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入口流量分配对超紧凑级间燃烧室性能的影响

彭瀚 黄玥 邢菲 刘晨 林志伟

彭瀚, 黄玥, 邢菲, 刘晨, 林志伟. 入口流量分配对超紧凑级间燃烧室性能的影响[J]. 航空动力学报, 2017, 32(1): 60-65. doi: 10.13224/j.cnki.jasp.2017.01.009
引用本文: 彭瀚, 黄玥, 邢菲, 刘晨, 林志伟. 入口流量分配对超紧凑级间燃烧室性能的影响[J]. 航空动力学报, 2017, 32(1): 60-65. doi: 10.13224/j.cnki.jasp.2017.01.009
Performance of ultracompact interturbine burner with different inlet mass flow splits[J]. Journal of Aerospace Power, 2017, 32(1): 60-65. doi: 10.13224/j.cnki.jasp.2017.01.009
Citation: Performance of ultracompact interturbine burner with different inlet mass flow splits[J]. Journal of Aerospace Power, 2017, 32(1): 60-65. doi: 10.13224/j.cnki.jasp.2017.01.009

入口流量分配对超紧凑级间燃烧室性能的影响

doi: 10.13224/j.cnki.jasp.2017.01.009
基金项目: 国家自然科学基金(51406171); 福建省自然科学基金(2015J05111); 中央高校基本科研业务费项目(20720150094)

Performance of ultracompact interturbine burner with different inlet mass flow splits

  • 摘要: 对超紧凑级间燃烧室入口的流量分配进行了优化分析.首先基于化学反应模拟软件Chemkin,建立了航空煤油RP3/空气的小型级间燃烧室性能简化分析方法,并利用现有实验数据对其进行了验证.选取了入口主流流量/腔体流量分别为60/40,65/35,70/30,75/25,80/20五种分配方案,利用简化分析模型对各分流方案进行了对比研究,主要关注出口温度、燃烧效率和污染物排放的变化情况.结果表明:分流比为65/35时,燃烧效率相对于5种分流比中最高燃烧效率只下降0.249%,但NOx及CO排放均相对降低了50%以上.基于此研究方法得到的结论,可为超紧凑级间燃烧室设计初期的分流方案选取提供依据和性能简化分析方法.

     

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出版历程
  • 收稿日期:  2016-03-29
  • 刊出日期:  2017-01-28

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