中国民航大学学报

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航空燃气涡轮发动机分析

田川1,曹惠玲2   

  1. (1.厦门航空有限责任公司,厦门361006;2.中国民航大学航空工程学院,天津300300)
  • 收稿日期:2012-07-04 修回日期:2012-09-21 出版日期:2014-02-24 发布日期:2014-01-02
  • 作者简介:田川(1989—),男,河北保定人,工程师,学士,研究方向为航空发动机状态性能分析.

Exergy analysis of gas turbine engine

TIAN Chuan1,CAO Hui-ling2   

  1. (1. Xiamen Airlines,Xiamen 361006,China;2. College of Aeronautical Engineering,CAUC,Tianjin 300300,China)
  • Received:2012-07-04 Revised:2012-09-21 Online:2014-02-24 Published:2014-01-02

摘要:

应用分析方法分别对单轴涡喷发动机、涡轮风扇发动机以及采用中冷回热技术后的涡扇发动机进行了全面的分析。结果表明,单喷和涡扇发动机的尾流损是航空发动机整体损中的最大组成部分,而航空发动机的第二大损发生在燃烧室,对涡扇发动机引入中冷回热技术后,可以有效提高发动机的整体利用率,减少尾流中的损失。

关键词: 燃气涡轮发动机, 分析法, 中冷回热技术, 尾流损失

Abstract:

In order to find out the exergy loss of aero-engines,and to reveal the weakest chain of the exergy utilization,this article analyzes the exergy efficiency of single-spool turbo engine,turbofan engine and the intercooled and recuperated turbofan engine. The calculation results prove that the exergy loss during the wake equilibration process is the largest part of the exergy loss,which is more than one third of the overall exergy.The second largest part of the exergy loss is in the combustion chamber. When the intercooled and recuperated components are applied,the entire exergy efficiency can be better,what's more,the exergy loss during the wake equilibration process is significantly reduced. By analyzing the exergy efficiency of different types of aero-engines,this article will contribute to the design and improvement of the future aero-engines.

Key words: gas turbine engine, exergy efficiency, intercooled and recuperated aero-engine, wake loss

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