Polymer composite for antistatic application in aerospace

The phenomenon of static electricity is unpredictable, particularly when an aircraft flying at high altitude that causes the accumulation of static charges beyond a threshold value leading to the failure of its parts and systems including severe explosion and radio communication failure. The accumulation of static charges on aircraft is generated by the virtue of interaction between the outer surface of aircraft and the external environmental attributes encompasses air particles, ice, hail, dust, volcanic ash in addition to its triboelectric charging. In the recent years, advanced polymer-based composites or nanocomposites are preferred structural constituents for aircrafts due to their light weight and comparable mechanical properties, but such composite systems do not render low impedance path for charge flow and are subsequently vulnerable to effect of lightning strike and precipitation static. In this context, it is essential to develop conductive composite systems from non-conductive polymer matrix by nanofiller embodiments. The advent of carbon-based nanocomposite/nanomaterials have adequately addressed such issues related to the nonconductive polymer matrix and further turned into an avant-garde genre of materials. The current review envisioned to illustrate the detailed exploitation of various polymer nanocomposites in addition to especially mentioned epoxy composites based on carbon fillers like carbon black, carbon nanotube (single walled carbon nanotube and multi walled carbon nanotube) and graphene the development of antistatic application in aircraft in addition to the static charge phenomenon and condition for its prevalence in avionic systems.     

应用锤击法的大型复合材料桁架结构段自由振动分析

复合材料桁架结构以其轻质和优异的力学性能应用于大型航天航空飞行器结构,其承载能力和振动特性是决定其应用效果的关键因素。本文考察了大型碳纤维/环氧复合材料方形截面桁架结构段的自由振动特性。采用锤击法实验测试得到了复合材料桁架结构段自由振动的模态和频率,并与有限元数值模拟结果进行对比分析,论证了锤击法测试振动特性在复合材料桁架结构上应用的可行性和准确性。     

Survey and technological analysis of laser and its defense applications

The laser technology has made remarkable progress over the past couple of decades.It is being widely employed in diverse domains,such as holography,space sciences,spectroscopy,medical sciences,micro and power electronics,industrial engineering,and most distinctively,as directed energy military weapons.Owing to their active transmissions,laser systems are similar to microwave radars to some extent;however,unlike conventional radars,the laser operates at very high frequencies thus making it a potent enabler of narrow-beam and high energy aerial deployments,both in offensive and defensive roles.In modern avionics systems,laser target indicators and beam riders are the most common devices that are used to direct the Laser Guided Weapons(LGW)accurately to the ground targets.Additionally,compact size and outstanding angular resolution of laser-based systems motivate their use for drones and unmanned aerial applications.Moreover,the narrow-beam divergence of laser emissions offers a low probability of intercept,making it a suitable contender for secure transmissions and safety-critical operations.Furthermore,the developments in space sciences and laser technology have given syner-gistic potential outcomes to use laser systems in space operations.This paper comprehensively reviews laser applications and projects for strategic defense actions on the ground or in space.Additionally,a detailed analysis has been done on recent advancements of the laser technology for target indicators and range-finders.It also reviews the advancements in the field of laser communications for surveillance,its earlier state of the art,and ongoing scientific research and ad-vancements in the domain of high energy directed laser weapons that have revolutionized the evolving military battlefield.Besides offering a comprehensive taxonomy,the paper also critically analyzes some of the recent contributions in the associated domains.     

切向空气气流对激光辐照碳纤维复合材料的影响

实验研究了靶材表面存在和不存在切向空气气流时,975nm连续激光对碳纤维增强树脂基复合材料的辐照效应,发现切向气流的加载有利于激光对碳纤维复合材料的破坏.从理论上对激光辐照下碳纤维复合材料的破坏机理进行了初步分析,基于碳的氧化特性和氧化反应机理,推导了碳纤维的氧化速率方程.采用改进的光滑粒子方法,对激光辐照下复合材料树...     

