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Remote sensing of temperature and concentration profiles of a gas jet by coupling infrared emission spectroscopy and LIDAR for characterization of aircraft engine exhaust

机译:通过红外发射光谱和激光雷达对飞机喷气发动机的温度和浓度分布进行遥感监测,以表征飞机发动机排气

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Temperature data play an important role in the combustion chamber since it determines both the efficiency and the rate of pollutants emission of engines. Air pollution problem concerns the emissions of gases such as CO, CO_2, NO, NO_2, SO_2 and also aerosols, soot and volatile organic compounds. Flame combustion occurs in hostile environments where temperature and concentration profiles are often not easy to measure. In this study, a temperature and CO_2 concentration profiles optical measurement method, suitable for combustion analysis, is discussed and presented. The proposed optical metrology method presents numerous advantages when compared to intrusive methods. The experimental setup comprises a passive radiative emission measurement method combined with an active laser-measurement method. The passive method is based on the use of gas emission spectroscopy. The experimental spectrometer device is coupled with an active method. The active method is used to investigate and correct complex flame profiles. This method similar to a LIDAR (Light Detection And Ranging) device is based on the measurement of Rayleigh scattering of a short laser pulse recorded using a high-speed streak camera. The whole experimental system of this new method is presented. Results obtained on a small-scale turbojet are shown and discussed in order to illustrate the potentials deliver by the sophisticated method. Both temperature and concentration profiles of the gas jet are presented and discussed.
机译:温度数据在燃烧室中起着重要的作用,因为它决定了发动机的效率和污染物排放的速度。空气污染问题涉及诸如CO,CO_2,NO,NO_2,SO_2等气体以及气溶胶,烟灰和挥发性有机化合物的排放。火焰燃烧发生在通常难以测量温度和浓度分布的恶劣环境中。在这项研究中,讨论并提出了适合燃烧分析的温度和CO_2浓度分布光学测量方法。与侵入式方法相比,所提出的光学计量方法具有许多优势。实验装置包括无源辐射发射测量方法和有源激光测量方法。被动方法基于气体发射光谱法的使用。实验光谱仪设备与主动方法耦合。主动方法用于研究和校正复杂的火焰轮廓。该方法类似于LIDAR(光检测和测距)设备,是基于使用高速条纹相机记录的短激光脉冲的瑞利散射的测量结果。介绍了该新方法的整个实验系统。展示并讨论了在小型涡轮喷气发动机上获得的结果,以说明复杂方法所产生的电势。介绍并讨论了气体射流的温度和浓度分布图。

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