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Emissions of Volatile Particulate Components from Turboshaft Engines Operated with JP-8 and Fischer-Tropsch Fuels

机译:使用JP-8和费托燃料运行的涡轮轴发动机的挥发性微粒成分的排放

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Particulate emissions from two types of helicopter turboshaft engines operated with military JP-8 and paraffinic Fischer-Tropsch (FT) fuels were characterized as an objective of the field campaign held at the Hunter Army Airfield in Savannah, GA in June 2007. In general helicopter engines exhaust particles size distributions observed at the engine nozzle and 4.14 m downstream locations showing the geometric mean diameters smaller than 50 nm for all engine power settings investigated in this study. For both locations, the geometric mean diameter increased as the engine power setting increased; this trend also holds true for the emitted particle number concentration. The growth of particle geometric mean diameter was found significant, 7 nm, only in the case of the idle power setting.
机译:2007年6月在佐治亚州萨凡纳的Hunter Army Airfield举行的野外活动的目标是表征两种使用军用JP-8发动机和石蜡菲舍尔(FT)燃料的直升机涡轮轴发动机的微粒排放。在本研究中研究的所有发动机功率设置下,在发动机喷嘴和下游4.14 m处观察到的发动机排气颗粒尺寸分布均显示出小于50 nm的几何平均直径。对于两个位置,几何平均直径都随着发动机功率设置的增加而增加;对于发射的粒子数浓度,这种趋势也成立。仅在空载功率设置的情况下,发现粒子几何平均直径的增长显着,为7 nm。

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