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脉冲爆震涡轮发动机研究进展

郑龙席 卢杰 严传俊 邱华 王治武 黄希桥 李晓丰

郑龙席, 卢杰, 严传俊, 邱华, 王治武, 黄希桥, 李晓丰. 脉冲爆震涡轮发动机研究进展[J]. 航空动力学报, 2014, (5): 993-1000.
引用本文: 郑龙席, 卢杰, 严传俊, 邱华, 王治武, 黄希桥, 李晓丰. 脉冲爆震涡轮发动机研究进展[J]. 航空动力学报, 2014, (5): 993-1000.
ZHENG Long-xi, LU Jie, YAN Chuan-jun, QIU Hua, WANG Zhi-wu, HUANG Xi-qiao, LI Xiao-feng. Research progress on pulse detonation turbine engine[J]. Journal of Aerospace Power, 2014, (5): 993-1000.
Citation: ZHENG Long-xi, LU Jie, YAN Chuan-jun, QIU Hua, WANG Zhi-wu, HUANG Xi-qiao, LI Xiao-feng. Research progress on pulse detonation turbine engine[J]. Journal of Aerospace Power, 2014, (5): 993-1000.

脉冲爆震涡轮发动机研究进展

详细信息
    作者简介:

    郑龙席(1970- ),男,陕西西安人,教授、博士生导师,博士,研究领域为航空发动机燃烧与流动,新概念航空航天推进技术,航空发动机强度、振动与可靠性.

  • 中图分类号: V235

Research progress on pulse detonation turbine engine

  • 摘要: 介绍了脉冲爆震涡轮发动机的基本概念、主要结构形式以及基本特点.详细介绍了国内外研究状况及课题组的最新研究进展,对脉冲爆震涡轮发动机需要突破的关键技术、主要研究内容以及发展途径进行了探讨.研究表明:相比于传统的涡轮喷气发动机,脉冲爆震涡轮发动机的耗油率能降低5%~15%;在相同的燃烧室入口条件下,与等压燃烧驱动涡轮相比,用脉冲爆震燃烧驱动涡轮时的涡轮的单位输出功率要高;实现了由脉冲爆震燃烧室驱动涡轮,涡轮带动压气机给脉冲爆震燃烧室供气的自吸气模式,表明用脉冲爆震燃烧室代替传统等压燃烧室是完全可行的.

     

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  • 收稿日期:  2013-03-19
  • 刊出日期:  2014-05-28

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