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脉冲爆震燃气膨胀过程及能量转换难易度评价方法

李晓丰 肖俊峰 胡孟起 王玮 王峰

李晓丰, 肖俊峰, 胡孟起, 王玮, 王峰. 脉冲爆震燃气膨胀过程及能量转换难易度评价方法[J]. 航空动力学报, 2021, 36(8): 1586-1593. doi: 10.13224/j.cnki.jasp.20200474
引用本文: 李晓丰, 肖俊峰, 胡孟起, 王玮, 王峰. 脉冲爆震燃气膨胀过程及能量转换难易度评价方法[J]. 航空动力学报, 2021, 36(8): 1586-1593. doi: 10.13224/j.cnki.jasp.20200474
LI Xiaofeng, XIAO Junfeng, HU Mengqi, WANG Wei, WANG Feng. Pulse detonation gas expansion process and evaluation method of energy conversion difficulty degree[J]. Journal of Aerospace Power, 2021, 36(8): 1586-1593. doi: 10.13224/j.cnki.jasp.20200474
Citation: LI Xiaofeng, XIAO Junfeng, HU Mengqi, WANG Wei, WANG Feng. Pulse detonation gas expansion process and evaluation method of energy conversion difficulty degree[J]. Journal of Aerospace Power, 2021, 36(8): 1586-1593. doi: 10.13224/j.cnki.jasp.20200474

脉冲爆震燃气膨胀过程及能量转换难易度评价方法

doi: 10.13224/j.cnki.jasp.20200474
基金项目: 

陕西省自然科学基金(2020JQ-996)

详细信息
    作者简介:

    李晓丰(1985-),男,高级工程师,博士,主要从事燃气轮机燃烧技术研究。

  • 中图分类号: V231.2

Pulse detonation gas expansion process and evaluation method of energy conversion difficulty degree

  • 摘要: 为了提高脉冲爆震燃气的能量转换效率,分析了脉冲爆震燃气在涡轮内的膨胀过程,建立了评价爆震燃气能量转换难易度计算方法,并基于脉冲爆震燃烧室与轴流涡轮匹配工作数值模型,采用涡轮效率对燃气能量转换难易度计算方法进行了验证,结果表明: ①爆震波膨胀过程,爆震燃气在涡轮静叶内会产生热壅塞现象,并往上游形成前传压缩波; ②涡轮内爆震燃气的膨胀主要分一次膨胀、过度膨胀和二次膨胀三个阶段,爆震燃气在涡轮内的焓降主要发生在一次膨胀和二次膨胀阶段,在过度膨胀阶段,燃气在涡轮内做负功; ③当量比为0.72、0.89和1.00三种计算工况的燃气能量转换难易度分别为0.396、1.000和0.803,对应的涡轮效率分别为0.473 6、0.597 2和0.570 3,验证了燃气能量转换难易度计算方法的准确性。

     

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出版历程
  • 收稿日期:  2020-11-06
  • 刊出日期:  2021-08-28

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