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陶瓷基复合材料叶片发汗冷却技术现状与展望

LI Guangchao QIAO Chuhan ZHAO Zhiqi HONG Chao ZHAO Changyu

沈阳航空航天大学学报2025,Vol.42Issue(6):1-11,11.
沈阳航空航天大学学报2025,Vol.42Issue(6):1-11,11.DOI:10.3969/j.issn.2095-1248.2025.06.001

陶瓷基复合材料叶片发汗冷却技术现状与展望

Transpiration cooling technology for ceramic matrix composite blade:review and prospect

LI Guangchao 1QIAO Chuhan 1ZHAO Zhiqi 1HONG Chao 1ZHAO Changyu1

作者信息

  • 1. College of Aero-engine,Shenyang Aerospace University,Shenyang 110136,China
  • 折叠

摘要

Abstract

To ensure the normal operation of turbine blades Facing continuously increasing turbine inlet temperatures,the development of more efficient cooling technologies has become particularly urgent.Ceramic matrix composite(CMC)transpiration cooling technology combines the excellent high-temperature resistance of CMC with the efficient heat dissipation potential of transpiration cooling,showing broad application prospects in future thermal protection of turbine blades.However,the strong anisotropy of CMC materials and their complex internal porous structure pose significant challenges for the thermal analysis of the transpiration cooling process,and the underlying flow and heat transfer mechanisms remain unclear.This review summarized recent research progress on the anisotropic thermal conductivity and microporous seepage characteristics of CMC,analyzed key existing problems and challenges in current studies,and offerd suggestions for establishing a comprehensive design framework for CMC turbine blade transpiration cooling structures.

关键词

陶瓷基复合材料/发汗冷却/各向异性导热系数/微孔隙渗流/CMC涡轮叶片

Key words

ceramic matrix composite/transpiration cooling/anisotropic thermal conductivity/microporous seepage/CMC turbine blade

分类

航空航天

引用本文复制引用

LI Guangchao,QIAO Chuhan,ZHAO Zhiqi,HONG Chao,ZHAO Changyu..陶瓷基复合材料叶片发汗冷却技术现状与展望[J].沈阳航空航天大学学报,2025,42(6):1-11,11.

基金项目

国家自然科学基金(项目编号:52376028). (项目编号:52376028)

沈阳航空航天大学学报

2095-1248

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