斜撑离合器楔块线切割工艺优化及变质层分析

对目前国内PCE型斜撑离合器楔块制造工艺进行概述。为制造高质量的斜撑离合器楔块,提出了一种以慢走丝线切割为核心的楔块加工工艺,采用正交方法对线切割电参数进行了匹配实验,采用扫描电镜对线切割试样表面进行分析。实验结果表明,影响线切割表面粗糙度的因素顺序为脉宽、休止时间、伺服倍率、起始电压,线切割表面存在结构疏松、含Cu和Zn元素、厚度约为15~20μm的变质层。     

基于使用问题分析的航空保障设备发展研究

基于试验鉴定过程中保障设备问题分布,构建了保障设备10种常见问题分类,利用多型机使用鉴定数据,对我国航空保障设备存在的使用问题进行统计分析,对"三化"、功能/性能、转场运输等高发问题的主要表现进行梳理,对使用问题的深层次原因进行了剖析,并从顶层规划、标准规范、"三化"统型、保障模式和试验鉴定等层面提出了改进意见和建议。     

飞机弹射救生系统内弹道数值仿真研究

以往研究弹射筒,主要以单级弹射筒为对象,对多级套筒式弹射筒研究不足。在计算中,往往忽略了有效面积以及滑轨摩擦的因素,所建立的模型通用性差。在分析弹射机构的结构以及工作过程的基础上,建立了适用于套筒式弹射机构的内弹道模型,仿真并与实验值进行对比,误差在0.77%~1.91%之间,证明了模型的正确性,可以为弹射筒方案设计和验证提供理论依据。     

电动轻型飞机电推进系统选型与参数匹配

电动飞机为实现彻底的绿色航空提供了一条光明的技术途径,作为电动飞机动力和能量的来源,电推进系统的参数匹配对电动飞机环保、节能和高效起到关键作用。首先,本文对电动轻型飞机电推进系统进行了简要概述,并分析了其组成部分的特点。其次,结合目前电动轻型飞机电推进系统的特点,给出了电推进系统选型与参数匹配的设计过程。然后,根据电推进系统各组成部分的特点,提出了一套电推进系统选型与参数匹配的方法,包括螺旋桨的选型与参数匹配、电动机的选型与参数匹配、控制器的选型与参数匹配、电池组的选型与参数匹配,该方法可以为电推进系统的优化设计提供依据。最后,以RX1E电动轻型飞机为例对此方法进行了验证,匹配结果满足设计要求,说明了此方法的可行性。     

非对称广义特征值问题的拟-Eberlein算法及其并行化

非对称广义特征值问题的并行计算,目前在国内外研究得很少, Ｇ． Ｗ ． Ｓｔｅｗ ａｒｔ 和 Ｐ． Ｊ． Ｅｂｅｒｌｅｉｎ 曾分别研究非 Ｈｅｒｍ ｉｔｅ 矩阵标准特征值的并行拟 Ｊａｃｏｂｉ算法,１９８９ 年 Ｊ． Ｐ． Ｃｈａｒｌｉｅｒ 和 Ｐ． Ｖａｎ Ｄｏｏｒｅｎ 在 Ｇ． Ｗ ． Ｓｔｅｗ ａｒｔ 的工作基础上提出了求解非对称广义特征值问题的拟 Ｊａｃｏｂｉ算法（简称 Ｃ Ｖ 算法）与并行拟 Ｊａｃｏｂｉ算法。文中以 Ｊ． Ｐ． Ｃｈａｒｌｉｅｒ 等人的工作为基础,提出求解大型非对称广义特征值问题的拟 Ｅｂｅｒｌｅｉｎ 算法与并行拟 Ｅｂｅｒｌｅｉｎ 算法, Ｃｈａｌｌｅｎｇｅ Ｌ 并行系统上的数值试验表明,不仅并行效率很高,且敛速远优于 Ｃ Ｖ 算法     

弹道导弹预警系统目标运动建模和类型识别

针对弹道导弹预警系统的识别任务,建立了弹道导弹和飞机类目标的运动模型,通过分析弹道导弹和飞机目标间的运动特性差异,采用灰色关联分析方法建立了目标类型识别模型,给出了进行目标类型识别的具体步骤.具体的算例验证了基于灰色关联分析的目标类型识别模型应用于目标识别的可行性和有效性.     

