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Modeling and performance analysis of the integrated power unit

  • Beihang University
  • Collaborative Innovation Center of Advanced Aero-Engine

科研成果: 期刊稿件会议文章同行评审

摘要

This paper describes an integrated power unit (IPU) supplying bleed air and shaft power for main engine starting, aircraft environment control, and in-flight emergency power demand. The zero-dimension steady-state numerical simulation model of the IPU is built for both the normal air breathing (NAB) mode and the stored energy (SE) mode. The design point of the IPU is set in the NAB mode and the off-design performance calculations are accomplished for both modes. The Altitude-Mach characteristic of the NAB mode and the altitude characteristic of the SE mode are discussed and the fundamental control laws of the SE mode are established to minimize stored air consumption. The overall efficiency of the IPU is illustrated in the paper for the two modes.

源语言英语
页(从-至)1547-1552
页数6
期刊Energy Procedia
158
DOI
出版状态已出版 - 2019
活动10th International Conference on Applied Energy, ICAE 2018 - Hong Kong, 中国
期限: 22 8月 201825 8月 2018

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