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氢燃料先进旋涡燃烧室流动和燃烧特性

邓洋波 孙海涛 王玉龙 严春吉

邓洋波, 孙海涛, 王玉龙, 严春吉. 氢燃料先进旋涡燃烧室流动和燃烧特性[J]. 航空动力学报, 2013, 28(1): 120-128.
引用本文: 邓洋波, 孙海涛, 王玉龙, 严春吉. 氢燃料先进旋涡燃烧室流动和燃烧特性[J]. 航空动力学报, 2013, 28(1): 120-128.
DENG Yang-bo, SUN Hai-tao, WANG Yu-long, YAN Chun-ji. Flow and combustion characteristics of advanced vortex combustor with hydrogen fuel[J]. Journal of Aerospace Power, 2013, 28(1): 120-128.
Citation: DENG Yang-bo, SUN Hai-tao, WANG Yu-long, YAN Chun-ji. Flow and combustion characteristics of advanced vortex combustor with hydrogen fuel[J]. Journal of Aerospace Power, 2013, 28(1): 120-128.

氢燃料先进旋涡燃烧室流动和燃烧特性

基金项目: 国家自然科学基金(51076020)

Flow and combustion characteristics of advanced vortex combustor with hydrogen fuel

  • 摘要: 为了对整体煤气化联合循环(IGCC)燃气轮机的氢燃料先进旋涡燃烧室(advanced vortex combustor,AVC)结构设计提供理论依据,应用实验和数值模拟相结合的方法对AVC气流流动特性受燃烧室几何参数影响规律进行研究,在此基础上,确定氢燃料AVC内前、后钝体合理的布置方式.应用19步氢气和空气详细化学反应机制,对氢燃料AVC流动和燃烧特性进行数值模拟研究,结果显示:氢气和空气预混和气体主气流当量比为0.65时,在前、后钝体之间形成的凹腔内无喷射气流条件下,燃氢AVC能够形成稳定燃烧,出口温度被控制在1950K以下,总压损失系数为2.7665%,燃烧效率为99.54%.相对于凹腔内无喷射气流,凹腔内有喷射气流的AVC旋涡在z轴方向分层有序、结构更加稳定,但不同xy截面上温度分布不同,导致出口截面温度分布不均匀,总压损失系数略有增大,燃烧效率提高了.

     

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  • 收稿日期:  2012-02-23
  • 刊出日期:  2013-01-28

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