research of failure mechanism, nondestructive testing, and life prediction, which cannot achieve the requirements of higher temperature, higher speed and higher reliability for aero-engine. The technology of the large scientific facilities of synchrotron radiation and neutron scattering technique with such excellent performance of high penetrability, high precision, high coupling and the characteristics of high flux, which is more suitable for the research and applications on aero-engine high temperature structural materials and coatings in the future. However, the improvement of investigations is still required for further investigation, such as related algorithm, special line station and typical environment. This paper focuses on the research and engineering applications of synchrotron radiation and neutron scattering techniques for high temperature structural materials and coatings of aero-engines in recent years.

Key words: superalloy, thermal barrier coating, synchrotron radiation, neutron diffraction, nondestructive testing, residual stress

中图分类号:

V257

尚勇, 冯阳, 刘巧沐, 王君武, 杨惠君, 茹毅, 张恒, 赵文月, 裴延玲, 李树索, 宫声凯. 大型科学装置在航空发动机高温结构材料和涂层上的研究与应用[J]. 航空学报, 2022, 43(10): 527481-527481.

SHANG Yong, FENG Yang, LIU Qiaomu, WANG Junwu, YANG Huijun, RU Yi, ZHANG Heng, ZHAO Wenyue, PEI Yanling, LI Shusuo, GONG Shengkai. Research and application of large scientific facility on high-temperature structural materials and coatings of aero-engine[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527481-527481.

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

大型科学装置在航空发动机高温结构材料和涂层上的研究与应用

Research and application of large scientific facility on high-temperature structural materials and coatings of aero-engine

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