微机控制变螺距螺纹的追踪修正法

本文探讨用经济型数控系统加工变螺距螺纹的原理,提出了一种插补算法——追踪修正法。通过仿真计算,考核了这种算法的理论误差。结果表明,其控制精度是令人满意的.     

Book reviews

America's Secret Power: the CIA in a Democratic Society. By Loch K. Johnson. Oxford University Press, New York (1989), ISBN 0–19–505490–3, $24.95

The Bundeswehr and Western Security. Edited by Stephen F. Szabo. Houndmills, Basingstoke, and Macmillan, London (1990), ISBN 0–333–49880–1, £45.00

Symbolic Defense: the Cultural Significance of the Strategic Defense Initiative. By Edward Tabor Linenthal. University of Illinois Press, Chicago, IL (1989), ISBN 0–252–01619‐X, $19.95

Rethinking European Security. Edited by Furio Cerutti and Rodolfo Ragionieri. Crane Russak, New York (1990), £29.00

Alternative Conventional Defense Postures in the European Theater, Vol. 1: The Military Balance and Domestic Constraints. Edited by Hans Günter Brauch and Robert Kennedy, Crane Russak, New York (1990), £32.00

The Gulf War. Edited by Hanns Maull and Otto Pick. Pinter, London (1989), ISBN 0–86187–763–2, £36.00     

五位量子纠错码的各种形式

在各种量子纠错方案中五位量子纠错码被讨论得最多,本文按照正交条件,用图表对各种错误形式进行分类,再利用图表的直观性和对称性提供了一个较方便地找出５位量子纠错码各种形式的方法。     

网络安全脆弱性分析与处置系统的研究与实现

在分析国内外研究现状的基础上,针对现有的漏洞库系统在漏洞信息的组织、使用等方面存在的不足,采用分布计算技术、数据库技术、Web技术实现了网络安全脆弱性分析与处置系统。该系统实现了基于Web的漏洞库(含补丁库)的访问与维护工具,便于获取相应漏洞的解决方案和下载相应的补丁程序,降低了系统维护的开销,提高了系统的可维护性;补丁推送程序实现了对系统补丁程序的远程推送、漏洞修补和补漏检测,提高了系统的自动化程度,为网络安全脆弱性处置提供了有力工具。     

一种武器装备通用防护油的研制

介绍了武器装备通用防护油的研制过程、配方、性能及应用情况。实验室理化性能评定和实际使用结果表明,该油具有功能多、性能好、通用性强和使用方便等特点,综合性能达到了国际同类产品的先进水平,可广泛应用于军事装备和民用机械设备的擦拭保养和防护。     

传统的方位定义应用局限性研究

本文分析了传统的方位定义与计算存在的应用局限性根源,提出了适合航海及各种规模军事演练需求的改进的方位定义和计算方法,并分析了两种方位定义下的方位计算误差及适用条件.     

新型扫雷装药爆炸场特性分析及应用

基于爆破法扫雷爆破筒扫雷作用原理,设计了8.2 kg一次引爆型固态FAE扫雷装置。通过改变起爆位置和设置方式,多次野外近地面爆炸试验,采用反射压力传感器在装药正向与侧向离爆点不同位置进行压力测试,同时在正向测线压力传感器的对应位置设置某型防步兵地雷,得到爆炸场不同位置处的爆炸参数以及防步兵雷扫雷范围。结果表明:水平设置扫雷装药的扫雷范围明显大于垂直设置的装药,最佳炸高约为0.60 m;且其爆炸场正压区作用时间曲线呈“V”形,产物作用范围达63倍装药半径,与等当量的TNT的作用时间有明显的优势;本装置的扫雷范围约为目前扫雷爆破筒爆破扫雷范围的1.8～3.85倍,正向可靠扫雷范围可达其装药半径的77倍,侧向达69倍。由于该装药爆炸作用区域正压作用时间明显加长,因此有利于各种地雷的清除,是一种潜在高效的爆破法扫雷装药。     

通气空泡与超音速尾喷流耦合作用实验研究

基于开放式水洞,构建了通气空泡与超音速尾喷流耦合作用实验系统。设计了四种可变长度实验模型,重点研究射流与通气空泡相对位置对空泡射流耦合作用机理的影响。针对不同外形实验模型,改变通气流量和射流流量,获得了不同工况下空泡界面瞬态演化规律。通过实验,观察到射流完全补气、射流部分泄气、射流完全泄气三种不同耦合作用模式。进一步结合实验数据和Paryshev理论分析,建立了不同模式下临界转变条件和空泡尺度计算模型。当≤0.1 时,空泡长度可用经典空泡经验公式来描述;当0.1<<1.5 时,空泡长度分为模型长度和尾部空泡长度两部分,而尾部空泡长度只与无量纲动量比有关;当 ≥1.5时,空泡闭合在喷管出口,空泡长度与模型长度相等。     

美国太空安全领域最新发展分析

美国认为太空已被普遍认定为最重要的作战域之一,未来的太空安全态势将愈发严峻。本文认为, 美国正面向未来太空对抗环境进行全面转型, 从顶层战略、作战理论、组织结构、战备训练、装备技术等方面开展研究、调整和长远布局, 如以我为主要对手谋划布局、发布系列军事航天顶层指导文件、大幅增加太空攻防作战相关经费投入等。 目前, 美军正处于新旧体系转换、 下一代能力构建发展的关键期, 不仅正在变革军队组织体制、重组太空攻防作战力量, 还积极开展系列演习演训, 以加速形成太空攻防实战能力。美军这一系列动向将对未来太空领域安全与发展产生重大影响, 应引起我高度重视。     

Experimental and numerical investigations of interface properties of Ti6Al4V/CP-Ti/Copper composite plate prepared by explosive welding

Explosive welding technique is widely used in many industries. This technique is useful to weld different kinds of metal alloys that are not easily welded by any other welding methods. Interlayer plays an important role to improve the welding quality and control energy loss during the collision process. In this paper, the Ti6Al4V plate was welded with a copper plate in the presence of a commercially pure titanium interlayer. Microstructure details of welded composite plate were observed through optical and scanning electron microscope. Interlayer-base plate interface morphology showed a wavy structure with solid melted regions inside the vortices. Moreover, the energy dispersive spectroscopy analysis in the interlayer-base interface reveals that there are some identified regions of different kinds of chemical equilibrium phases of Cu–Ti, i.e. CuTi, Cu₂Ti, CuTi₂, Cu₄Ti, etc. To study the mechanical properties of composite plates, mechanical tests were conducted, including the tensile test, bending test, shear test and Vickers hardness test. Numerical simulation of explosive welding process was performed with coupled Smooth Particle Hydrodynamic method, Euler and Arbitrary Lagrangian-Eulerian method. The multi-physics process of explosive welding, including detonation, jetting and interface morphology, was observed with simulation. Moreover, simulated plastic strain, temperature and pressure profiles were analysed to understand the welding conditions. Simulated results show that the interlayer base plate interface was created due to the high plastic deformation and localized melting of the parent plates. At the collision point, both alloys behave like fluids, resulting in the formation of a wavy morphology with vortices, which is in good agreement with the experimental results.