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Ground verification experiment of plasma-assisted combustion in annular combustor fan-shaped test piece

机译:环形燃烧器扇形试件中等离子燃烧的地面验证实验

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摘要

A plasma-assisted combustion (PAC) test platform for annular combustor fan-shaped test piece was developed to validate the feasibility of using PAC actuation to enhance annular combustor performance. Comparing experiments between conventional combustion (CC) and PAC were conducted where combustion efficiency, flue gas emissions, and outlet temperature distribution were measured. The performance of present method under different combustor excessive air coefficients were also evaluated. Compared with the test results of CC of fuel-rich, approximate stoichiometric ratio and fuel-lean kerosene/air mixtures, when PAC actuation was exerted with applied voltage of 10.1 kV, combustion efficiencies increased by 1.32, 1.52, and 2.03%, respectively; CO emissions reduced 43, 103, and 48 ppm, respectively; outlet temperature distribution coefficients decreased by 23.06, 22.04, and 11.46%, respectively; NOx emission from fuel-rich mixture combustion reduced 20 ppm, whereas it increased 41 and 5 ppm, respectively, for approximate stoichiometric ratio and fuel-lean kerosene/air mixtures; radial temperature distribution coefficients decreased by 25.71 and 22.50%, respectively, for fuel-rich and approximate stoichiometric ratio mixtures; however, it increased by 3.24% for fuel-lean mixture. The results lead to potential directions for the future optimization of kerosene-fueled aero-engine when using plasma-assisted combustion devices to enhance annular combustor performance.
机译:开发了用于环形燃烧器扇形试件的等离子体辅助燃烧(PAC)测试平台,以验证使用PAC致动来增强环形燃烧器性能的可行性。在常规燃烧(CC)和PAC之间进行了比较实验,测量了燃烧效率,烟道气排放和出口温度分布。还评估了本方法在不同燃烧器过量空气系数下的性能。与富燃料CC,近似化学计量比和贫燃料煤油/空气混合物的CC测试结果相比,当施加10.1 kV电压施加PAC驱动时,燃烧效率分别提高了1.32、1.52和2.03%。一氧化碳排放量分别减少了43、103和48 ppm;出口温度分布系数分别降低了23.06%,22.04和11.46%;对于近似化学计量比和贫燃料的煤油/空气混合物,富含燃料的混合物燃烧产生的NOx排放降低了20 ppm,而分别增加了41和5 ppm。对于富燃料和近似化学计量比的混合物,径向温度分布系数分别降低了25.71%和22.50%。但是,对于贫油混合气,它增加了3.24%。当使用等离子辅助燃烧装置来增强环形燃烧器性能时,这些结果为未来优化煤油燃料航空发动机提供了可能的方向。

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  • 来源
    《Journal of propulsion and power》 |2017年第6期|1439-1447|共9页
  • 作者单位

    94655 Unit of Chinese People's Liberation Army, Wuhu, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;

    Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;

    Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China,Research Institute of Army Aviation, Beijing, China;

    Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;

    Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;

    Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;

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