自行开发的图形组件在航空发动机设计集成系统中的应用

结合具体开发的图例,阐述了自行开发、应用于航空发动机设计集成系统的图形组件的功能、应用情况和关键技术。     

着陆姿态对地外天体表层采样的影响研究

表层采样技术是获得地外天体特性的重要手段,是完成地外天体采样任务的一项关键技术。文章结合4自由度表层采样装置的特点,建立了表层采样装置的逆运动学模型,分析了极限着陆姿态下表层采样装置安装位置在当地参考坐标系中的变化,并针对一次封装与二次封装过程中表层采样装置的位置和姿态要求,明确了末端采样器姿态补偿方法,提出了着陆姿态对表层采样影响的分析算法。仿真结果表明,该算法能有效分析着陆姿态对表层采样的影响,可为表层采样装置适应性设计提供支持。     

Effects of TADs on the F region of the mid-latitude ionosphere during an intense geomagnetic storm

Based on observations of two ionosondes at Wuhan and Kokubunji, this paper presents effects of TADs on the daytime mid-latitude ionosphere during the intense geomagnetic storm on March 31, 2001. During a positive ionospheric storm, the start of the enhancement of the foF2 (F2 peak plasma frequency) at Wuhan lags that at Kokubunji by 15 min, which corresponds to the time interval of traveling atmospheric disturbances (TADs’) propagation from Kokubunji to Wuhan. Associated with the uplifting of the hmF2 (height of F2 peak) caused by TADs, it is observed by the two ionosondes that the F1 cusp becomes better developed. Therefore, during a geomagnetic storm, TADs originating from the auroral oval may have a strong influence on the shape of the electron density profile in the F1 region ionosphere at middle latitudes. It is highly likely that TADs are responsible for the evolution of the F1 cusp.     

“阿波罗”登月舱的软着陆支架

登月舱的软着陆支架是确保月面探测活动及宇航员返回地球的关键装置。文章对“阿波罗”登月舱软着陆支架进行了介绍,描述了其技术指标、功能要求和基本组成,并对“阿波罗”登月舱软着陆支架的构型设计,主支柱、辅助支柱、足垫、展开架、收拢释放机构、展开锁定机构、触杆高度器以及铝蜂窝缓冲元件的设计方案进行了说明。鉴于“阿波罗”登月舱软着陆支架的设计通过了多次飞行试验的验证,文章结合“阿波罗”登月舱软着陆支架的方案,提出了中国载人登月工程中登月舱软着陆支架研制的建议。     

1Cr18Ni9Ti 对接管接头表面缺陷分析

对接管接头采用1Cr18Ni9Ti 棒材生产,经过机械加工后与相同牌号管材焊接,焊接后酸洗发现

零件表面存在缺陷。通过对失效件缺陷形貌观察、化学成分分析、金相分析及显微硬度测试,并结合酸洗试验。

结果表明:对接管接头材料内部存在沿变形流线的贫铬区,导致该区域的耐蚀性差,在机加工的过程中贫铬区

暴露在表面或近表面,在酸洗过程中该区域被优先腐蚀,形成了蚀孔类宏观缺陷,此贫铬现象为原材料缺陷。

     

PC控制在炼焦项目中的应用

以三菱AnS系列可编程控制器为例，在介绍其主要模块的性能参数基础上，从硬件和软件两方面，阐述了如何实现对拦焦机和装煤车的控制及其控制特点。     

A systematic approach to nonlinear rotorcraft model identification

The development of a powerful parameter estimation routine and its integration into the simulation environment HOST is described. With this tool approaches are being made towards new strategies of mathematical modeling, aimed at providing highly accurate and nevertheless run-time efficient simulation models. The identification routine is capable of optimizing parameterized models in both dynamic time domain simulation and static (e.g. trim state variation) conditions. Examples of both cases are presented to emphasize the improvement in the system response prediction and to demonstrate the abilities of the identification techniques in combination with the nonlinear simulation platform. This article reviews the activities and achievements accomplished by the DLR Institute of Flight Research and the ONERA Systems Control and Flight Dynamics Department during the last few years in the research on rotorcraft flight dynamics modeling and model identification. Future activities that require extensive high fidelity modeling are in the scope of the current and coming modeling activities that include the use of the presented methods and software technologies.     

Blazar nuclei in radio-loud narrow-line Seyfert 1?

It has been suggested that some radio-loud narrow-line Seyfert 1 contain relativistic jets, on the basis of their flat-spectrum radio nuclei and studies on variability. We present preliminary results of an ongoing investigation of the X-ray and multiwavelength properties of 5 radio-loud NLS1 based on archival data from Swift and XMM-Newton. Some sources present interesting characteristics, very uncharacteristic for a radio-quiet narrow-line Seyfert 1, such as very hard X-ray spectra, and correlated optical and ultraviolet variability. However, none of the studied sources show conclusive evidence for relativistic jets. γ-Ray observations with Fermi are strongly recommended to definitely decide on the presence or not of relativistic jets.     

Characterization of the cataloged Fengyun-1C fragments and their long-term effect on the LEO environment

The intentional breakup of Fengyun-1C on 11 January 2007 created the most severe orbital debris cloud in history. The altitude where the event occurred was probably the worst location for a major breakup in the low Earth orbit (LEO) region, since it was already highly populated with operational satellites and debris generated from previous breakups. The addition of so many fragments not only poses a realistic threat to operational satellites in the region, but also increases the instability (i.e., collision cascade effect) of the debris population there.