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Statistical model for gas turbine engines exhaust emissions

机译:燃气涡轮发动机废气排放的统计模型

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A statistical analysis has been developed from the ICAO databank to predict aero-engines exhaust emissions during a landing and take-off cycle (LTO). The ICAO databank contains updated emission indices for a vast number of turbojet and turbofan engines only, with thrust ratings greater than 26.7 kN. Correlations are developed and proposed for turboprop and turboshaft engines to overcome the difficulty of assessing exhaust emissions from these engines in absence of industry data. LTO emissions are predicted for a turbofan-powered commuter airplane (Embraer E195) using the surrogate model. It is demonstrated that the predictions are closer to the values extracted from the flight data recorder than to the emissions calculated with the ICAO method. Thus, approximate emissions indices applied to actual flight procedures are a better choice than a standard ICAO LTO emission estimate from the databank. The correlations are then applied to the prediction of LTO emissions of a turboprop airplane (Bombardier Q400).
机译:国际民航组织数据库已经进行了统计分析,以预测飞机在着陆和起飞周期(LTO)期间的废气排放。 ICAO数据库仅包含推力额定值大于26.7 kN的大量涡轮喷气发动机和涡轮风扇发动机的更新排放指数。为涡轮螺旋桨和涡轮轴发动机开发并提出了相关性,以克服在缺乏行业数据的情况下评估这些发动机的废气排放的困难。使用替代模型预测了涡轮风扇动力通勤飞机(Embraer E195)的LTO排放。事实证明,与从国际民航组织方法计算出的排放量相比,预测更接近从飞行数据记录器提取的值。因此,与数据库中标准的ICAO LTO排放估算值相比,应用于实际飞行程序的近似排放指数是更好的选择。然后将相关性应用于涡轮螺旋桨飞机(Bombardier Q400)的LTO排放的预测。

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