基于智慧校园建设推进军队院校教育现代化路径探究

教育信息化是教育现代化的基本内涵和显著特征。当前,我国正处于由基本实现教育现代化迈向整体实现教育现代化的重要战略期,国家教育从理论和实践层面进行了大量探索。在军队院校教育领域,教育技术应用、训练管理领域网络建设、数字校园建设等均为军队院校教育现代化奠定了创新发展基础,智能教育应用模式的改革探索也为军队院校教育现代化描绘了未来建设愿景。本文认为,推进军队院校教育现代化应发挥智慧校园建设平台的基础作用,充分融入国家教育体系,注重以先进教育理念驱动创新发展、以前沿信息技术提供解决方案、以总体架构设计规范目标功能、以智慧育人环境承载应用服务、以数据资源体系孕育智慧生态,走开军委军种院校三级联动推动创新发展的路子。     

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.     

裂纹叶片非线性振动响应理论分析与实验验证

叶片裂纹严重威胁航空安全,已引发数起严重飞行事故。为诊断叶片早期裂纹,对裂纹叶片的非线性振动规律进行了理论和实验研究。建立了裂纹叶片动力学非线性模型,梳理了裂纹尺寸与动力学参数的对应关系,推导得到了非线性振动响应谐波分量功率的耦合量化关系式,结果表明叶片振动分量谐波功率与相邻分量谐波功率以及谐波分量的阶次有关,而且谐波分量相对功率与裂纹深度呈正相关。据此,提出了一种基于谐波分量相对功率的裂纹检测方法。对钢直板叶片进行了模拟仿真和振动台实验,仿真结果和实验结果都表明这种方法可以有效区分裂纹叶片和正常叶片。     

通信设备及其网络仿真训练模型的分析

根据通信设备及其网络的特点和通信业务训练的要求 ,提出了层次化结构的仿真训练模型 ,并提供和分析了各层建模方法和编程技术。然后介绍了通信设备及其网络仿真训练系统的典型实例 ,结果表明 :该模型对于建立通信设备及其网络仿真训练系统具有易于代码开发、易于理解、易于维护管理、易于系统功能扩展的特点。     

程控交换机硬件系统建模研究

底层功能实现模块是程控交换机多媒体仿真训练系统通用设计平台的关键部分。硬件配置是交换机工作的基础 ,是底层功能实现模块的重要组成部分。该文介绍了交换机硬件系统的建模 ,利用两种典型机型硬件实际的工作情况 ,解释并验证了所建立的通用功能流程图 ,并介绍了参数接口的管理与应用