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Combustion of JP-10-Based Slurry with Nanosized Aluminum Additives

机译:JP-10-基浆料与纳米铝添加剂的燃烧

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Nanosized aluminum (16% by weight) was added into JP-10 and surfactant (2% by weight) was used to reduce the agglomeration of nanoparticles. Combustion of metalized fuel, as well as pure JP-10, was carried out in a small-scale combustor. The oxygen-to-fuel ratios were set to be 1.7,1.8, and 1.9, respectively. An additional trial of water injection during combustion was also tested. The pressures at the combustion chamber and nozzle exit, along with the thrust, were measured during the combustion; and intervals of true values of the specific impulse were presented. The results showed that a relatively higher combustion efficiency was achieved with JP-10-based slurry by 3.0 to 9.0% when compared to pure JP-10. However, the specific impulse could be increased only when the combustion-induced heat release was improved enough to overcome the two-phase loss. Depositions at different positions were collected after combustion for deep analysis; and the results of the x-ray diffraction, thermogravimetry analysis, scanning electron microscope, and laser light scattering were presented. A relatively high oxidation rate of the aluminum was obtained in tests without water injection, and the solid particles were mainly spherical and in dimensions of 100-300 nm. In the tests with water injection, stable combustion and increased thrust were achieved; whereas the combustion efficiency and specific impulse were deceased. And, the size of the particles was increased due to the addition of water.
机译:将纳米尺寸的铝(16%重量)添加到JP-10中,并使用表面活性剂(2%重量)减少纳米颗粒的团聚。金属化燃料以及纯JP-10的燃烧均在小型燃烧器中进行。氧/燃料比分别设置为1.7、1.8和1.9。还测试了燃烧过程中注水的其他试验。在燃烧过程中测量燃烧室和喷嘴出口处的压力以及推力。并给出了特定脉冲真实值的间隔。结果表明,与纯JP-10相比,基于JP-10-的浆液可实现3.0至9.0%的相对较高的燃烧效率。但是,只有当燃烧引起的热量释放得到足够改善以克服两相损失时,才能增加比脉冲。燃烧后收集不同位置的沉积物进行深入分析;并给出了X射线衍射,热重分析,扫描电子显微镜和激光散射的结果。在不注水的测试中获得了较高的铝氧化速率,固体颗粒主要为球形,尺寸为100-300 nm。在注水试验中,燃烧稳定,推力增加。而燃烧效率和比冲降低。并且,由于添加水,颗粒的尺寸增加。

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  • 来源
    《Journal of propulsion and power》 |2016年第5期|1167-1177|共11页
  • 作者单位

    Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China;

    Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China;

    Tianjin University, 300072 Tianjin, People's Republic of China;

    Tianjin University, 300072 Tianjin, People's Republic of China;

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