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航空发动机空气系统气源引气的研究进展

赵斌 李绍斌 周盛 黄生勤 邹学奇

航空工程进展2012,Vol.3Issue(4):476-485,10.
航空工程进展2012,Vol.3Issue(4):476-485,10.

航空发动机空气系统气源引气的研究进展

Research Progress on the Aircraft Engine Air System Bleeding

赵斌 1李绍斌 2周盛 2黄生勤 3邹学奇3

作者信息

  • 1. 中航空天发动机研究院有限公司基础技术研究中心,北京100028
  • 2. 北京航空航天大学航空发动机气动热力国防科技重点实验室,北京100191
  • 3. 中国航空工业集团公司中国航空动力机械研究所,株洲412002
  • 折叠

摘要

Abstract

Air system is mainly used for cooling the engine hot components and cabin air conditioning, and supports the safe and reliable operation of aircraft engines. Air system is closely related to the aerodynamic performance of the com pressor because it changes the air flow within the compressor by extracting bleed air from the compressor. The flow rate of the air system keeps growing to meet the demand of multiple aircraft functions, various external environment and higher turbine inlet temperature. The growing flow rate of air system highlights the impact of air system on the compressor aerodynamic performance. The characteristics of the air system bleeding is analyzed, sums up the progress on the research of the inter-stage bleeding of the compressor both home and abroad is summed up, and the future de velopment and application of the air system bleeding research are explored.

关键词

航空发动机/空气系统引气/压气机/气动性能/设计体系

Key words

aircraft engine/air system bleeding/compressor/aerodynamic performance~ design system

分类

航空航天

引用本文复制引用

赵斌,李绍斌,周盛,黄生勤,邹学奇..航空发动机空气系统气源引气的研究进展[J].航空工程进展,2012,3(4):476-485,10.

基金项目

国家自然科学基金 ()

航空工程进展

1674-8190

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