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    何小民

    • 教授
    • 招生学科专业:
      动力工程及工程热物理 -- 【招收博士、硕士研究生】 -- 能源与动力学院
      航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
      能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
    • 毕业院校:南京航空航天大学
    • 学历:南京航空航天大学
    • 学位:工学博士学位
    • 所在单位:能源与动力学院
    • 联系方式:hxm@nuaa.edu.cn
    • 电子邮箱:

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    Performance enhancement of a trapped-vortex combustor for gas turbine engines using a novel hybrid-atomizer

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    所属单位:能源与动力学院

    发表刊物:APPLIED ENERGY

    关键字:Trapped vortex combustor Combustion efficiency Ignition Lean blowout Atomizer

    摘要:A novel hybrid-atomizer, combining the spray characteristics of pressure-swirl, airblast and fan atomizers, was designed and adopted for cavity fueling in a trapped vortex combustor (TVC). Furthermore, comparison experiments were conducted under atmospheric pressure to investigate the combustion characteristics of the combustor fueled using the novel hybrid atomizer and a simplex pressure-swirl atomizer. The discrepancies were directly explored in terms of ignition, lean blowout (LBO) limit, and combustion efficiency. The results indicate that the novel hybrid atomizer achieves significant advantages in terms of the combustion characteristics when compared to the simplex pressure-swirl atomizer. The outer-cavity ignition FAR achieved by the novel hybrid atomizer is 50% lower than pressure-swirl atomizer at Mach 0.25 and 0.29, with an inlet temperature of 373 K. In addition, the LBO limits acquired by the novel hybrid atomizer are lower than those of the pressure-swirl atomizer within the full range of operating conditions. Furthermore, a higher combustion efficiency is achieved by the novel hybrid atomizer compared to the pressure-swirl atomizer under most operating regimes.

    ISSN号:0306-2619

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    发表时间:2018-04-15

    合写作者:Li, Mingyu,Zhao, Yuling,金义,Yao, Kanghong,Ge, Zhenghao

    通讯作者:何小民