定量反馈理论在侧向飞行控制系统中的应用

分析总结了定量反馈理论(QFT)的基本原理、设计步骤和特点,运用该理论对飞行控制系统(FCS)进行了设计研究.针对侧向通道的多输入多输出耦合系统,研究了QFT理论在多变量解耦控制问题中的应用.研究发现,QFT能够很好地解决飞行控制系统由于模型参数具有不确定性而造成的控制系统鲁棒性设计问题.仿真表明该理论具有良好的鲁棒性能和解耦能力.     

水下激光成像系统在反蛙人侦察中的应用

水下激光成像系统作为一种主要的水下光电侦察装备,具有抗干扰能力强、探测距离远、成像质量高等诸多优点,可用于探测水下多种类型的目标。针对水下激光成像系统的反蛙人侦察应用问题展开研究,介绍了水下激光成像系统反蛙人侦察的技术、特点和现状,重点研究了水下激光成像系统几种典型的反蛙人侦察使用方法,并对今后水下激光成像系统反蛙人侦察的发展趋势进行了分析。     

“艾科尔斯”改进型光学助降系统的纵向着舰精度研究*

基于“艾科尔斯”(ICOLS:Improved carrier optical landing system)改进型光学助降系统的人工着舰系统是几种新型光电或激光舰载机助降系统之一,研究了“ICOLS”改进型光学助降系统的引导技术,整个系统的关键是引入激光束。研究重点是当航母在海浪、海涌干扰作用时,飞机在ICOLS系统引导下,人工操纵飞机着舰时的仿真结构配置,并导出终端误差方程。最后给出了在典型海浪作用下,ICOLS近程系统采用角稳定助降系统控制律的着舰精度仿真计算实例,从而为地面仿真研究着舰误差提供了基本思路与研究手段,对保证飞机安全着舰有十分重要的意义。     

射频隐身反隐身E&V系统的设计与实现

针对战机射频隐身性能很难评估的现实问题,提出一种射频隐身反隐身实验与验证半实物仿真系统的设计与实现方法。该系统不仅能对战机的射频隐身性能进行验证,同时还可以对飞机的隐身波形、辐射策略等设计提供理论依据和实验支撑。在分析辐射信号模型以及截获模型的基础上,详细介绍了该系统的各功能组成和结构框图。该系统可以开展对于射频隐身的作战需求、管控模型、使用准则等方面的定量研究,对于提高战机的生存能力、突防能力和作战能力具有重要的意义。     

复合材料修补金属裂损结构吸湿老化的试验与有限元分析

暴露在湿热环境中的复合材料修补金属裂损结构易吸湿老化,导致该结构性能下降,服役寿命缩短。为研究吸湿性对复合材料修补金属裂损结构修补效果和耐久性的影响,利用试验方法分析了吸湿性对复合材料胶补金属裂损结构及胶黏剂力学性能的影响;利用有限元方法评估了吸湿性对复合材料胶补金属裂损结构试验件修补效果和耐久性的影响。研究结果表明:吸湿后含穿透双边裂纹铝合金板玻璃纤维单面胶补试验件的疲劳裂纹扩展寿命和极限载荷的平均值分别下降为吸湿前的71%和90%;吸湿造成拉伸条件下复合材料胶补金属裂损结构胶层失效模式由内聚破坏为主转变为界面破坏为主;在"湿-热"老化30天后,E44/聚酰胺环氧树脂胶黏剂试验件吸水饱和,弹性模量下降为未老化前的40%,塑性应变超过了总应变的25%;有限元分析发现胶层损伤受吸湿影响明显,吸湿性加速了胶层损伤,且裂纹长度越长,加速作用越明显;同时吸湿使得裂纹尖端的J积分值急剧增大,导致修补结构的疲劳裂纹扩展寿命缩短,裂纹长度越长,吸湿性对于复合材料胶接修补效果的危害越严重。     

