供油挂车泵机油温度变化规律实验研究

通过实验研究了100 mm野战输油管线供油挂车泵运行时及停运后机油温度随时间的变化规律。采用数据拟合、回归分析等数学方法,分别研究了供油挂车泵空载和带负荷两种情况下机油温度的变化规律;针对供油挂车泵各种工作状态,分析了影响机油温度变化的主要因素,建立了温度变化数学模型。研究结果为100 mm和150 mm野战输油管线供、输油挂车泵机组模拟器的研制提供了一定参考。     

舰载试验指挥控制系统研究与实践

针对靶场海上试验发展的综合需求,对舰载试验指挥控制系统发展的必要性及现状进行了分析,重点从与靶场其它系统的接口关系、系统功能、体系结构及软件设计几方面完成了系统总体设计研究,最后阐述了系统实现过程的关键技术。实践表明,该系统的应用大大提高了海上试验指挥水平。     

Bionic stab-resistant body armor based on triangular pyramid structure

A stab-resistant substrate was designed and realized with a triangular pyramidal structure, inspired by the biological armor model in nature. The stab-resistance behavior and dynamic response mechanisms were studied through numerical simulation and experimental testing of a knife impacting a substrate, and an optimal structural design was obtained accordingly, with a tilted angle of 22.5° and optimal thickness of 1.2 mm. It was shown that the triangular pyramidal structure generated twice the internal energy of the knife than the flat substrate due to the dispersing effect of the structure. The force parallel to the inclination caused a significant scratch on the substrate surface, while the force perpendicular caused obvious substrate deformation. A new riveting method was used to form the total layer, which passed the GA 68—2008 standard. The stab-resistant clothing coupled with the reduced wearing burden could provide effective protection and avoid fatal injuries on security personnel working in dangerous environments. The method provided may enlighten the future design and manufacturing of stab-resistant clothing.     

Influence of propagation direction on operation performance of rotating detonation combustor with turbine guide vane

Due to the pressure gain combustion characteristics, the rotating detonation combustor (RDC) can enhance thermodynamic cycle efficiency. Therefore, the performance of gas-turbine engine can be further improved with this combustion technology. In the present study, the RDC operation performance with a turbine guide vane (TGV) is experimentally investigated. Hydrogen and air are used as propellants while hydrogen and air mass flow rate are about 16.1 g/s and 500 g/s and the equivalence ratio is about 1.0. A pre-detonator is used to ignite the mixture. High-frequency dynamic pressure transducers and silicon pressure sensors are employed to measure pressure oscillations and static pressure in the combustion chamber. The experimental results show that the steady propagation of rotating detonation wave (RDW) is observed in the combustion chamber and the mean propagation velocity is above 1650 m/s, reaching over 84% of theoretical Chapman-Jouguet detonation velocity. Clockwise and counterclockwise propagation directions of RDW are obtained. For clockwise propagation direction, the static pressure is about 15% higher in the combustor compared with counterclockwise propagation direction, but the RDW dominant frequency is lower. When the oblique shock wave propagates across the TGV, the pressure oscillations reduces significantly. In addition, as the detonation products flow through the TGV, the static pressure drops up to 32% and 43% for clockwise and counterclockwise propagation process respectively.     

Experimental investigation on enhanced damage to fuel tanks by reactive projectiles impact

Enhanced damage to the full-filled fuel tank,impacted by the cold pressed and sintered PTFE/AL/W reactive material projectile(RMP)with a density of 7.8 g/cm3,is investigated experimentally and theoretically.The fuel tank is a rectangular structure,welded by six pieces of 2024 aluminum plate with a thickness of 6 mm,and filled with RP-3 aviation kerosene.Experimental results show that the kerosene is ignited by the RMP impact at a velocity above 1062 m/s,and a novel interior ignition phenomenon which is closely related to the rupture effect of the fuel tank is observed.However,the traditional steel projectile with the same mass and dimension requires a velocity up to 1649 m/s to ignite the kerosene.Based on the experimental results,the radial pressure field is considered to be the main reason for the shear failure of weld.For mechanism considerations,the chemical energy released by the RMP enhances the hydrodynamic ram(HRAM)effect and provides additional ignition sources inside the fuel tank,thereby enhancing both rupture and ignition effects.Moreover,to further understand the enhanced ignition effect of RMP,the reactive debris temperature inside the kerosene is analyzed theoretically.The initiated reactive debris with high temperature provides effective interior ignition sources to ignite the kerosene,resulting in the enhanced ignition of the kerosene.     

基于粗糙集和神经网络的无人机侦察效能评估

针对无人机在多条件下的侦察效能评估问题,提出一种基于粗糙集和神经网络的无人机侦察效能评估方法.在该方法中,寻找影响因素构建无人机侦察效能评估指标体系;结合粗糙集理论去除当中的冗余因素;并在处理因素基础上利用遗传优化的BP神经网络构建无人机侦察效能的评估模型,以提高预测精度.仿真结果表明:该模型不仅能够克服传统BP神经网络容错性差,收敛速度慢的缺点,而且可以较好地完成无人机侦察效能评估.     

气体灭火系统联动可靠性探讨

气体灭火系统用在特殊、重要的场所,其联动控制可靠性是成功灭火的关键.但由于设计单位、建设单位重视不够,影响了联动可靠性.为此针对气体灭火系统联动控制模式规范设计,严把施工质量关,搞好配套设备的控制,以确保系统联动控制可靠性.     

有约束的Hartley域自适应算法的应用研究

通过对有约束的Hartley域自适应算法、频域自适应算法及时域自适应算法用于自适应降噪系统的计算机仿真研究 ,认为在自适应通信降噪中采用基于Hartley变换的自适应算法较频域自适应算法及时域自适应算法性能更优、降噪效果更好 ,并在高速信号处理器TMS32 0C30上开发实现了该算法 .实验结果表明 ,将Hartley域自适应算法应用于通信降噪系统 ,方法实际可行     

全垫升式气垫船水压场数值模拟

提出了任意分布的气垫压力所产生的水压场的计算方法 ,对椭圆域上均匀分布的气垫压力产生的水压场进行了数值模拟 ,并将计算结果与实验进行了比较 .结果表明 ,用数值模拟的方法研究全垫升式气垫船水压场是可行的     

化学敏感材料的应用与发展

对敏感材料的特点、分类及其在科技、化工等领域内的广泛应用和发展前景 ,进行了较全面的综述