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.     

PID在柴油发电机组输出稳定性控制中的应用研究

针对目前移动式柴油发电机组机械式调速器响应速度慢、精度差以及负载变化较大时发电机组输出电压和频率波动较大的问题,研究了PID在柴油发电机组稳定性控制中的应用,进行了电子调速器电路的研究与设计。对75kW柴油发电机组进行了空载、半载及满载实验,实验结果验证了设计电路和控制方法的正确性。该电子调速器采用PID方法对发动机转速进行控制,达到了改善柴油发电机组输出稳定性的目的,并且具有响应速度快和准确度高的特点。     

基于HLA的维修保障仿真系统设计研究

针对作战单元维修保障能力评估的需求,提出建立基于HLA的维修保障仿真分析平台。在分析维修保障系统构成和运行过程的基础上,阐述了仿真联邦的设计思想和构建方法,并进行了系统设计。根据实际系统的运行逻辑开发了联邦剧情,基于HLA的开发和执行过程模型构建了联邦系统框架,设计了联邦对象模型,并指出了仿真实现的关键技术所在。     

RTI测试研究

运行支撑系统(RTI)作为应用高层体系结构(HLA)进行分布仿真的支撑系统,是实现HLA的核心。RTI的功能和性能直接关系到HLA仿真系统开发与应用的成败。首先阐述了RTI测试的内容和指标,接着结合例子详细研究了RTI测试的方法,最后对RTI测试研究进行了总结,为提高基于HLA的分布交互仿真系统的质量及可信度提供了基础。     

HLA联邦的桥接扩展和影响时空一致性的实例分析

随着计算机技术和仿真应用的发展 ,越来越需要组建大规模分布仿真系统 ,HLA框架的定义和应用为此提供了很好的契机。使用桥接技术把不同的联邦连接起来是构建大规模联邦的有效方法 ,其中桥接邦元更适合于不同RTI的异地连接。桥接HLA联邦会带来影响系统时空一致性和性能的新问题 ,时间推进和所有权转移是两个有代表性的例子 ,需要重点解决     

空空导弹三维导引模型和机动目标导引规律研究

给出了三维空间导弹-目标追逃运动的空间矢量方程,在三维空间建立了导弹-目标的追逃运动模型。在目标运动信息完全未知条件下对变速机动目标应用李雅普诺夫稳定性分析方法提出了一种非线性三维制导算法,这种方法在导引末段不需要过大的加速度命令,不需要知道目标精确的加速度和速度方位信息。全弹道六自由度数学仿真结果表明了模型的正确性和制导算法的有效性。     

柴油机PID、F并联调速控制研究

为了提高柴油机动态和稳态控制性能,提出了PID、F并联调速控制的方法,并利用Matlab/Simulink工具箱对PID、F交替调速控制和并联调速控制进行了仿真研究,表明Fuzzy-PID并联控制的性能优于常规PID控制和单纯的模糊调速控制以及PID、F交替调速控制的调速性能.     

高能量强夯在处理湿陷性黄土地基和不良地质体工程中应用研究

结合某工程采用6 000 kN·m高能量强夯处理湿陷性黄土地基和人为采金遗留的不良地质体的工程实践,分析研究了高能量强夯的加固机理、施工工艺、有效加固深度、影响深度的计算方法及有关参数,探讨了该技术处理湿陷性黄土地基和不良地质体的优点与适用性等问题.     

弹性BP神经网络消除轮速传感器误差方法的研究

汽车轮速是汽车运动状态参数的主要信息源,是控制系统的核心,其精度直接影响这些系统的性能.为了提高轮速的精度,降低传感器的研制成本,提出了一种基于弹性BP神经网络的误差分析方法消除轮速传感器误差.将改进的BP神经网络--弹性BP神经网络用于误差分析,并提出误差匹配的算法.理论和仿真结果表明,该方法使绝对误差达到2×10-4>rad,能够有效地消除传感器误差,提高轮速信号的精度.