Emission inventory evaluation using observations of regional atmospheric background stations of China

Any accurate simulation of regional air quality by numerical models entails accurate and up-to-date emissions data for that region.The INTEX-B2006 (I06),one of the newest emission inventories recently popularly used in China and East Asia,has been assessed using the Community Multiscale Air Quality model and observations from regional atmospheric background stations of China.Comparisons of the model results with the observations for the species SO2,NO 2,O 3 and CO from the three regional atmospheric background stations of Shangdianzi,Longfengshan and Linan show that the model can basically capture the temporal characteristics of observations such as the monthly,seasonal and diurnal variance trends.Compared to the other three species,the simulated CO values were grossly underestimated by about two-third or one-half of the observed values,related to the uncertainty in CO emissions.Compared to the other two stations,Shangdianzi had poorer simulations,especially for SO2 and CO,which partly resulted from the site location close to local emission sources from the Beijing area;and the regional inventory used was not capable of capturing the influencing factors of strong regional sources on stations.Generally,the fact that summer gave poor simulation,especially for SO2 and O 3,might partly relate to poor simulations of meteorological fields such as temperature and wind.  

带温控装置的机载外挂设备挂飞可靠性试验方法

目的 制定安装于带温控装置吊舱内的机载外挂电子设备挂飞可靠性试验剖面，并提出一种安装于带温控装置吊舱内的机载外挂电子设备挂飞可靠性试验方法。方法 结合机载外挂电子设备的典型任务剖面及其复杂多样的环境条件，以某机载侦察相机为例，给出带温控装置吊舱内的机载外挂电子设备可靠性鉴定试验中试验方案的选择依据，然后根据GJB 899A—2009中的温度应力、振动应力简化处理原则和典型任务剖面的持续时间及其占比，得到温度、振动应力条件，并合成挂飞可靠性试验剖面。结果 使用该方法对某机载侦察相机的温度、振动应力进行处理，得到了带温控装置的吊舱内的机载外挂电子设备挂飞可靠性试验剖面。结论 提出的带温控装置吊舱内的机载外挂电子设备挂飞可靠性试验剖面设计方法，为安装于带温控装置的吊舱内的机载外挂电子设备开展可靠性鉴定试验提供了指导。  

一种飞机发动机影响区设备的可靠性试验剖面设计方法

目的 准确制定飞机发动机影响区设备的可靠性试验剖面,提出一种可靠性试验剖面设计方法.方法 结合飞机发动机影响区设备的振动"宽带随机信号叠加窄带尖峰信号"的特点,采用工程截取等效法对实测振动数据分析归纳,得到振动试验谱.然后根据振动应力简化原则和飞机典型任务状态的持续时间及其占整个任务剖面的时间比例得到振动应力条件,并合成可靠性试验剖面.结果 使用此方法对某飞机发动机影响区设备的振动数据进行处理,得到飞机发动机影响区设备的可靠性试验剖面.结论 提出的工程截取等效法非常适合发动机影响区设备振动信号的分离和归纳;提出的可靠性试验剖面设计方法,为飞机发动机影响区设备的可靠性剖面设计工作提供了新思路,对飞机发动机影响区域设备的可靠性设计有重要意义.