高层建筑火灾中防烟空气幕实验

高层建筑火灾中,烟气是影响人员疏散及造成人员伤亡的主要原因.文中从理论上分析与比较了目前世界各国在高层建筑中所采用的防排烟模式与防烟空气幕的优缺点,从理论上解释了防烟空气幕的合理性与可行性.根据防烟空气幕的理论计算确定空气幕流量、吹风口宽度和风口射流速度并进行实验.实验结果表明,当空气幕流量与烟气流量之比为0.6左右,空气幂射流厚度在25-45 mm且射流角度在25°-35°之间时,空气幕对烟气能起到很好的阻隔作用.由于空气幕的卷吸作用,防烟效果只能达到98%.实验结果验证了本文理论计算的正确性.     

临近空间飞行器信息一体化初步设计

临近空间信息一体化体系的建设,是完备和闭合天地信息一体化网络的重要课题。简单介绍临近空间飞行器作为构建信息网络载体的优势,并简述课题研究的必要性以及国内外在该领域的发展现状与趋势。重点介绍临近空间信息一体化的基本体系与构成设想,分析构建临近空间信息一体化网络所面临的技术挑战。     

太赫兹脉冲测量技术及其在计量领域的应用CSCD

本文对国内外太赫兹脉冲的产生和测量技术进行了综述,详细介绍了太赫兹脉冲产生与测量技术的原理和优缺点,以及太赫兹脉冲技术在宽带示波器、超快光电探测器、超快脉冲产生器等仪器设备计量中的应用。     

Collaborative Navigation in an Unfamiliar Environment with People Having Different Spatial Aptitudes

This study addressed the issue of collaborative navigation by examining the types of information communicated in the processes of direction giving and receiving between people who guided each other simultaneously to a destination over the cell phone in a novel environment. When paired with a partner whose sense of direction differed greatly from their own, people found the collaboration difficult and took a longer time to verbally direct the partner to the destination. Landmarks that people used in giving navigational instructions differed depending on sense of direction. People with a good sense of direction adjusted route directions to their partners' wayfinding ability. Results from a detailed qualitative analysis of participants' verbal protocols and implications for personalized navigation tools are discussed.     

雷达侦察系统近场相位校正方法的实现

对采用多基线相位干涉仪进行测向定位的雷达侦察系统,分析在近场条件下进行相位一致性校正时引入的波程差,提出了近场条件下的相位校正方法.该方法可有效地消除或减小环境因素对雷达侦察系统相位校正和测向误差的影响,从而提高测向和定位精度.     

ExoMars 2016火星探测计划进入、减速、着陆的验证任务分析

对欧洲航天局(ESA)火星探测的ExoMars 2016计划进行了概述,着重分析了进入、减速、着陆验证任务的关键环节,详细分析了进入、减速、着陆验证的任务组成、任务目标、任务规划以及相关关键技术等。结合我国火星探测目前的技术状态,需要针对进入、减速、着陆各关键技术进行合理的规划,并适时开展相关的试验验证。首先完成整个火星探测进入、减速、着陆平台的验证与研制,再进一步开展深入的火星探测科学任务研究。文章所述内容和分析可为我国下一步开展火星等深空探测任务提供参考。     

Neural network modeling of flight control system

Modeling of angle tracking systems in the presence of actuator non-linearity such as angle, position and rate limits is a very significant and difficult task in the design and implementation of aircraft, target-tracking, and missile guided systems. A new recurrent neural network with time-delayed inputs and output feedback is used for the modeling of angle tracking systems, with emphasis on the neural network architecture, principles and algorithms. The neural network controller with modeling units for angle tracking is designed by using TMS320C25 processors. For time and size requirements, limited precision technology and look-up table technology are used in the design of the hardware and software systems. Given a set of input commands, the network is trained to control the system within the constraints imposed by actuators. The results show that the proposed networks are able to model the angle tracking system through learning without separate consideration of the non-linearity of actuators     

中华世纪坛旋转圆坛工程

中华世纪坛作为世纪之交的纪念性建筑物受到国内外广泛关注,由于国内外已有与其造型相似的建筑,因而旋转便成为其新颖性的主要标志,是中华世纪坛主体建筑的核心部分,中华世纪坛旋转圆坛是一种巨型旋转结构,不能完全用传统的静态方法进行设计和制作,这样重载低速旋转的建筑物确系国内外首创,其设计、制作、安装、电气控制均具有较大难度. 　　中国航空工业第303研究所作为中华世纪坛旋转圆坛的总承包单位,承担机械传动及计算机系统的设计和机电联调.负责旋转圆坛总体技术的制定和施工技术指导,并对施工质量,施工进度进行监督和协调.负责旋转圆坛施工现场协调管理工作,为旋转圆坛施工现场指挥办公室负责单位.303研究所接受中华世纪坛旋转圆坛任务后,在航空工业总公司的领导下,专门成立了工程领导小组,组建了“零点工程”项目组.确定为303所1999年六个必保的任务之一,所长亲自挂帅.提出“精心组织,精心设计,精心施工,质量第一,力争十一,确保零点”的指导方针.并委托所科学技术委员会组织所内外专家对支撑及驱动、钢结构等方案、计算书、设计图纸、加工工艺等进行评审,负责技术把关.同时通过科学试验取得关键技术数据,并以航空精密机械的质量意识严把质量关,创造世纪精品.     

EXPERIMENTAL INVESTIGATION ON R134A AIRBORNE VAPOR-COMPRESSION REFRIGERATION SYSTEM

The airborne high power electrical equipments have been widely used in modern aircrafts, which conse- quently causes the dramatic increase of heating load up to dozens of kilowatts. Accordingly, vapor-compression re- frigeration system （VCRS） with lower engine bleed air and larger refrigeration capacity has been paid much atten- tion in recent years. Therefore, based on the analysis of the characteristics of VCRS, an experiment system of VCRS using R134a is set up to simulate operation performances. The influences of different parameters including evaporation pressure, condensing pressure, refrigerant mass flow rate and compressor rotation speed are also in- vestigated. The impacts of different parameters on the system performance are various. This work can help to es- tablish the specific control law under different work conditions.     

4H-SiC材料中刃型位错的仿真模拟研究

根据4H-SiC刃型位错的特点,在Castep软件中建立了6×6×1的刃型位错模型。基于第一性原理,利用Castep程序对刃型位错的相关性质进行了计算,并与完整晶格的模拟结果进行了对比。结果表明在引入刃型位错之后,4H-SiC材料的带隙变窄,在靠近导带底部态密度出现了一个新的峰值,这主要是由位错芯处的悬挂键在禁带中引入了一个缺陷能级所致。