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Remote measurement of the plume shape of aircraft exhausts at airports by passive FTIR spectrometry

机译:通过被动FTIR光谱法测量机场飞机耗尽的羽流形状

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Information about the interaction between the exhaust plume of an aircraft jet engine and ambient air is required for the application of small-scale chemistry-transport models to investigate airport air quality. This interaction is not well understood. In order to study the interaction, spatial information about the plume is required. FTIR emission spectroscopy may be applied to analyze the aircraft exhausts. In order to characterize the plumes spatially, a scanning imaging FTIR system (SIGIS) has been improved. SIGIS is comprised of an interferometer (Bruker OPAG), an azimuth-elevation-scanning mirror, a data acquisition and control system with digital signal processors (DSP), an infrared camera and a personal computer. With this instrumentation it is possible to visualise the plume and to obtain information about the temperature distribution within the plume. Measurements are performed at low spectral resolution, because the dynamic environment of these measurements limits the measurement time to about 2 minutes. Measurements of the plume shapes of an APU and of main engines were performed.
机译:关于飞机喷气发动机和环境空气的排气羽流与环境空气之间的相互作用所需的信息是应用小型化学传输模型来调查机场空气质量。这种互动并不熟知。为了研究互动,需要有关羽流的空间信息。可以应用FTIR发射光谱来分析飞机排气。为了在空间上表征羽毛,已经提高了扫描成像FTIR系统(SIGI)。 Sigis包括干涉仪(Bruker Opag),方位角升降扫描镜,具有数字信号处理器(DSP)的数据采集和控制系统,红外相机和个人计算机。利用这种仪器,可以可视化羽流并获得有关羽流内温度分布的信息。测量以低频分辨率执行,因为这些测量的动态环境将测量时间限制为大约2分钟。进行APU和主发动机的羽流形状的测量。

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