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材料导报  2023, Vol. 37 Issue (14): 22010147-8    https://doi.org/10.11896/cldb.22010147
  无机非金属及其复合材料 |
航空发动机用SiC/SiC复合材料典型元件设计及性能评价研究进展
刘虎1, 束小文2, 洪智亮3, 杨金华1, 郭洪宝3, 孙世杰1, 焦健1,*
1 中国航发北京航空材料研究院先进复合材料科技重点实验室,北京 100095
2 陆军装备部航空军事代表局驻北京地区航空军事代表室,北京 100101
3 中国航发商用航空发动机有限责任公司,上海 200241
Research Progress on Design and Evaluation of Typical SiC/SiC Composite Sub-elements Used for Aero Engines
LIU Hu1, SHU Xiaowen2, HONG Zhiliang3, YANG Jinhua1, GUO Hongbao3, SUN Shijie1, JIAO Jian1,*
1 National Key Laboratory of Advanced Composites, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China
2 Army Aviation Representative Office in Beijing, Affiliated with the Equipment Department of People’s Liberation Army Ground Force, Beijing 100101, China
3 AECC Commercial Aircraft Engine Co., Ltd., Shanghai 200241, China
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摘要 SiC/SiC复合材料具有轻质、耐高温、高强度等优点,已在国外航空发动机热端部件上大量应用并取得积极效果。作为航空发动机关键材料“积木式”评价技术中的重要组成部分,元件级评价是连接材料级测试和部件级考核的桥梁纽带,对促进材料在部件上的应用至关重要。本文梳理了航空发动机热端部件中几种典型的SiC/SiC复合材料元件,包括开孔、“C”形、“T”形、筒形及翼形元件等,综述了针对不同类型元件所开展的评价试验及测试方法,包括力学性能测试、服役环境性能评价等,阐述了结构特征、材料性质等因素对元件损伤行为和失效机制的影响,最后提出我国在完善航空发动机用SiC/SiC复合材料元件研究方面的建议。
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刘虎
束小文
洪智亮
杨金华
郭洪宝
孙世杰
焦健
关键词:  SiC/SiC复合材料  典型元件  “积木式”验证  航空发动机    
Abstract: Continuous SiC fiber reinforced SiC matrix (SiC/SiC) composites have been widely used in hot-section components of aero engines due to their excellent properties such as light weight, high strength, and high temperature resistance. As an important part of the ‘building block’ approach in the evaluation of key aero engine materials, sub-element evaluation acts as a key stepping stone in bridging basic coupon testing and more complex component verification and validation. Here, typical forms of SiC/SiC composite sub-elements with structural characteristics such as open holes, and different shapes, e.g. ‘C’, ‘T’, cylinder and airfoil were reviewed. Meanwhile, the experiments performed, including mechanical test and service performance evaluation, were summarized, along with the mechanism of damage and failure with different characteristic structure and test conditions. Further, suggestions were proposed about research on SiC/SiC composite sub-elements for domestic aero engine developments.
Key words:  SiC/SiC ceramic matrix composite    typical sub-elements    ‘building block’ approach    aero engine
出版日期:  2023-07-25      发布日期:  2023-07-24
ZTFLH:  TB332  
基金资助: 国家科技重大专项(2017-VI-0007-0077)
通讯作者:  *焦健,研究员,硕士研究生导师,现任中国航发北京航空材料研究院表面工程研究所副所长。2006年获德国斯图加特大学自然科学博士学位,目前主要从事陶瓷基复合材料研制与应用研究,发表学术论文120余篇,获授权国家发明专利30 余项,出版译作1部。jian.jiao@biam.ac.cn   
作者简介:  刘虎,中国航发北京航空材料研究院高级工程师,2014年于东南大学获得应用化学专业博士学位,毕业后入职北京航空材料研究院至今,目前主要从事陶瓷基复合材料制备工艺研究。发表学术论文30余篇,获授权国家发明专利10余项。
引用本文:    
刘虎, 束小文, 洪智亮, 杨金华, 郭洪宝, 孙世杰, 焦健. 航空发动机用SiC/SiC复合材料典型元件设计及性能评价研究进展[J]. 材料导报, 2023, 37(14): 22010147-8.
LIU Hu, SHU Xiaowen, HONG Zhiliang, YANG Jinhua, GUO Hongbao, SUN Shijie, JIAO Jian. Research Progress on Design and Evaluation of Typical SiC/SiC Composite Sub-elements Used for Aero Engines. Materials Reports, 2023, 37(14): 22010147-8.
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http://www.mater-rep.com/CN/10.11896/cldb.22010147  或          http://www.mater-rep.com/CN/Y2023/V37/I14/22010147
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