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Comparison of remote sensing techniques for measurements of aircraft emissions indices at airports

机译:遥感技术对机场飞机排放索引测量的比较

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The emission indices of aircraft engine exhausts were measured at airports by non-intrusive optical measurements by FTIR emission spectrometry at the engine nozzle exit as well as by FTIR absorption spectrometry and DOAS (Differential Optical Absorption Spectrometry) behind the aircraft. Two measurement campaigns were performed to compare these different measurement methods. A kerosene-powered burner was operated in such a way that the different methods were applied for the exh aust gas investigations during the same time and at nearly the same exhaust gas volume. The burner was built with a nozzle exit diameter of 37 cm and a power of about 150 kW. Fresh air is pumped into the burner tube by a fan. Calibration gases of CO and NO (pure gases) were added in different amounts to vary the concentration of these gases in the exhaust. The sampling probe of the intrusive measurement system was installed in the centre of the exhaust stream near the exhaust exit for measurements of CO_2, CO, NO, NO_2, UHC, SO_2 and O_2. An APU (GTCP36-300) in a test bed was used in the same way. CO was mixed into the exhausts near the nozzle exit. The passive FTIR instrument was operated in the test bed using special noise and vibration isolation. The open-path instruments were installed at the chimney exit on the roof of the test bed building. The deviations between the different measurement methods were of the order of +-10 up to +-20 %.
机译:通过在发动机喷嘴出口的FTIR发射光谱和飞机后面的FTIR吸收光谱法和DOA(差分光学吸收光谱)在机场通过非侵入式光学测量来测量飞机发动机排气的排放索引。进行两项测量活动以比较这些不同的测量方法。以这样的方式运行煤油动力燃烧器,使得在同一时间和几乎相同的废气容积和几乎相同的废气容积中施加不同的方法。燃烧器采用37厘米的喷嘴出口直径,电源约为150千瓦。用风扇将新鲜空气泵入燃烧器管中。 CO和NO(纯气体)的校准气体以不同的量加入,以改变排气中这些气体的浓度。侵入式测量系统的采样探针安装在排气出口附近的排气流的中心,用于测量CO_2,CO,NO,NO_2,UHC,SO_2和O_2。以相同的方式使用测试床中的APU(GTCP36-300)。将CO混合到喷嘴出口附近的排气中。无源FTIR仪器使用特殊的噪音和振动隔离在试验台中操作。开放式仪器安装在试验台屋顶上的烟囱出口处。不同测量方法之间的偏差为+ -10级,高达+ -20%。

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