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.     

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。     

导线过负荷引燃能力的模拟实验研究

为了考查导线过负荷对不同可燃物的引燃能力，选择1．5,2．5和4mm^2三种规格的铝导线在不同倍数过负荷电流条件下进行实验，测得导线温度并观察过负荷导线对火场中常见的棉布、阻燃管、防水板的引燃能力。通过实验得出过负荷导线引燃能力与导线截面积、过负荷时间、过负荷电流的大小的关系，并讨论了可燃物种类对过负荷导线引燃能力的影响。结果表明，过负荷导线的引燃能力与过负荷电流和时间成正比，而导线的截面积对引燃能力的影响是多方面的。为防止火灾发生，在建筑物中布置导线时要远离可燃物并要穿阻燃管铺设。     

战区导弹防御系统(TMD)对抗技术浅析

探讨了战区导弹防御系统(TMD)对抗技术的初步设想与实现方法,重点对TMD系统激光对抗技术和TMD系统红外对抗技术进行了可行性分析论证,介绍了一些具体的光电对抗措施。     

高规在执行中面临的新问题及对策

分析目前《高层民用建筑设计防火规范》在执行中面临的新问题 ,并结合工程实例 ,对《高层民用建筑设计防火规范》中相关条款提出看法。     

加热时间和温度对过负荷铜导线金相组织的影响

模拟火灾现场的热环境对过负荷铜导线在不同温度下加热不同时间,冷却后得到一系列近似于火灾现场中遗留的过负荷铜导线试样。通过分析过负荷铜导线试样的金相组织,找出过负荷之后的加热温度和加热时间对其金相组织的影响。结果表明,过负荷铜导线在火灾现场继续受热时,随着受热温度的升高和时间的延长,其晶粒会进一步增大。在实际进行火灾原因判断时,为了准确反映火灾事实,应根据现场调查取证情况,结合鉴定结论进行综合分析,不断提高火灾调查工作的科学性和准确性。     

Influence of high overload on the collimating lenses of laser ranging systems

Collimating lenses are an important component of laser ranging systems, and high overload environments severely affect the beam shaping effect of such lenses. This study proposes a buffer isolation method on the basis of impact stress wave attenuation theory for collimating lens spacers. ANSYS finite element software was applied to simulate the high load dynamics of collimating lenses, and the buffer isolation performance of different materials and composite structures was compared and analysed. Optical simulation analysis of the collimating lenses under different buffer conditions was performed using ZEMAX software to study the mechanism by which a high overload affects the collimating lenses. High overload and optical shaping experiments based on theoretical analysis were further conducted. Results showed the superiority of butadiene rubber to polytetrafluoroethylene after application of 70000 g impact acceleration. The combination-gasket method was superior to the single-gasket method, and the sandwich combination-gasket method was superior to the double-layer combination-gasket method.     

电源插座过载火灾危险性分析

利用反复过载实验方法对电源插座分别采用1.5倍、2.0倍、2.5倍、3.0倍额定电流进行过载实验,在过载3次及6次后分别通以额定电流,得出了一系列温度—时间的变化曲线及相关数据,并进行了分析。在实验所得结果的基础上,分析了插座过载引起火灾的原因,并提出了相应的火灾预防对策,这对预防插座过载引起电气火灾,减少火灾损失具有重要意义。     

Performance study of jute-epoxy composites/sandwiches under normal ballistic impact

This study is undertaken to explore the use of natural fiber Jute-epoxy (JE), Jute-epoxy-rubber (JRE) sandwich composite for ballistic energy absorption. Energy absorbed and residual velocities for these composites are evaluated analytically and through Finite Element Analysis (FEA). FE analysis of JE plates is carried out for different thicknesses (3, 5, 10 and 15 mm). JE plates and JRE sandwiches having the same thickness (15 mm) are fabricated and tested to measure residual velocity and energy absorbed. The analytical results are found to agree well with the results of FE analysis with a maximum error of 9%. The study on JE composite plate reveals that thickness influences the energy absorption. Experimental and FE analysis study showed that JRE sandwiches have better energy absorption than JE plates. Energy absorption of a JRE sandwich is about 71% greater than JE plates. Damages obtained from FEA and testing are in good agreement. SEM analysis confirms composites failed by fiber rupture and fragmentation.