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101.
《中国航空学报》2020,33(2):550-560
Experimental investigations on NOx emissions of a single-cup, Lean Premixed Prevaporized (LPP), module combustor were carried out at elevated inlet temperature and pressure up to 810 K and 2.0 MPa, close to the real operating conditions of aero-engine combustors. This LPP combustor adopts centrally staged fuel injections which could produce separated stratified swirling spray flame. In the NOx emissions measurements, the ranges of dome equivalence ratio and fuel stage ratio were from 0.55 to 0.58 and 8% to 24%, respectively. The optical diagnosis on separated stratified swirling spray flame were carried out with fuel stage ratio changing from 15% to 30%. Therefore, NO* and OH* chemiluminescence images were obtained. The results show that NOx emissions increase with the increase of the fuel stage ratio. And from the chemiluminescence images, the main flame and pilot flame are found weakly coupled. The pilot flame plays a significant role in NOx emission production because of its higher adiabatic flame temperature. Based on the results of chemiluminescence optical tests, a new NOx emission prediction model is proposed based on the Lefebvre’s single flame model. The estimate of local equivalence ratio of the pilot stage’s non-premixed flame is modified considering the characteristics of spray combustion, and a “PLUS” emission prediction model suitable for separated stratified swirling spray flame is obtained. Compared to the experimental data, the “PLUS” model exhibits a good prediction in a range of ±13% of deviation. 相似文献
102.
Eugene M. Trunkovsky 《Space Science Reviews》1995,74(3-4):485-488
Photoelectric WBVR observations of Be star HDE 245770=V 725 Tau, the optical counterpart of the transient X-ray pulsar A0535+26, having a pulse period of about 104 s, were conducted for more than 10 years. An irregular long-term optical variability of the star with amplitudes of the order of a few tenths of magnitude was found to be a usual phenomenon. In some cases rapid changes of the star's optical luminosity with a characteristic period of a few tens of minutes or a few hours, and an amplitude of several hundredths of magnitude in all the spectral bands used, which have practically coincided or correlated with the X-ray pulsar outbursts detected by X-ray satellites, were observed.Photoelectric recording of the optical flux from HDE 245770 were made in 1981–1982 with a time resolution of 1 second and 10 s, respectively, in theR spectral band (0 7000 Å) and in the narrowH
-emission-line band (1/2 75 Å) using a 48-cm reflector of High-Mountain Tien-Shan observatory of the Sternberg Astronomical Institute near Alma-Ata. An analysis of autocorrelation functions of the flux changes from object under study and a comparison with the star BD+26° 876 indicated the variability of luminosity of V 725 Tau in theR spectral band on a time scale of a few tens of second; this variability resembles shot noise with a characteristic time of stochastic bursts of about 15–20 s and their amplitudes of about a few tenths of a percent. InH
-emission-line radiation autocorrelation functions and power spectra show quasiperiodic variability of luminosity of HDE 245770 with a characteristic period of about 100–150 s and an amplitude in the neighbour-hood of 0.5%. The latter result is not quite reliable because of not quite fine weather conditions during the observations; independent observations and check-up are required. 相似文献
103.
航空航天复合材料结构健康监测技术研究进展 总被引:1,自引:0,他引:1
通过在线监测结构响应,实时掌握结构的健康状况,并在此基础上对可能发生的损伤和故障进行预报,以便能及时采取措施,保证复合材料结构的服役安全.综述了几种重要的结构健康监测方法的研究进展、应用场合与发展历程,包括:全局状态感知技术(光纤传感监测法)、全局损伤诊断技术(波传播损伤诊断法)、局部损伤诊断方法(机电阻抗监测法、真空比较监测法、智能涂层法等),讨论了复合材料结构健康监测传感器的安装方法.结合各种技术的发展历程和优缺点展望了航空航天复合材料结构健康监测技术的发展趋势. 相似文献
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106.
随着光学遥感器的不断发展,对光学遥感器的性能要求也不断提高。遥感器系统偏振特性也逐渐为人们所重视。特别是对辐射灵敏度要求较高的光学遥感器。文章首先分析了光学遥感器偏振特性的表述及与遥感器系统辐射灵敏度的关系。讨论了系统偏振影响的因素和系统偏振补偿设计的几种考虑。最后提出了遥感器系统偏振灵敏度测试方法和应用实例。 相似文献
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108.
高截止度新型红外滤光片是三轴稳定卫星红外地球敏感器的关键件之一。文章介绍了用等效折射率概念设计这种滤光片的方法 ,讨论并给出了膜系设计和研制的结果 ,简介了镀膜的工艺技术 ,并与国内外同类滤光片的光学特性进行了比较 ,试验表明新型红外滤光片的膜系设计是成功的。 相似文献
109.
介绍了“资源一号”卫星红外多光谱扫描仪辐射定标设备的光学系统;介绍了用空间光线追迹法,求离轴抛物面光学系统弥散圆的方法。 相似文献
110.