Investigating the surface integrity of aluminium based composites machined by EDM

In the present work, the surface characteristics of Electrical Discharge Machined (EDM) Al (6351)SiC and Al (6351)SiCB₄C composites are investigated. The composites are prepared by employing the conventional stir casting technique, as it can produce better particle dispersion in the matrix. The detailed experimental study is performed on the composites by varying current (I), duty factor (τ), pulse on time (T_on), and the gap voltage (V) in order to analyze the Heat Affected Zone (HAZ) formed in the sub surface and the average crater diameter formed on the machined surface of the composites as an output function. The formation of recast layers, presence of bubbles and the surface texture of the composites at various machining conditions are observed. The results show that the increased Metal Removal Rate (MRR) increases the depth of HAZ and the average crater diameter on the machined area. Further, the addition of B₄C particles to the composite produces more surface defect than the AlSiC composite.     

The surface activation of boron to improve ignition and combustion characteristic

Boron is a very promising and highly attractive fuel because of high calorific value. However, the practical applications in explosives and propellants of boron have been limited by long ignition delay time and low combustion efficiency. Herein, nano-Al and graphene fluoride (GF) as surface activated materials are employed to coat boron (B) particles to improve ignition and combustion performance. The reaction heat of nano-Al coated B/KNO₃ and GF coated B/KNO₃ are 1116.83 J/g and 862.69 J/g, respectively, which are higher than that of pure B/KNO₃ (823.39 J/g). The ignition delay time of B/KNO₃ could be reduced through nano-Al coating. The shortest ignition delay time is only 75 ms for B coated with nano-Al of 8 wt%, which is much shorter than that of pure B/KNO₃ (109 ms). However, the ignition delay time of B/KNO₃ coated with GF has been increased from 109 to 187 ms. B coated with GF and nano-Al shown significantly influence on the pressure output and flame structure of B/KNO₃. Furthermore, the effects of B/O ratios on the pressure output and ignition delay time have been further fully studied. For B/KNO₃ coated with nano-Al and GF, the highest pressures are 88 KPa and 59 KPa for B/O ratio of 4:6, and the minimum ignition delay time are 94 ms and 148 ms for B/O ratio of 7:3. Based on the above results, the reaction process of boron coated with GF and nano-Al has been proposed to understand combustion mechanism.     

地空导弹与弹道导弹的技术融合正在促使这两类导弹产生突破性的发展

地空导弹采用弹道导弹的抛物弹道技术 ,能够实现应用固体推进剂达到低质量远射程的目标。弹道导弹采用地空导弹末段弹道的寻的制导控制技术 ,可以达到降速、增程并实现末段有效制导控制和弹道机动的目标 ,从而大幅度提高命中精度和突防概率。地空导弹和弹道导弹之间的技术融合 ,已经开始并将很快形成这两类导弹的新一轮突破性的发展     

Preparation and characterization of HMX/NH2-GO composite with enhanced thermal safety and desensitization

To improve the safety of HMX, HMX/NH₂-GO composite was prepared with aqueous ammonia functionalized graphene oxide (NH₂-GO). The composite was characterized by SEM, Zeta potential, XPS, Raman spectrum, XRD, HPLC, DSC and BAM sensitivity test. The results indicated that the functionalization with aqueous ammonia can enhance the interaction between GO and HMX, and more efficiently desensitize the explosive. The optimal impact sensitivity of the HMX/NH₂-GO composite can be not less than 40 J, which is also the most insensitivity compared to the previous reports prepared by coating desensitization with non-energetic desensitized material. Moreover, the potential reason for the different impact and friction sensitivity was also discussed, which may bring a novel perspective to achieve the desensitization of energetic material.     

Influence of Al2O3 particles on the microstructure and mechanical properties of copper surface composites fabricated by friction stir processing

The influence of three factors, such as volume percentage of reinforcement particles (i.e. Al₂O₃), tool tilt angle and concave angle of shoulder, on the mechanical properties of Cu–Al₂O₃ surface composites fabricated via friction stir processing was studied. Taguchi method was used to optimize these factors for maximizing the mechanical properties of surface composites. The fabricated surface composites were examined by optical microscope for dispersion of reinforcement particles. It was found that Al₂O₃ particles are uniformly dispersed in the stir zone. The tensile properties of the surface composites increased with the increase in the volume percentage of the Al₂O₃ reinforcement particles. This is due to the addition of the reinforcement particles which increases the temperature of recrystallization by pinning the grain boundaries of the copper matrix and blocking the movement of the dislocations. The observed mechanical properties are correlated with microstructure and fracture features.     

考虑浮绳联结的双无人船艇系统协同控制策略研究

针对青岛等海域浒苔泛滥成灾的问题,开展了由浮绳柔性连接两艘水面无人船艇构成的双无人船艇系统协同控制策略研究,通过双无人船艇系统清扫浒苔,并将其拖运至海岸.考虑系统中的无人船艇动力、浮绳力矩和水流产生的干扰力矩,建立了欠驱动无人船艇三自由度动力学模型,提出了基于距离的包含编队和跟踪两个模式的协同控制策略.双无人船艇系统作...     

采用固液冲压发动机的地空导弹弹道建模

针对采用固液混合冲压发动机的地空导弹弹道设计中出现的新问题, 给出了解决这些问题的弹道设计方法, 并利用弹道仿真对其进行了验证。     

浅谈舰载燃料空气炸药武器抗击巡航导弹

通过对FAE武器的特种杀伤效果和对巡航导弹相关技战术性能分析,利用FAE武器(云爆弹)的爆轰、冲击波、破片、窒息和电磁电热效应等特种杀伤效果,剧烈改变导弹的工作环境和对巡航导弹的弹体、导引系统、控制系统和发动机等关键部件进行“软”、“硬”破坏,以期达到抗击巡航导弹的目的,同时阐述了装备水面舰艇的可行性。     

世界防空导弹市场发展分析

以世界防空导弹型号为研究对象,概述了世界防空导弹市场的总体发展现状,分别对便携式防空导弹、中低空中近程防空导弹和中高空中远程防空导弹市场现状进行了分析。预测了未来１０年世界防空导弹市场的发展趋势。     

地空导弹阵地伪装及效果评价

分析了某型地空导弹武器阵地的暴露特征,根据伪装学的原理,针对这些特征采取了相应的伪装措施,并根据观测试验数据,对该型地空导弹武器阵地伪装前后的光学、热红外及雷达伪装效果进行了定量评价分析。结果表明,在伪装前完全暴露的阵地,伪装后目标的暴露特征大大减小,伪装效果非常明显。