论兵器运用工程

本文阐述了兵器运用工程研究的目的、对象、内容及要解决的问题,简要地回顾了这门学科形成的过程,并着重讨论了构成本学科的专业理论和今后急待研究的方向。     

紧固件用钢复验的动态抽验方案

本文针对现行紧固件原材料进厂抽样复验方法的不足,套改《ISO2859计数抽查程序和图表》,提出动态抽样方案,并对新旧方案实际应用进行了比较。以比较科学的决策,取得提高效益、降低消耗的结果.     

对加强农村消防工作的思考

针对我国农村消防工作现状 ,就如何加强农村消防工作谈几点看法 ,旨在全面提高农村整体防灾能力。     

通用导弹告警设备的试验和研究

导弹在进攻时,其截面相当于一个偶极子天线或单根箔条,利用导弹对特定频率雷达信号的谐振特性来增大目标的散射截面积。通过反辐射导弹告警实验设备系统的实弹打靶试验,验证了该理论的正确性和可行性。     

一种面向对象类级状态测试的形式化方法研究

面向对象的软件开发给测试带来了新的挑战,传统的测试技术不能直接用于面向对象的软件测试中,必须对其进行扩充和完善.类级测试是面向对象测试过程中的一个重要阶段,而类状态的测试是类级测试的核心.作者将扩充后的黑盒测试技术应用到类状态的测试过程中,可直接使用方法级的测试数据有效测试类中方法间的交互及其类状态的变化.最后,通过一个实例说明对类级状态的测试及其测试用例的生成.     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

Pressure relief of underground ammunition storage under missile accidental ignition

Safety of underground ammunition storage is an important issue, especially during the accidental ignition of missiles. This work investigates the pressure and temperature distribution of the multi-layer underground ammunition storage with a pressure relief duct during the accidental ignition process of the missile. A large-scale experiment was carried out using a multi-layered restricted space with a pressure relief duct to simulate the underground ammunition store and a solid rocket motor to simulate the accidental ignition of the missile. The results show that when the motor gas mass flow increased by 5.6 times, the maximum pressure of the ammunition storage increased by 5.87 times. At a certain motor flow rate, when the pressure relief exhaust area at the end of the relief duct was reduced by 1/2, the maximum pressure on the first layer did not change. But the rate of pressure relief was reduced and the time delayed for the pressure of ammunition store to drop to zero. In this experiment, when the motor ignition position was located in to the third layer ammunition chamber, the maximum pressure was reduced by 32.9％ and also reduced the rate of change of pressure. In addition, for the experimental conditions, the theoretical analysis of the pressure relief of the ammunition storage is given by a simplified model. Based on the findings, some suggestions to the safety protection design of ammunition store are proposed.     

反作用轮低速特性观测补偿方法

反作用轮在现代高精度卫星姿态控制中占据着重要的地位。但由于反作用轮工作于低速状态,其转速过零时摩擦力矩的非线性特征将会对姿态控制精度产生较大的影响,并影响卫星运行寿命。基于Dahl摩擦模型建立了直流电机驱动的反作用轮系统数学模型,在此基础上设计了用于改善反作用轮低速性能的补偿观测器,并将其应用于三正交结构姿态控制系统。数字仿真说明此方法可以有效地抑制反作用轮低速摩擦产生的扰动,从而大幅度改善卫星姿态控制精度及其姿态稳定性。最后探讨了该观测器方法同变结构控制方法的综合应用前景。     

卧式储油罐罐体变位模型与罐容表标定

针对储油罐罐体变位影响油品计量精度的问题,建立了球冠形封头卧式储油罐罐体变位模型,将罐体变位后的油位高度转换成无变位时的油位高度,再利用罐体无变位时的储油体积计算模型得到变位后储油体积与油位高度的关系。分析了罐体变位对罐容表的影响,提出了一种基于最小二乘原理的变位参数识别算法,最后对该变位模型进行了检验,并采用插值算法重新标定了变位后的罐容表。结果表明:该变位模型与实际情况基本相符,变位参数识别算法能估计出罐体倾斜角度和偏转角度。     

两路相互注入锁定Nd:YAG激光器

通过锁定多模块输出激光相位实现激光功率扩展的相干合成技术是获得高能高光束质量光源的有效途径.本文分析了相互注入锁定相干合成的机理及其对激光器相干性的影响,利用偏振元件将两路独立的Nd:YAG激光器关联起来,解决了耦合过程中的损耗问题,实现了两路激光器的相互注入锁定,获得了总功率4.4W的部分相干激光输出,长曝光结果表明远场光斑峰值功率密度提高了1.4倍,对利用相干合成技术实现高能固体激光器技术进行了初步探索.