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NOxemission indices of subsonic long-range jet aircraft at cruise altitude: In situ measurements and predictions

机译:邮轮高度喷气式飞机的Noxemission指标在巡航高度:原位测量和预测

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摘要

In the course of the Commissions of the European Communities project “Pollution From Aircraft Emissions in the North Atlantic Flight Corridor (POLINAT)”, in situ measurements of NO, NOx , and CO2 volume mixing ratios in the near-field exhaust plumes of seven subsonic long-range jet aircraft have been carried out by using the research aircraft Falcon of the Deutsche Forschungsanstalt für Luft- und Raumfahrt (DLR). For three additional aircraft, only NO and CO2 were measured. Plume ages of 50 s to 150 s have been covered, with maximum observed exhaust gas enhancements of 319 parts per billion by volume and 51 parts per million by volume for Δ[NOx] and Δ[CO2], respectively, in relation to ambient values. Aircraft cruising altitudes and Mach numbers ranged from 9.1 to 11.3 km and from 0.77 to 0.85, respectively. These measurements are used to derive NOx emission indices for seven of the individual aircraft/engine combinations. The NOx emission indices derived range from 12.3 g/kg to 30.4 g/kg. They are compared with predicted emission index values, calculated for the same aircraft engine and the actual conditions by using two newly developed fuel flow correlation methods. The calculated emission indices were mostly within or close to the error limits of the measured values. On average, the predictions from both methods were 12% lower than the measured values, with an observed maximum deviation of 25%. The ratio γ = [NO2]/[NOx] found during the present measurements ranged from 0.06 to 0.11 for five daytime cases and was around 0.22 for two nighttime cases. By use of a simple box model of the plume chemistry and dilution these data were used to estimate the initial value γ0 present at the engine exit plane. We found γ0 values between 0 and 0.15. These were applied to estimate the corresponding NO2 for the three cases in which only NO was measured.
机译:在欧洲共同体委员会的课程项目“污染来自北大西洋的飞行走廊(POLINAT)飞机排放”,在NO,NOx的现场测量,并在近场CO2体积混合比7亚音速的排气羽远程喷气飞机已经通过使用德意志Forschungsanstalt献给叶轮应力UND Raumfahrt(DLR)的研究飞机隼进行。有关其他三架飞机中,只有NO和CO2测量。的50〜150秒羽年龄已覆盖,最大分别观察到废气的增强的319份每十亿(体积)和每百万51份(体积)为Δ[NOx的]和Δ[CO2],...,相对于环境的值。飞机巡航分别介于9.1至11.3公里,0.77〜0.85的高度和马赫数。这些测量用于得出NOx排放指数对各个飞机/发动机组合中的七个。 NOx排放指数衍生范围12.3克/千克至3040克/千克。它们与预测的排放指标值,同样的飞机发动机计算,通过使用两个新开发的燃料流相关方法的实际情况进行比较。所计算出的排放指数大多内或接近测量值的误差极限。平均而言,这两种方法的预测分别为12%比的测量值降低,具有25%所观察的最大偏差。比γ= [NO 2]本测量期间/实测值[NOx的]从0.06至不等0.11五白天箱子和约为0.22两个夜间情况。通过使用羽化学和稀释的简单盒模型的这些数据被用来估计存在于发动机出口平面的初始值γ0。我们发现0和0.15之间γ0值。这些被用于估计对应NO2对于其中仅NO测量三种情况。

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