基于Pro/Engineer的直齿圆锥齿轮三维实体造型

介绍在Pro／Engineer环境下实现直齿圆锥齿轮精确造型的方法。在此基础上,利用Pro／Engineer的Program模块完成二次开发。设计人员只需输入直齿圆锥齿轮的已知设计参数,就可迅速准确地生成所需的三维实体模型。     

空间光学遥感器光-机-热集成分析方法研究

首先对论文的工程背景空间太阳望远镜进行了介绍;然后介绍了空间光学遥感器光 机 热集成分析的技术路径和技术实现,技术实现主要探讨如何将透镜的折射率温度系数效应和反射镜面的热变形效应数据变成光学分析软件可以接受的数据;最后以光 机 热集成分析为基础,对空间太阳望远镜主镜的热设计方案进行了论证。全文说明了光 机 热集成分析的可实现性以及其对热设计的指导、评价和优化。     

Stability and shape analysis of relative equilibrium for three-spacecraft electromagnetic formation

The invariant shapes for close formation flying with inter-craft electromagnetic force ensure several potential space applications. However, the 6-DOF relative equilibrium problem has not been systematically investigated. This paper mainly analyzes the invariant shapes of relative equilibrium for the three-spacecraft electromagnetic formation, and studies the families of invariant shape solutions with real and constant magnetic moments as well as their linear stability. The problem is examined based on the full nonlinear coupled dynamic models for collinear and general triangular configurations. The relative equilibrium conditions are analyzed to determine whether an invariant shape do exist, and the corresponding families of invariant shape solutions are identified for static and spinning configurations respectively. Finally, the linear stability of such invariant shapes is numerically discussed, which have shown that most invariant shapes are unstable and controllable.     

Characteristics of the seasonal variation of the global tropopause revealed by COSMIC/GPS data

Using the Global Navigation Satellite System (GNSS) radio occultation observations from Formosa Satellite mission-3/Constellation Observing System for Meteorology, Ionosphere, and Climate (FORMOSAT-3/COSMIC) from 2007 to 2012, the climatological characteristics of the global tropopause was studied, with the following features identified. The overall results generally agree with previous studies. The tropopause has an obvious zonal structure, with more zonal characteristics in the Southern Hemisphere than the Northern Hemisphere. The vertical shape of the tropopause is sharp in the tropics and broad in the sub-tropical latitudes, with the sharpest latitudinal gradient in the mid-latitudes of both hemispheres. The global tropopause exists in a large range between 8 km and 17 km (or between 100 hPa and 340 hPa). The highest tropopause is over the South Asian monsoon regions for the entire year. The spatial structure of the tropopause in the polar region is of concentric structure, with an altitude between 7.5 km and 10 km. It is more symmetric in the Antarctic than the Arctic. Differing from other places, the height of the tropopause in the Antarctic is higher in winter as opposed to summer. The tropopause has distinct seasonal variability, especially in polar regions.     

超高/超声速轴向运动梁的模态频率特性

研究了高速轴向运动梁的横向振动特性.首先采用Hamilton原理得到了两端自由轴向运动梁的振动方程和边界条件.再运用伽辽金法得到了求解系统响应的近似方程.最后研究了对梁的振动频率影响较大的3个方面:(1)轴向速度,第一阶固有频率随轴向速度增加而减小,存在一个失稳的临界速度;(2)质量亏损,梁的某部分质量亏损可以增加固有频率;(3)热效应,温度上升会减小梁的弹性模量,使得固有频率减小.     

基于灰色多层次模糊理论的 L/HIRF 维修间隔确定

随着先进复合材料在民机上大量使用及飞机电磁环境日趋复杂,雷击高能辐射场(Lighing and mighIntensiy Radiation Field--LMHIRF)防护部件维修间隔的合理确定,已成为制定民机维修大纲的关键内容之一。以国产民机L/HIRF防护部件维修间隔为研究背景,综合考虑偶然损伤、环境损伤,可见性3种主要影响因素,将灰色模型、模糊逻辑与多层次分析理论相结合,建立 LMIRF 防护部件维修间隔确定的分析模型,并通过选取相似机型的典型结构进行实例验证。分析结果表明,模型计算结果与维修大纲给出的参考间隔趋于一致符合工程实际。在一定程度上,解决国产民机 LHIRF 防护部件维修间隔制定过程中,由于缺少工程经验而导致维修间隔的确定偏主观的问题。     

Resol型酚醛树脂热解特征的TG-MS 研究

合成了一种低醛 /酚摩尔比 (1.3∶1)的Resol型酚醛预聚物。利用TG -MS详细研究了热交联固化后树脂的热分解特征。低于 35 0℃时 ,主要表现为分子内醚键断裂和脱端羟甲基 ,并逸出H2 O、CO2 和CH3 OH等产物及它们的碎片。在 35 0℃～ 75 0℃范围内 ,大分子主链在不同位置发生主链断裂而形成一甲基苯酚、二甲基苯酚和三甲基苯酚等产物及它们的碎片。说明了大分子主链热稳定性的提高是减少和防止Resol型酚醛树脂前驱体C/C复合材料缺陷的重要组成部分     

液氧/煤油发动机试验系统

设计并建立了液氧／煤油发动机发生器-涡轮泵联动装置和整机试验系统。详细介绍了推进剂供应系统、煤油回流系统、试验工艺辅助系统、控制系统的组成及试验能力,重点论述了关键试验工艺技术,主要包括启动技术、增压技术、试车工艺、安全措施。     

基于双相关峰检测的C/A码伪距精密估计

采用软件无线电技术和数字信号处理技术，直接对A／D变换后的中频信号进行处理，并得到C／A码的相关曲线。利用曲线拟合方法对相关峰波形进行拟合，进一步确定相关曲线的峰值点位置。同时基于双相关峰检测的伪距估计方法，精确求解C／A码伪距观测值。利用自编的仿真程序包，在Matlab中进行了相应的模拟计算。仿真结果表明当信噪比大于26dB时，可得到毫米数量级的伪距估计精度，能够满足GPS模拟源系统高精度自校的要求。     

全复合材料发动机壳体与喷管连接结构

结合国外先进固体发动机纤维缠绕壳体与喷管连接的技术,分析了实现全复合材料固体发动机壳体-喷管的连接方式,技术途径,并提出了有关设计参数,可供设计人员参考.