点阵结构空气舵及内部流体热流固耦合研究

开展了钛合金TC4材料激光粉末床熔融(LPBF)工艺研究,在此基础上设计了多孔轻质空气舵模型,并基于有限差分法(FDM),采用三维流固耦合共轭传热数值计算方法,利用流体体积法(VOF)追踪流体自由液面,研究了典型的点阵夹层结构的空气舵内部冷却液动态换热过程的相互影响过程,考虑了冷却液与钛合金材料蒙皮间的耦合传热及湍流换热。结果表明,空气舵的内部流体压强随速度的增加而增加,从而导致流体出口的速度增加。当压强增加到一定程度时,流体的出口以水柱形式喷出。虽然较大的流体速度可以带走较多的热量,但是影响远小于对压强的影响。综合考虑空气舵的服役要求,获得了合适的冷却水入口速度。     

战术导弹中小型固体发动机技术的发展

通过对战术导弹中小型固体发动机具体发展需求的分析,明确了高能化、轻质化、可控化和低易损4个主要的中小型固体发动机发展方向。可以从提高推进剂黏合剂密度和燃烧室工作压强来实现高能化;采用轻质高性能金属壳体、纤维缠绕复合材料壳体以及提高绝热层性能以实现轻质化;可控化需要在高功率密度的驱动装置、高精度的控制算法等方面获得突破和支撑;低易损则可以从钝感推进剂、主动扩稳、防护材料等途径开展工作。通过对这4个技术方向上国内外研究现状和发展趋势进行梳理,明确提出未来研究需要突破推进剂和热防护原材料、新型装药工艺、可调燃气阀门、压力闭环控制和有效扩稳等关键技术,加速工程化进程,为我国战术导弹的跨越式发展提供支撑。     

冲击温度的理论计算及分析

当空间飞行器受到碎片的碰撞时,其壳体中会产生冲击加热。文章概述了计算冲击温度的三种基本方法;计算了铁的冲击加热温度,并与实验测量值作了比较。结果表明,利用三项式物态方程计算的冲击温度与测量值符合得比较好。另外,还对影响冲击温度计算值的若干因素进行了分析     

协同空战与多智能体强化学习下的关键问题

自从协同作战的概念提出后,各军事强国在协同空战领域均取得了重大进展,协同成为提升作战能力的倍增器。近数十年来,作为解决序列问题的现代智能方法,强化学习在各领域高速发展。然而,面对高维变量问题时,传统的单智能体强化学习往往表现不佳,多智能体强化学习算法为解决复杂多维问题提出新的可能。通过对多智能体强化学习算法原理、训练范式与协同空战的适应性进行分析,提出了协同空战与多智能体强化学习的未来发展方向,为更好地把多智能体强化学习应用于协同空战提供思路。     

集团化实验室信息管理系统中台建设实践

中台通过重新构建企业级的服务能力,消除企业内部各业务部门、各分子公司间的壁垒,可更好的适应企业发展。描述了当前中台发展现状,结合集团化计量检测机构特点,提出了实验室信息管理系统中台的一种划分方法,为集团化实验室信息管理系统建设提供一种解决方案。实现企业业务、资源、财务的综合管理,提升企业管理能力。     

捷联惯导系统动基座对准的可观测性分析

建立了SINS(捷联惯导系统)动基座对准的误差模型,首次应用PWCS(分段定常系统)可观测性分析理论对SINS动基座对准过程中的可观测性进行了全面研究.将载体的运动分解为平动和姿态变化两大类情形,深入研究和详细分析了载体的各种运动对系统可观测性的影响,指出在SINS动基座对准过程,无论载体的线运动还是角运动在一定条件下都能提高SINS的可观测性.定性地得出了不同运动对系统可观测性的影响结果,这为研究SINS的快速精确对准方法奠定了理论基础.      

基于GRNN网络和遗传算法的旋翼动平衡调整

针对传统旋翼调整方法没有考虑调整参数与振动信号之间的非线性关系,提出一种结合广义回归神经网络GRNN(General Regression Neural Network)和遗传算法的旋翼调整方法,采用GRNN建立旋翼动平衡调整模型,以桨叶调整参数作为GRNN输入,以旋翼转轴3个方向的加速度测量值和机身3个方向加速度测量值作为网络输出,建立调整参数与直升机振动信号之间的模型.以直升机振动作为目标函数,采用改进的遗传算法对桨叶调整参数进行寻优,获得直升机振动最小时的桨叶的调整量.飞行实验表明,通过1到2次飞行调整,可使3个方向机身振动(旋翼的一阶振动)为最小,完成旋翼的动平衡调整.      

Coronal mass ejection detection using wavelets,curvelets and ridgelets: Applications for space weather monitoring

Coronal mass ejections (CMEs) are large-scale eruptions of plasma and magnetic field that can produce adverse space weather at Earth and other locations in the Heliosphere. Due to the intrinsic multiscale nature of features in coronagraph images, wavelet and multiscale image processing techniques are well suited to enhancing the visibility of CMEs and suppressing noise. However, wavelets are better suited to identifying point-like features, such as noise or background stars, than to enhancing the visibility of the curved form of a typical CME front. Higher order multiscale techniques, such as ridgelets and curvelets, were therefore explored to characterise the morphology (width, curvature) and kinematics (position, velocity, acceleration) of CMEs. Curvelets in particular were found to be well suited to characterising CME properties in a self-consistent manner. Curvelets are thus likely to be of benefit to autonomous monitoring of CME properties for space weather applications.     

凝聚式过滤器的开发与设计

着重介绍了凝聚式过滤器的开发、设计及与空气压缩机厂原有产品在性能上是有区别的。新的凝聚式过滤器实现了对压缩空气进行切向进气，用丝网除沫器和精滤芯等代替原有的陶瓷管堆积过滤和毛毡缠绕过滤法。在过滤精度，气流均匀性阻力特性等性能上有一定优势，且成本低、数命长，经济实用。     

What Determines the Composition of SEPs in Gradual Events?

Gradual solar energetic particle (SEP) events are evidently accelerated by coronal/interplanetary shocks driven by coronal mass ejections. This talk addresses the different factors which determine the composition of the accelerated ions. The first factor is the set of available seed populations including the solar wind core and suprathermal tail, remnant impulsive events from preceding solar flares, and remnant gradual events. The second factor is the fractionation of the seed ions by the injection process, that is, what fraction of the ions are extracted by the shock to participate in diffusive shock acceleration. Injection is a controversial topic since it depends on the detailed electromagnetic structure of the shock transition and the transport of ions in these structured fields, both of which are not well understood or determined theoretically. The third factor is fractionation during the acceleration process, due to the dependence of ion transport in the turbulent electromagnetic fields adjacent to the shock on the mass/charge ratio. Of crucial importance in the last two factors is the magnetic obliquity of the shock. The form of the proton-excited hydromagnetic wave spectrum is also important. Finally, more subtle effects on ion composition arise from the superposition of ion contributions over the time history of the shock along the observer’s magnetic flux tube, and the sequence of flux tubes sampled by the observer.