How far is far enough? Requirements derivation for planetary mobility systems

The origination of duration and distance requirements on planetary mobility systems (generally, rovers) are reviewed in detail. It is found that a ‘clean’ flow down from scientific objectives to requirement to capability is rarely presented. Rather, the historical record shows that the capability of emerging designs has been adopted post-hoc as a requirement, simple comparative superiority to predecessor missions has been invoked in competitive situations, or the requirement has been driven by capability of other elements of a mission architecture, such as delivery precision or astronaut life support. These deviations from the idealized systems engineering process have nonetheless resulted in missions that have generally been considered highly successful.     

Experimental study of an insert and its influence on churning losses in a high-speed electro-hydrostatic actuator pump of an aircraft

The speed of an Electro-Hydrostatic Actuator (EHA) pump can recently reach 20000 r/min, and its churning losses increase obviously with an increasing speed, which results in low efficiency and thus increasing heat in aircraft EHA systems. In order to reduce churning losses at high speeds, more attention should be given to the design of an insert. In this paper, the effect of an insert with different design parameters on churning losses is investigated through Computational Fluid Dynamics (CFD) simulation and experiments by calculating the difference between churning losses torques of the test pump with and without the insert based on a high-speed churning losses test rig. Analytical results show that the gap between the insert and the cylinder is critical for churning losses reduction. It is found that the churning losses of the test pump can be reduced with a decreasing gap between the cylinder block and the insert at high speeds. This is because the insert can decrease the turbulence occurrence at high speeds. The results can be used for flow field analysis and optimization of the high-speed EHA pump and provide a new method for improving efficiency of high-speed EHA pumps.     

变速恒频电源控制器的设计与实现

首先对变速恒频电源控制器（ＧＣＣＵ）的控制功能，保护功能，ＢＩＴ功能进行了详细分析，重点讨论了ＢＩＴ功能和ＧＣＣＵ的硬件设计方案。采用８０９７ＢＨ单片微型计算机，使硬件结构大大简化。文中还对电源系统的故障模式进行了较详细的分析，并阐述了ＧＣＣＵ软件设计的主要技术问题，提出了若干软件设计原则，给出了主要软件框图。所设计的ＧＣＣＵ在变速恒频电源系统中获得了满意的应用     

柔性转子逆回旋振动特性的研究

论述了具有陀螺效应的柔性转子在各向异性支承条件下回旋振动的特性，推导出了转子在正回旋激励作用下产生逆回旋振动的条件，提出转子振动存在逆回旋带的概念，并举例说明了转子在整个转速范围和振动频率范围内回旋振动的特点，作出了逆回旋带的曲线图。     

用解题法调试某型飞机斜板系统

某型飞机是国家重点工程项目之一 ,该机进气道自动调节系统采用计算机进行结算、调节与控制 ,增加了系统调节精度和可靠性。但在首批飞机的调试中 ,极难实现技术条件的要求 ,且无规律可循。对此 ,我们通过对斜板调节机理的研究实验 ,摸索出了斜板在大小πk 时调节曲线的对比规律 ,设置了调整计算方程 ,可靠地解决了这一难题。     

半自动担架车的运动仿真

在讨论半自动担架车工作原理的基础上，应用运动学原理将担架车整个运动过程进行了分析。应用矩阵理论对担架车任意位置的13个关键点进行运动求解和运动仿真。     

基于磁致伸缩传感器的液体密度测量的研究

简要介绍了利用磁致伸缩传感器测量液体密度的原理以及测量系统的组成和应用。利用脉冲回波法测量了声速从而算出液体密度。验证了扭转波在液体中传播速度与液体密度的关系。     

低速风洞试验段槽道对流场方向的影响

现代一些大型低速风洞出于测量上的考虑，往往在试验段侧壁开有供移测架移动的槽道。本文则以西南交通大学低速工业风洞为例，分析了这种槽道结构对试验段方向场的影响。试验结果表明，不同的槽道封闭状态对试验段流动的方向场，特别是β（偏航角）方向场有较明显影响，为此，本文最后提出了一种改进方案。     

某型飞机交流电源系统改造研究

某系列飞机采用了一台变频发电机，为满足该系列飞机改造的要求，研究了采用变速恒频技术将该机的单相变频交流电源改造为恒频三相交流电源的方案。本文介绍了新型交流电源系统的设计方案和主要设计参数，包括总体方案、发电机工作点选取、功率和电磁部件设计、控制器构成和系统的工作逻辑。采用本文方案研制的电源系统作为某型飞机改型验证机的主交流电源得到了实际应用，该电源系统工作稳定可靠，满足了加装电子设备的需求。     

大气行星波影响低频电波吸收变化的机制

本文根据冬季中低纬低电离层中、低频（ＬＦ）电波振幅扰动与高纬平流层中大气行昨波活动密切相关的观测事实，分析研究了可能引起低电离层对ＬＦ电波吸收变化诸因素的作用后，提出了一种能较好地解释观测现象的物理机制，大气行星波可通过两种方式改变大气离化率ｑ，因而引起低电离层中电子密度Ｎ扰动，进而改变由Ｎ大小决定的电离层电波吸收值，结果导致ＬＦ电波振幅发生相应变化。文中给出了描述这一物理计算公式和某些计算结果。