一类二阶奇异Hamiltonian系统的非碰撞解

运用变分原理,拓扑度理论以及微局部分析技巧相结合的方法,作者讨论了一类二阶奇异Hamiltonian系统的时滞周期解之存在性。     

坦克履带板材料的现状和探讨

论述了现用坦克履带板的使用情况和主要失效形式,通过分析ZGMn13的加工硬化特点,提出了降低奥氏体的稳定性,在使用中实现应变诱发马氏体相变的强化机制,并完成了实验室条件下的成分设计和优化.     

船用汽轮机减速箱运行状态监测方法

本文对船用汽轮机减速箱运行状态监测方法进行了探讨。主要对可能用于船用汽轮机减速箱运行状态监测方法及相应的状态特征提取技术进行了分析,给出了一个一般的状态监测处理流程。然后讨论了监测方法的一般评价准则、特征量的选择准则及判决决策准则。最后给出了一个应用范例结果。     

坦克发动机技术状况的两种模糊诊断模型

提出了诊断坦克柴油机技术状况的模糊综合模型和模糊模式识别模型。对59坦克柴油机的技术状况进行了诊断计算,证实了这两种模型的实用性和可靠性。     

面向柔性加工环境的过程状态振动监测

本文运用提出的通用状态监测模型及策略,以振动信号监测为例,提取设备运行状态的振动信号方差和振动信号建立AR模型的参数估计的变化率参数作为两类通用特征参数,对柔性加工系统进行归一化监测,取得了良好的效果。建立的监测系统简洁、快速、可靠,满足柔性制造环境下设备运行状态监测的要求。     

极大单调算子零点的逼近问题

设H为实Hilbert空间,C为H的非空闭凸子集,T:C→2H为极大单调算子,假设S(T)={x∈H:0∈Tx}≠Φ。 xk∈H,βk>0,求 xk及ek满足( )　　xk+ek∈ xk+βkT( xk),‖ek‖≤ηk‖xk- xk‖, k≥0,其中,ηk≥0,supk>0ηk<1,βk≥β>0。设PC:H→C为H到C上的最近点投影算子,定义xk+1=PC( xk-ek),k≥0,证明了若T满足(S)型条件,则{xk}k≥0强收敛于T的某个零点。     

基于灰局势决策理论的维修级别分析方法

简要介绍了某型无人机维修级别分析及灰局势决策理论的一般概念,针对传统维修级别分析中经济性分析的数据来源广、模型可信度较差的情况,研究基于灰局势决策原理建模的一般方法,通过筛选原始数据并修正计算公式,大大减少了冗余计算,最后运用这一模型对某机载无线电设备进行了经济性分析。     

基于熵值法的坦克动力舱热工况的综合评价

坦克动力舱的结构和布置有多种型式,为了对不同结构的动力舱热工况的优劣进行对比、评价,必须用量化的指标加以衡量.提出了一种坦克动力舱热工况的评价指标体系,运用熵值法原理科学地确定各评价指标权重,建立了综合评价模型,并对某型主战坦克动力舱的不同布置方案进行了热工况综合评价.     

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.     

军用装备基于状态的维修策略研究

基于状态的维修(CBM)是设备(武器系统)预报初始故障的主动维修的一种形式[1],是本世纪初国内外维修领域研究的热点课题.研究目的是进一步推进基于状态的维修理论在军用装备领域的研究与应用.通过分析维修技术的变化和维修所面临的挑战,说明了CBM是一种更有效的维修方式.文章首先从技术的角度分析CBM可行性,采用流程图的方法对基于状态的维修工作过程(包括状态监控、故障诊断和预测、维修决策)进行了说明,最后探讨了基于状态的维修的发展趋势.研究证明,CBM具有很好的应用前景.