飞机发动机关键系统智能故障诊断方法

飞机发动机是一个非常复杂的大系统,由于其结构复杂,工作环境恶劣,对其关键系统的故障进行准确诊断始终是困扰业界的技术瓶颈之一。提出了采用EMD小波阈值降噪与主元分析相结合的方法,对飞机发动机气路系统故障诊断进行了深入研究。针对某型真实飞机发动机进行测试试验采集的气路多参量数据,首先采用经验模态分解(Empirical Mode Decomposition,EMD)对气路系统各参量信号进行EMD分解,然后采用软阈值函数对其进行降噪,并进行信号重构,从而可得到飞机发动机气路工作状态有效数据。在此基础上,设计了飞机发动机气路系统主元分析故障诊断模型,并结合预处理得到的飞机发动机气路有效数据,运用所设计的主元分析故障诊断模型对飞机发动机进行故障诊断技术研究。研究结果表明,所提出的方法能够很好地诊断出飞机发动机气路系统实际运行时所出现的故障,具有重要的实际应用价值,并有广泛的应用前景。     

Direct ink writing of 3D-Honeycombed CL-20 structures with low critical size

3D-Honeycombed CL-20 structures with low critical size of detonation have been fabricated successfully for intelligent weapon systems using a micro-flow direct ink writing (DIW) technology. The CL-20-based explosive ink for DIW technology was prepared by a two-component adhesive system with waterborne polyurethane (WPU) and ethyl cellulose (EC). Not only the preparation of the explosive ink but also the principle of DIW process have been investigated systematically. The explosive ink displayed strong shear-thinning behavior that permitted layer-by-layer deposition from a fine nozzle onto a substrate to produce complex shapes. The EC content was varied to alter the pore structure distribution and rheological behavior of ink samples after curing. The deposited explosive composite materials are of a honeycombed structure with high porosity, and the pore size distribution increases with the increase of EC content. No phase change was observed during the preparation process. Both WPU and EC show good compatibility with CL-20 particles. Apparently high activation energy was realized in the CL-20-based composite ink compared with that of the refined CL-20 due to the presence of non-energetic but stable WPU. The detonation performance of the composite materials can be precisely controlled by an adjustment in the content of binders. The 3D honeycombed CL-20 structures, which are fabricated by DIW technology, have a very small critical detonation size of less than 69 μm, as demonstrated by wedge shaped charge test. The ink can be used to create 3D structures with complex geometries not possible with traditional manufacturing techniques, which presents a bright future for the development of intelligent weapon systems.     

定向能武器技术的发展动向

随着激光、新材料、微电子、声光、电光等高技术的发展,利用各种束能产生强大杀伤威力的定向能武器已引起世界高度重视。定向能武器成为战场上高速移动目标的"克星",是能有效制敌的"杀手锏"装备,对未来作战样式和形态具有重要影响。文章系统分析了定向能武器的军事应用前景,详细剖析了世界定向能武器技术的研究进展及发展动向,给出了未来要大力发展的激光武器、高功率微波武器和粒子束武器关键技术,对于加快我军定向能武器装备发展,提升非对称制衡能力,具有十分重要的意义。     

作战实验在海军装备体系建设中的应用研究

结合国内外作战实验研究现状,详细分析了作战实验体系的应用领域和类别,描述了典型作战实验体系的构架,在此基础上重点对作战实验在海军装备体系建设中的应用需求进行了分析,最后提出了一种作战实验在海军装备体系建设中的典型应用模式。     

舰载激光武器系统建模与仿真技术

针对舰载激光武器系统仿真技术发展要求和应用方向,通过对舰载激光武器系统组成、功能和作战过程的分析,归纳整理出一套较完整的舰载激光武器仿真模型,其中对激光能量传输仿真模型和毁伤效果仿真模型进行详细描述;并提出仿真软件设计方案,包括软件功能组成、软件结构、软件运行流程等仿真软件设计要点;最后介绍了软件的仿真输出结果。文中设计的仿真软件可支持舰载激光武器系统的设计开发,也可以应用到舰船新型防空反导火控系统仿真认证中。     

