Shock initiation performance of NTO-based polymer bonded explosive

3-nitro-1,2,4-tri-azol-5-one (NTO) is a high energy insensitive explosive. To study the shock initiation process of NTO-based polymer bonded explosive JEOL-1 (32%octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX), 32% NTO, 28% Al and 8% binder system), the cylinder test, the gap experiments and numerical simulation were carried out. Firstly, we got the detonation velocity (7746 m/s) and the parameters of Jones-Wilkins-Lee (JWL) equation of state (EOS) for detonation product by cylinder test and numerical simulation. Secondly, the Hugoniot curve of unreacted explosive for JEOL-1 was obtained calculating the data of pressure and time at different Lagrangian positions. Then the JWL EOS of unreacted explosive was obtained by utilizing the Hugoniot curve as the reference curve. Finally, we got the pressure growth history of JEOL-1 under shock wave stimulation and the parameters of the ignition and growth reaction rate equation were obtained by the pressure-time curves measured by the shock-initiation gap experiment and numerical simulation. The determined trinomial ignition and growth model (IG model) parameters can be applied to subsequently simulation analysis and design of insensitive ammunition with NTO-based polymer bonded explosive.     

A numerical study on the disturbance of explosive reactive armors to jet penetration

The disturbance of flat and V-shaped sandwich reactive armor configurations to shaped-charge jet is studied by a numerical approach. The disturbing and cutting effects of the two reactive armor configurations to the jet are successfully captured. The predicted disturbance characteristics and patterns are in fairly good agreement with the X-ray photographic observations. The residual depth of penetration into a semi-infinitive homogeneous steel target behind the reactive armor is computed for a series of jet/armor parameters. For the flat configuration, it is demonstrated that the residual penetration depth is not significantly reduced for a normal impact while it is reduced up to 75% for an oblique impact. In comparison, the V-shaped configuration reduces the penetration depth of the jet to 90%, and it is observed that the penetration depth is not sensitive to the V-shaped angle.     

环管型燃烧室喷雾燃烧DES模拟

为研究燃气轮机燃烧室内复杂的两相三维湍流燃烧问题,采用基于Realizable k-ε模型的分离涡模拟(DES)方法对环管型燃烧室进行喷雾燃烧数值模拟.数值模拟结果表明:DES模拟在燃烧区发挥出大涡模拟(LES)的作用,能获取结构复杂的流场、温度场和涡量场,其对流场内涡结构的捕捉和分辨能力明显强于传统的RANS(雷诺时均N-S方法)模拟.与实验数据对比发现,DES模拟所得燃烧产物含量和燃烧室出口温度分布更符合.因此,DES方法可用于复杂形状燃烧室的燃烧数值模拟,能够避免RANS模型对湍流脉动进行平均处理导致耗散过大、抹平涡结构的缺点,从而可获取更准确的计算结果.     

一种新型内孔热喷涂技术及涂层性能研究

介绍了一种新型的内孔热喷涂技术———离心雾化等离子喷涂技术,并阐述了该技术的工作原理和工作过程。通过试验制取了3Cr13涂层和铝涂层,使用扫描电镜、能谱仪和光学显微镜等仪器设备对2种涂层的表面和截面进行观察分析,结果表明,通过该技术制取的涂层具有和传统电弧喷涂层类似的组织结构,并具有氧化物含量低,喷涂粒子大等特点。     

全气动步兵武器表层自动喷涂机设计

分析目前步兵武器零件表层喷涂技术现状,提出全气动自动喷涂机设计方案,根据步兵武器零件结构特点,规划自动喷涂轨迹,设计全气动自动化喷涂专用设备．该设备具有本质安全性,适于部队条件下使用．     

自动喷水灭火系统喷头布置探讨

依据《自动喷水灭火系统设计规范》(GB50084-2001),结合实际工程设计经验,就规范对喷头布置的一般规定在具体工程设计中可能存在的矛盾和问题进行了分析,并提出了具体解决办法。     

气液同轴离心式喷嘴雾化特性实验研究

采用自行设计的两相喷雾实验设备和测量装置,通过ＭＦ激光散射测粒仪,对液氧液氢火箭发动机所用量气液同轴离心式喷嘴后方喷雾液滴的平均直径ＭＭＤ和液滴尺寸分布指数ｎ等雾化特性,进行了试验研究,测量了Ａ型喷嘴在不同气体和液体喷注压降、不同空间位置的喷雾特性。分析了气体喷注压降一定时液体喷注压降对雾化特性的影响规律,以及当液体喷注压降一定时气体喷注压降对雾化特性的影响规律,得出了一些有意义的结论。研完结果对气液同轴离心式喷嘴设计有一定的指导意义。     

基于变步长LMS的谐波电流检测方法的研究

能否快速准确检测出三相电力系统中谐波电流是决定有源滤波器整体滤波性能的关键.基于瞬时无功功率的谐波电流检测理论,提出了一种改进的自适应滤波器谐波检测算法,通过构造步长因子与误差信号的非线性函数,调整步长参数,使权向量达到最优,在确保稳态误差的前提下,提高了系统的收敛速度.仿真实验验证了该算法的正确性和有效性.     

高掺量碳纤维增强活性粉末混凝土力学性能实验

采用一种新的碳纤维自分散工艺和专用分散设备制备出了掺量达胶结材质量8％的碳纤维增强活性粉末混凝土；研究了碳纤维掺量对活性粉末混凝土的力学性能影响规律。实验结果表明，在碳纤维掺量高时，活性粉末混凝土的力学性能受碳纤维掺量和水胶比两个因素共同作用。     

试论自动喷水灭火系统在控制群死群伤火灾事故中的关键作用

对自动喷水灭火系统在控制群死群伤火灾事故中的关键作用加以阐述，使消防工作又好又快的向前发展，为社会经济的发展做出更大的贡献。