平台驱动的机载产品线建设研究与实践

为了提高机载产品的“三化”水平,提升研发效率、保证产品质量和降低开发成本,在企业推行产品线建设十分必要。在深入研究产品型谱、产品平台、架构和共用构建模块等相关要素的基础上,设计了一种构建产品线的通用方法并进行了实践,为企业推行基于产品线组合规划的产品开发模式提供了一种思路。     

先进涡扇发动机空气系统与零件传热设计技术验证

本文简要介绍了中国燃气涡轮研究院在先进涡扇发动机空气系统与零件传热设计技术验证方面的研究情况,内容涉及发动机空气系统设计技术、零件热分析设计技术、涡轮叶片冷却设计技术及新型铸冷双层壳型高效涡轮冷却叶片设计中的关键技术。探讨了空气系统与零件传热设计技术中的设计计算方法、设计软件校核与改进、试验研究与参数测试、以及设计体系建设等问题,通过系统的模型、部件和发动机整机三个层次的试验验证,初步形成了空气系统与零件传热设计体系。     

Qualitative estimation of magnetic storm efficiency in producing relativistic electron flux in the Earth’s outer radiation belt using geomagnetic pulsations data

It is well known that during many but not all of the geomagnetic storms enhanced fluxes of high-energy electrons are observed in the outer radiation belt. Here we examine relativistic (>2 MeV) electron fluxes measured by GOES at the synchronous orbit and on-ground observations of two types of ULF pulsations during 30 magnetic storms occurred during 1996–2000. To characterize the effectiveness of the chosen magnetic storms in producing relativistic electron fluxes, following to (Reeves, G.D., McAdams, K.L., Friedel, R.H.W., O’Brien, T.R. Acceleration and loss of relativistic electrons during geomagnetic storms. Geophys. Res. Lett. 30, doi:10.1029/2002GL016513, 2003), we calculate a ratio of the maximum daily-averaged electron flux measured during the recovery phase, to the mean pre-storm electron flux. A storm is considered an effective one if its ratio exceeds 2. We compare behavior of Pi1 and Pc5 geomagnetic pulsations during effective and non-effective storms and find a tendency for a storm efficiency to be higher when the mid-latitude Pi1 pulsations are observed for a long time during the magnetic storm main phase. We note also that the prolonged powerful Pc5 pulsation activity during the recovery phase of a magnetic storm is the necessary condition for the storm effectiveness. To interpret the found dependences, we suggest that there are two prerequisites for generating relativistic electron populations during a storm: (1) the availability of seed electrons in the magnetosphere, and Pi1 emissions are indicators of the mid-energy electron interaction with the ionosphere and (2) acceleration of the seed electrons to MeV energies, and interaction of electrons with the MHD wave activity in the Pc5 range is one of the most probable mechanisms proposed in the literature for this purpose.     

Enhancement of solar wind low-energy energetic particles as precursor of geomagnetic disturbance in operational geomagnetic forecast

A study of the relationship between solar wind low-energy energetic particles using data from the Electron, Proton, and Alpha Monitor (EPAM) onboard the Advanced Compositional Explorer spacecraft (ACE) and geomagnetic activity using data from Canadian magnetic observatories in Canada’s polar cap, auroral zone, and subauroral zone was carried out for a period spanning 1997–2005. Full halo coronal mass ejections (CMEs) were used to gauge the initial particle enhancements and the subsequent geomagnetic activity. It was found that maximum geomagnetic activity is related to maximum particle enhancements in a non-linear fashion. Quadratic fit of the data results in expressions that can be easily used in an operational space weather setting to forecast geomagnetic disturbance quantitatively. A superposed epoch analysis shows increase in particle flux level starts hours before geomagnetic activity attains its peak, affirming the precursory nature of EPAM particles for the impending geomagnetic impact of CME. This can supplement the decision process in formulating geomagnetic warning after the launch of CME from the Sun but before the arrival of shock at Earth. The empirical relationships between solar wind low-energy energetic particles and geomagnetic activity revealed in this statistical study can be easily codified, and thus utilized in operational space weather forecast to appraise the geoeffectiveness of the CME and to provide a quantitative forecast for maximum geomagnetic activity in Canada’s polar cap, auroral zone, and subauroral zone after the occurrence of a CME.