基于Hurst指数的油罐声发射信号分析

由油罐声发射检测直接得出油罐底板状态等级的评价研究工作有待完善。提出一种基于Hurst指数理论分析声发射信号幅值最大值分布的评价方法。从Hurst指数分形理论出发,结合声发射信号参数处理方法,给出研究条件假设,分析现场油罐声发射信号结果,并与开罐检测的底板状况加以对比分析。研究发现,相同检测条件,同种类型油罐底板状态等级与Hurst指数呈相反的关系。     

一种高炮拦阻射击新体制

针对高炮拦阻射击,提出了一种新射击体制,详细叙述了该体制的实现机理,并建立了数学模型。在此基础上,针对某型现役高炮的武器性能参数,探讨了初速序列的确定等关键问题,并进行了数值计算。该体制射击过程中不需要改变方向角和射角,对随动系统的要求大幅降低,可缓解自行高炮系统的随动制约,还可使大量随动性能较差的牵引高炮重新焕发生机。该体制的提出与最终实现对提升高射综合体防空反导作战效能具有重要意义。     

营区文化景观塑造之思考

文化景观在现代营房建设及部队发展过程中发挥着举足轻重的作用,为打造营区特色文化,分析了营区文化景观的内涵和意义,指出了当前营区文化景观建设中存在的主要问题,并在此基础上提出了营区文化景观塑造的策略:尊重地域特色;挖掘营区历史;凸显主题精神;打造创意小品。     

一种新的双输入多通道直流变换器

在传统的含储能单元分布式供电系统中,一般都需要多个单向直流变换器和双向直流变换器才能实现其功能。提出一种新的双输入多通道直流变换器,它的功能等效于一个单向直流变换器和一个双向直流变换器。分析了双输入多通道直流变换器的工作原理,给出了变换器的稳态关系式以及能量管理方法,并运用Saber软件进行仿真,验证了理论分析的正确性。该直流变换器除具有双输入Buck直流变换器的优点外,还能实现可再生能源向储电输入源充电。     

基于灰色关联投影法的空中加油机驻场选址评价

提出了一种基于灰色关联投影法的空中加油机驻场选址评价方法,分析了空中加油机驻场选址影响因素,设计了评价指标体系,并运用熵值理论客观赋权,构建了加权灰色关联决策矩阵。通过比较备选方案与理想方案灰色关联投影角,根据灰色关联投影值对备选方案进行优劣排序。算例分析结果符合现实场站选择条件,说明该方法能够有效解决空中加油机驻场选址问题。     

耐海水高耐候丙烯酸树脂的合成及面漆性能分析

为合成耐海水与高耐候的丙烯酸树脂,选择甲基丙烯酸甲酯、甲基丙烯酸羟丁酯、丙烯酸异辛酯和丙烯酸已内酯,经引发剂作用,采用同步滴加法进行聚合反应,通过调节温度并测定酸价控制反应历程,并将合成的不同玻璃化温度的丙烯酸树脂配制成具有适当玻璃化温度梯度的耐海水面漆成膜树脂体系。选择HDT-90固化剂与丙烯酸成膜树脂作用,制备耐海水面漆涂层样品。性能测试结果表明,研制的耐海水面漆具有优良的耐候性和抗老化性。     

损伤本构模型在边坡工程损伤破坏研究中的应用

从材料破坏机理与规律出发研究结构性土体工程的渐进破坏过程,是实际工程研究的重要方向。针对结构性土的变形特点和传统本构模型解决结构性土体工程渐进破坏过程的不足,采用作者以前提出的结构性土损伤本构模型对边坡工程算例的渐进破坏过程进行模拟分析。算例计算结果分析表明：边坡在破坏过程中会形成一个贯通剪切带,剪切带土体完全损伤;剪切带上方土体损伤相对较小,且有距离剪切带越远损伤越小的趋势;剪切带下方土体损伤也较小,主要因为开挖对其影响很小且处于稳定的坡体内。研究证明,运用结构性土损伤本构模型能较好地解决实际工程损伤破坏问题。     

音波法气体管道泄漏定位影响因素分析及算法改进

为提高音波法气体管道泄漏定位的精度,对影响该方法泄漏定位的主要因素以及定位算法进行了研究。通过假设计算,分析了绝热指数和压缩因子对定位精度的影响。结果表明,压力较大时绝热指数和压缩因子变化较大,在定位计算中不能忽略。在此基础上,考虑管内沿线气体的流速、温度和压力分布等因素,对音速公式、气体流速公式以及定位公式进行修正,从而得到可以较为精确求解泄漏位置的计算公式,并通过牛顿-科茨公式改进算法。研究结果对进一步完善音波法管道气体泄漏检测技术具有一定的设计和理论指导意义。     

Driving force coordinated control of an 8 ×8 in-wheel motor drive vehicle with tire-road friction coefficient identification

Because of the complexities of tire-road interaction,the wheels of a multi-wheel distributed electric drive vehicle can easily slip under certain working conditions.As wheel slip affects the dynamic per-formance and stability of the vehicle,it is crucial to control it and coordinate the driving force.With this aim,this paper presents a driving force coordination control strategy with road identification for eight-wheeled electric vehicles equipped with an in-wheel motor for each wheel.In the proposed control strategy,the road identification module estimates tire-road forces using an unscented Kalman filter al-gorithm and recognizes the road adhesion coefficient by employing the recursive least-square method.According to road identification,the optimal slip ratio under the current driving condition is obtained,and a controller based on sliding mode control with a conditional integrator uses this value for accel-eration slip regulation.The anti-slip controller obtains the adjusting torque,which is integrated with the driver-command-based feedforward control torque to implement driving force coordination control.The results of hardware-in-loop simulation show that this control strategy can accurately estimate tire-road forces as well as the friction coefficient,and thus,can effectively fulfill the purpose of driving force coordinated control under different driving conditions.     

A study on the surface overpressure distribution and formation of a double curvature liner under a two-point initiation

The formation mechanism of an EFP(explosively formed projectile) using a double curvature liner under the overpressure effect generated by a regular oblique reflection was investigated in this paper.Based on the detonation wave propagation theory,the change of the incident angle of the detonation wave collision at different positions and the distribution area of the overpressure on the surface of the liner were calculated.Three-dimensional numerical simulations of the formation process of the EFP with tail as well as the ability to penetrate 45# steel were performed using LS-DYNA software,and the EFP ve-locity,the penetration ability,and the forming were assessed via experiments and x-ray photographs.The experimental results coincides with those of the simulations.Results indicate that the collision of the detonation wave was controlled to be a regular oblique reflection acting on the liner by setting the di-mensions of the unit charge and maintaining the pressure at the collision point region at more than 2.4 times the CJ detonation when the incident angle approached the critical angle.The distance from the liner midline to the boundary of the area within which the pressure ratio of the regular oblique reflection pressure to the CJ detonation pressure was greater than 2.5,2,and 1.5was approximately 0.66 mm,1.32 mm,and 3.3 mm,respectively.It is noted that pressure gradient caused the liner to turn inside out in the middle to form the head of the EFP and close the two tails of the EFP at approximately 120μs.The penetration depth of the EFP into a 45# steel target exceeded 30 mm,and there was radial expansion between the head and tail of the EFE increasing the penetration resistance of the EFP.Therefore,the structural size of the unit charge and the liner can be further optimized to reduce resistance to increase the penetration ability of the EFP.