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Preliminary exergy analysis of intercooled recuperated turbofan engine

  • Northwestern Polytechnical University Xian
  • China Aviation Industry Corporation

科研成果: 期刊稿件文章同行评审

摘要

By introducing the exergy destruction calculation method of the engine components, the intercooled recuperated turbofan engine calculation model and the simulation program were further developed. The component exergy destruction was calculated for the conventional turbofan engine and the intercooled recuperated turbofan engine, and comparison between each other was conducted. Preliminary exergy analysis of intercooled recuperated turbofan engine was carried out. The results indicate that, although intercooling and recuperation cause new loss, it can significantly reduce the losses of the high pressure turbine and the engine core exhaust stream, and improve the engine exergy efficiency.

源语言英语
页(从-至)975-979
页数5
期刊Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
36
5
出版状态已出版 - 1 5月 2015

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