Influence of high overload on the collimating lenses of laser ranging systems

Collimating lenses are an important component of laser ranging systems, and high overload environments severely affect the beam shaping effect of such lenses. This study proposes a buffer isolation method on the basis of impact stress wave attenuation theory for collimating lens spacers. ANSYS finite element software was applied to simulate the high load dynamics of collimating lenses, and the buffer isolation performance of different materials and composite structures was compared and analysed. Optical simulation analysis of the collimating lenses under different buffer conditions was performed using ZEMAX software to study the mechanism by which a high overload affects the collimating lenses. High overload and optical shaping experiments based on theoretical analysis were further conducted. Results showed the superiority of butadiene rubber to polytetrafluoroethylene after application of 70000 g impact acceleration. The combination-gasket method was superior to the single-gasket method, and the sandwich combination-gasket method was superior to the double-layer combination-gasket method.     

海军装备体系技术构成探析

在剖析海军装备体系与体系技术概念的基础上,分析了海军装备体系技术的特点与作用,提出了海军装备体系技术的基本构成,为海军装备体系技术的应用研究提供理论指导。     

Crashworthiness performance of hybrid kenaf/glass fiber reinforced epoxy tube on winding orientation effect under quasi-static compression load

This research was aimed to study the effect winding orientation on the crashworthiness performance of hybrid tube. The specimens tested under quasi-static compression load involve of three winding parameters (θ = 30°, 45° and 70°) of hybrid kenaf/glass fiber reinforced epoxy and glass fiber reinforced epoxy as contrast specimen. The automated filament winding technique has been used in fabrication of hybrid and non-hybrid composite tube and crashworthiness performance was investigated experimentally. The effects of winding orientation on energy absorption capabilities and crashworthiness characteristic were investigated through quasi-static compression load and the result are compared with the glass fiber composite tube to justify the capability of hybrid natural/synthetic as energy absorption application. Hybridized samples proved to enhancing the progressive crushing capability as combination of local buckling, delaminate and brittle fracturing as progressive crushing modes.In the view of winding orientation aspect, the results of high winding orientation of hybrid composite tube elevated the crush load efficiency, specific energy absorption and energy absorption capability compared to glass composite tube (GFRP). The hybrid kenaf/glass composite tube with high winding orientation showed the best winding orientation to enhance the energy absorber characteristics as energy absorption application.     

电磁弹射过程中涡流引入阻力的分析

永磁直线电机能够满足电磁弹射系统短距内高加速与快制动的应用要求,但是永磁直线电机的快速运动可能引入明显的涡流效应,在电机加速度段,涡流效应引入涡流阻力,削弱了系统的弹射能力,另一方面,在电机的制动段,涡流效应引入的阻力可以帮助系统实现快速制动.针对电磁弹射系统所采用的定子开槽、集中绕组、动磁式永磁直线电机,仿真分析了动...     

航空集群系统构建机理研究

围绕航空集群系统构建问题,从集群系统构建基本概念与内涵、构建要素以及构建思路及流程3个方面对集群系统构建机理进行阐述。首先,在分析集群系统的基本概念与内涵的基础上,提出了集群系统构建的概念;然后,将集群系统构建要素分为硬件资源、软件资源以及网络资源,并进行了梳理;最后,在分析集群作战一般流程的基础上归纳出了集群系统构建思路,并给出了构建流程。     

BTT控制系统半实物仿真方案 设计及试验结果分析

BTT控制系统半实物仿真试验以BTT试验器为背景,配合BTT控制技术研究可全面验证导弹控制系统设计。给出了半实物仿真试验方案、方法及试验结果分析,试验结果表明BTT控制系统设计满足最小侧滑(近似零侧滑角)倾斜转弯的技术指标要求,半实物仿真试验方法正确。