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11.
采用自动化高速电弧喷涂技术在镁合金基体上制备了FeCrBSiMoNbW非晶纳米晶涂层。采用Flir A20M型红外热像仪对Fe基非晶纳米晶喷涂层的表面温度场进行了实时监测。对Fe基非晶纳米晶涂层和传统的3Cr13涂层的组织结构、力学性能以及摩擦学性能进行了对比分析。实验结果表明:Fe基非晶纳米晶涂层组织致密,孔隙率低,具有相对较高的硬度和拉伸结合强度;形成了非晶相和纳米晶相组成的复合结构,使得涂层具备较好的耐磨减摩性能。  相似文献   
12.
In order to understand the mechanism of conoidal fracture damage caused by a high-speed fragment-simulating projectile in titanium alloy layer of a composite armor plate composed of titanium- and aluminum-alloy layers, the ballistic interaction process was successfully simulated based on the Tuler-Butcher and GISSMO coupling failure model. The simulated conoidal fracture morphology was in good agreement with the three-dimensional industrial-computed-tomography image. Further, three main damage zones (zones I, II, and III) were identified besides the crater area, which are located respectively near the crater area, at the back of the target plate, and directly below the crater area. Under the high-speed-impact conditions, in zone II, cracks began to form at the end of the period of crack formation in zone I, but crack formation in zone III started before the end of crack formation in zone II. Further, the damage mechanism differed for different stress states. The microcracks in zone I were formed both by void connection and shear deformation. In the formation of zone I, the stress triaxiality ranged from-2.0 to-1.0, and the shear failure mechanism played a dominant role. The microcracks in zone II showed the combined features of shear deformation and void connection, and during the for-mation process, the stress triaxiality was between 0 and 0.5 with a mixed failure mode. Further, the microcracks in zone III showed obvious characteristics of void connection caused by local melting. During the zone III formation, the triaxiality was 1.0-1.9, and the ductile fracture mechanism was dominant, which also reflects the phenomenon of spallation.  相似文献   
13.
Due to its high strength, high density, high hardness and good penetration capabilities, Depleted ura-nium alloys have already shined in armor-piercing projectiles. There should also be a lot of room for improvement in the application of fragment killing elements. Therefore, regarding the performance of the depleted uranium alloy to penetrate the target plate, further investigation is needed to analyze its advantages and disadvantages compared to tungsten alloy. To study the difference in penetration per-formance between depleted uranium alloy and tungsten alloy fragments,firstly, a theoretical analysis of the adiabatic shear sensitivity of DU and tungsten alloys was given from the perspective of material constitutive model. Then, taking the cylindrical fragment penetration target as the research object, the penetration process and velocity characteristics of the steel target plates penetrated by DU alloy frag-ment and tungsten alloy fragment were compared and analyzed, by using finite element software ANSYS/LS-DYNA and Lagrange algorithm. Lastly, the influence of different postures when impacting target and different fragment shapes on the penetration results is carried out in the research. The results show that in the penetration process of the DU and tungsten alloy fragments, the self-sharpening properties of the DU alloy can make the fragment head sharper and the penetrating ability enhance. Under the same conditions, the penetration capability of cylindrical fragment impacting target in vertical posture is better than that in horizontal posture, and the penetration capability of the spherical fragment is slightly better than that of cylindrical fragment.  相似文献   
14.
改善Al对B4C润湿性的研究   总被引:1,自引:0,他引:1  
依据金属Al的特性及其与B4C相互作用的关系,在理论上分析Al对B4C的润湿性,分析理论润湿性与实际润湿性差异的原因,在此基础上,通过实验寻求改善Al对B4C润湿性的方法和工艺,发现升高温度可以改善润湿性,温度由1 050℃升至1 100℃时,润湿角θ由52°降至23°;在Al中添加小量Mg后,真空1×10-3Pa,温度1 100℃×3 h时Al对B4C润湿角由原来的23°降至9°.  相似文献   
15.
基于随机Petri网的综合航电系统建模及分析   总被引:2,自引:0,他引:2  
提出了一种利用随机Petri网对综合航电系统进行建模和性能分析的方法.首先,建立了综合航电系统数据总线传输系统的随机Petri网系统模型,通过系统模型进行综合航电系统的性能分析;其次,给出了航空电子综合系统数据总线传输基于固定主控端周期指令的总线性能分析结果;最后,通过两种分析结果的比较,得出了基于随机Petri网对航空电子综合系统数据总线传输建模分析是可行的结论.  相似文献   
16.
航空电子总线测试系统的设计与实现   总被引:4,自引:0,他引:4  
现代航空电子综合化系统通常建立在M IL-STD-1533B多路传输数据总线通信网络基础之上,总线控制器(BC)和各个远程终端(RT)必须满足M IL-STD-1553B规定的各项协议指标要求,才能正确地联网通讯。讨论了某型航空电子总线测试系统的设计与实现,主要探讨了此系统的软、硬件开发,系统组成及其BC和RT有效性测试的主要内容和要求。在实际应用中收到了很好的效果。  相似文献   
17.
《防务技术》2019,15(3):353-362
AA5059 is one of the high strength armor grade aluminium alloy that finds its applications in the military vehicles due to the higher resistance against the armor piercing (AP) threats. This study aimed at finding the best suitable process among the fusion welding processes such as gas tungsten arc welding (GTAW) and gas metal arc welding (GMAW) by evaluating the tensile properties of AA5059 aluminium alloy joints. The fracture path was identified by mapping the low hardness distribution profile (LHDP) across the weld cross section under tensile loading. Optical and scanning electron microscopies were used to characterize the microstructural features of the welded joints at various zones. It is evident from the results that GTAW joints showed superior tensile properties compared to GMAW joints and this is primarily owing to the presence of finer grains in the weld metal zone (WMZ) and narrow heat-affected zone (HAZ). The lower heat input associated with the GTAW process effectively reduced the size of the WMZ and HAZ compared to GMAW process. Lower heat input of GTAW process results in faster cooling rate which hinders the grain growth and reduces the evaporation of magnesium in weld metal compared to GMAW joints. The fracture surface of GTAW joint consists of more dimples than GMAW joints which is an indication that the GTAW joint possess improved ductility than GMAW joint.  相似文献   
18.
本文对美军E-10飞机的项目背景、主要组成、性能参数以及其发展历程进行了梳理和分析,提出了网络中心战思想下关于装备发展和研制的几点思考,以期对我军装备研制和建设提供参考。  相似文献   
19.
概述了热塑性互穿聚合物网络(TIPN)的研究进展及其结构特点、制各方法和熔体的流动性,并对TIPN的前景作了简要的分析。  相似文献   
20.
基于B/S模式的雷达装备远程故障诊断系统   总被引:1,自引:0,他引:1  
探讨了基于B/S模式的雷达装备远程故障诊断系统,利用知识库、Web等技术构建了一个供雷达部队使用的雷达诊断网,对系统的体系结构和功能模块以及所涉及的关键技术进行了分析和研究,实现了雷达装备的实时监控和故障的自动诊断,提高了雷达装备的可靠性和雷达部队的应急抢修能力。  相似文献   
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