陶瓷基复合材料在航空发动机热端部件应用及热分析研究进展

Kun Du; Qi Hao Chen; Xian Long Meng; Li Quan Wang; Xiang Peng Pei; Ying Chen Jiao; Hua Rong Li; Cun Liang Liu

doi:10.13675/j.cnki.tjjs.210380

陶瓷基复合材料在航空发动机热端部件应用及热分析研究进展

Translated title of the contribution: Advancement in Application and Thermal Analysis of Ceramic Matrix Composites in Aeroengine Hot Components

Kun Du, Qi Hao Chen, Xian Long Meng, Li Quan Wang, Xiang Peng Pei, Ying Chen Jiao, Hua Rong Li, Cun Liang Liu

School of Power and Energy

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

25 Scopus citations

Abstract

Ceramic Matrix Composites(CMC), with low density and high thermal resistance, has been regarded as the potential thermal structure material for the future. Currently, the preparation technology, performance-based design and the application of the CMC are highlights in aeroengine and the rocket engine research field. Nevertheless, the anisotropy properties of CMC due to the internal structural and the difference between matrix and fibers lead to big challenges and difficulties for the hot components design and manufacturing. The present paper aims to analyze the development of CMC applications in aeroengine based on a brief review of the relevant public research work. Meanwhile, some suggestions for CMC components thermal analysis were proposed for the potential research.

Translated title of the contribution	Advancement in Application and Thermal Analysis of Ceramic Matrix Composites in Aeroengine Hot Components
Original language	Chinese (Traditional)
Pages (from-to)	107-125
Number of pages	19
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	43
Issue number	2
DOIs	https://doi.org/10.13675/j.cnki.tjjs.210380
State	Published - Feb 2022

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title = "陶瓷基复合材料在航空发动机热端部件应用及热分析研究进展",

abstract = "Ceramic Matrix Composites(CMC), with low density and high thermal resistance, has been regarded as the potential thermal structure material for the future. Currently, the preparation technology, performance-based design and the application of the CMC are highlights in aeroengine and the rocket engine research field. Nevertheless, the anisotropy properties of CMC due to the internal structural and the difference between matrix and fibers lead to big challenges and difficulties for the hot components design and manufacturing. The present paper aims to analyze the development of CMC applications in aeroengine based on a brief review of the relevant public research work. Meanwhile, some suggestions for CMC components thermal analysis were proposed for the potential research.",

keywords = "Aeroengine, Ceramic matrix composites, Combustor, Hot components, Turbine",

author = "Kun Du and Chen, {Qi Hao} and Meng, {Xian Long} and Wang, {Li Quan} and Pei, {Xiang Peng} and Jiao, {Ying Chen} and Li, {Hua Rong} and Liu, {Cun Liang}",

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AU - Du, Kun

AU - Chen, Qi Hao

AU - Meng, Xian Long

AU - Wang, Li Quan

AU - Pei, Xiang Peng

AU - Jiao, Ying Chen

AU - Li, Hua Rong

AU - Liu, Cun Liang

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AB - Ceramic Matrix Composites(CMC), with low density and high thermal resistance, has been regarded as the potential thermal structure material for the future. Currently, the preparation technology, performance-based design and the application of the CMC are highlights in aeroengine and the rocket engine research field. Nevertheless, the anisotropy properties of CMC due to the internal structural and the difference between matrix and fibers lead to big challenges and difficulties for the hot components design and manufacturing. The present paper aims to analyze the development of CMC applications in aeroengine based on a brief review of the relevant public research work. Meanwhile, some suggestions for CMC components thermal analysis were proposed for the potential research.

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KW - Turbine

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陶瓷基复合材料在航空发动机热端部件应用及热分析研究进展

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