Ti含量对Ti-B4C-C体系自蔓延高温合成的影响

以14Ti+3B4C+5C为基础反应体系,通过热力学分析及静态燃烧合成实验研究了钛含量对该体系SHS反应的绝热温度、反应速度和产物致密度的影响.研究表明,Ti含量适当增加,能够使反应速度加快、产物致密度提高.当Ti过量16%(摩尔分数)时,体系的绝热温度仍高达3 193K,反应速度最快,产物的致密度也较高.     

热真空条件下工作的电气电缆载流量计算与试验

高空制导飞行器从母舱释放后,制导舱与仪器舱之间部分电气电缆处于热真空条件下工作。对此种特定条件下的电缆进行了载流量计算。理论计算表明,给定的电缆设计满足在热真空条件下正常工作要求。最后简略介绍了载流量试验。     

导弹大攻角高机动飞行特性分析与仿真

以新一代无翼式气动布局导弹为背景,在大攻角气动特性理论基础上,分析了在导弹主动段、攻角在180°范围内变化的导弹飞行特性,得出了90°内大攻角最大转弯能力和180°攻角附近最大降速效果的结论。进行了俯仰平面S型轨迹机动飞行仿真,仿真结果说明了大攻角飞行的高机动特性。     

基于目标特征的光学遥感图像舰船检测方法

针对在大场景、高分辨率的光学遥感图像舰船目标检测中,传统的阈值检测方法效果不佳,而恒虚警法计算量大的缺点,研究一种根据检测舰船目标的特征,对每个可能的目标区域,快速计算检测阈值的方法。同时,研究基于RNN网络及信噪比的特征选择方法,对目标的特征进行优选并对候选目标进行鉴别。实验结果表明,采用本文方法进行舰船目标检测能获得较好的检测结果.     

基于以太环网的舰载网络设计技术

在对国外舰载网络发展分析后,结合舰载网络发展的军事需求,提出了基于以太网环网构建舰载高可靠网络的发展思路,并探讨了基于以太环网的舰载网络的体系结构、舰载多业务接入等相关技术。最后,利用三台万兆交换机搭建了单环网络测试环境,测试结果表明,以太环网的保护及恢复时间满足舰载网络的可靠性要求,基于以太环网的舰载网络设计方案可行。     

Formation of adiabatic shearing band for high-strength Ti-5553 alloy: A dramatic thermoplastic microstructural evolution

By using split Hopkinson pressure bar, optical microscopy and electronic microscopy, we investigate the influence of initial microstructures on the adiabatic shear behavior of high-strength Ti–5Al–5V–5Mo–3Cr (Ti-5553) alloy with lamellar microstructure and bimodal microstructure. Lamellar alloy tends to form adiabatic shearing band (ASB) at low compression strain, while bimodal alloy is considerably ASB-resistant. Comparing with the initial microstructure of Ti-5553 alloy, we find that the microstructure of the ASB changes dramatically. Adiabatic shear of lamellar Ti-5553 alloy not only results in the formation of recrystallized β nano-grains within the ASB, but also leads to the chemical redistribution of the alloying elements such as Al, V, Cr and Mo. As a result, the alloying elements distribute evenly in the ASB. In contrast, the dramatic adiabatic shear of bimodal alloy might give rise to the complete lamination of the globular primary α grain and the equiaxial prior β grain, which is accompanied by the dynamic recrystallization of α lamellae and β lamellae. As a result, ASB of bimodal alloy is composed of α/β nano-multilayers. Chemical redistribution does not occur in ASB of bimodal alloy. Bimodal Ti-5553 alloy should be a promising candidate for high performance armors with high mass efficiency due to the processes high dynamic flow stress and excellent ASB-resistance.     

Deconsolidation and combustion performance of thermally consolidated propellants deterred by multi-layers coating

Both heating and solvent-spray methods are used to consolidate the standard grains of double-base oblate sphere propellants plasticized with triethyleneglycol dinitrate (TEGDN) (TEGDN propellants) to high density propellants. The obtained consolidated propellants are deterred and coated with the slow burning multi-layer coating. The maximum compaction density of deterred and coated consolidated propellants can reach up to 1.39 g/cm³. Their mechanic, deconsolidation and combustion performances are tested by the materials test machine, interrupted burning set-up and closed vessel, respectively. The static compression strength of consolidated propellants deterred by multi-layer coating increases significantly to 18 MPa, indicating that they can be applied in most circumstances of charge service. And the samples are easy to deconsolidate in the interrupted burning test. Furthermore, the closed bomb burning curves of the samples indicate a two-stage combustion phenomenon under the condition of certain thickness of coated multi-layers. After the outer deterred multi-layer coating of consolidated samples is finished burning, the inner consolidated propellants continue to burn and breakup into aggregates and grains. The high burning progressivity can be carefully obtained by the smart control of deconsolidation process and duration of consolidated propellants. The preliminary results of consolidated propellants show that a rapid deconsolidation process at higher deconsolidation pressure is presented in the dynamic vivacity curves of closed bomb test. Higher density and higher macro progressivity of consolidated propellants can be obtained by the techniques in this paper.     

利用RLC电路合成高压方波脉冲

基于过阻尼RLC电路分时放电,提出了一种新型高压方波脉冲产生方法。理论分析表明过阻尼RLC电路产生的双指数电压波与PFL产生的方形电压波具有类似的上升沿和平顶。电路模拟表明通过人工过零技术可以对双指数电压波进行截尾,从而形成完整的高压方波脉冲。建立了原理验证性样机,由两组RLC电路构成,每组电路包含一台400 nF脉冲电容器和一只三电极场畸变气体开关,两组电路共用一个上升沿调节电感。实验证明样机可以在250 Ω电阻负载上输出幅值17 kV,平顶宽度330 ns~5.8 μs,上升沿100~ 350 ns 的单极性高压方波脉冲。该方法适应性强,对负载变化不敏感,同时具有良好的可调节性,方波上升沿、平顶宽度连续独立可调。     

基于HLA分布式仿真的Web服务化

HLA虽然能够简化各类仿真系统的互操作和重用,但是接口规范与编程语言的绑定、缺乏与商业技术的融合等阻碍了它在商业领域的广泛应用,Web服务具有平台和厂商独立等良好特性,实现基于HLA分布式仿真的Web服务化能够将Web服务的优势附加给HLA.该文在分析了HLA不足和web服务优势的基础上,提出了HLA Web服务化,对比了互操作在两个上下文中的差异,分析了实现HLA Web服务化的三个层次;之后,概述了相关研究,重点讨论了实现Web使能RTI的关键技术问题及其解决方案;最后,设计了原型系统,测试结果显示原型系统能够初步实现RTI的Web服务化.     

HLA数据回放及其可通用性问题研究

为了给HLA分布仿真系统提供运行数据的回放能力并解决各种回放策略都必须面对的数据完备、时序准确、运行高效及回放方法的可通用性等问题,对HLA联邦中的数据回放问题进行了研究,分析了HLA仿真中的回放需求以及HLA对回放实现技术的影响,指出回放方法的可通用性实质上是联邦独立性的概念,研究了将回放数据对象化处理的方法,针对成员式数据回放策略、基于对象序列化技术和成员自动生成技术提出了一种可通用的HLA数据回放实现方案,最后介绍了通用HLA数据回放工具的应用情况。