军队科研机构推进国防知识产权转化运用

军队科研机构作为国家科技创新体系的重要组成部分,承担了大量科技创新任务,产生了许多具有自主知识产权的高水平科技成果,推动军队科研机构国防知识产权转化运用,是贯彻军民融合发展战略的必要途径。分析了军队科研机构国防知识产权转化的现状及制约转化的现实障碍,并结合实际探讨了推进军队科研机构国防知识产权转化的建议举措。     

铝合金-纯铝-钢复合板爆炸焊接试验及性能研究

通过设计爆炸焊接试验复合了铝合金-纯铝-钢爆炸复合板,对其界面形态、显微硬度及力学性能进行了研究。结果表明,铝合金-纯铝界面纯规则正弦波形,纯铝-钢复合板界面波形较小,铝合金-纯铝-钢复合板的界面剪切强度在75 MPa以上,爆炸复合过程中,纯铝与钢界面生成了金属间化合物,其界面处基体金属发生强烈的塑性变形。复合板变形及组织变化的结果造成复合板界面处的显微硬度最高,随着距界面距离的增加,两侧基体金属的硬度逐渐降低。     

Modeling and realization of real time electronic countermeasure simulation system based on SystemVue

In this paper, we proposed a new design scheme of real time electronic countermeasure simulation system. This paper mainly expounds the modeling and realization methods of each part of the whole simulation system, and the real-time property of system has been lucubrated. Electronic countermeasure simulation system is the key part of military training of individuals; it can also allow the realistic evaluation of the performance of modern equipments and techniques. As a proof, we have drawn up a series of simulation scenarios, such as radar electronic reconnaissance simulation scenario, to explain the feasibility and the superiority of our modeling scheme in this paper.     

激光制备高附着性能的铜基类金刚石膜

提升类金刚石(Diamond-Like Carbon, DLC)膜在被保护基底上的附着能力具有明显的实际应用价值。从微观机理上分析了前期设计的Cu基多层DLC膜有效性的原因。在此基础上,研究了DLC/SiC循环层中两者厚度比例对膜层的附着性能、纳米硬度和耐磨性的影响,以优化结构、进一步提升实际应用所需的膜层性能。纳米划痕和压痕测试结果表明:随着DLC层与SiC层厚度比例的增大,多层DLC膜在Cu基上附着性能逐渐降低,但当厚度比小于2.3时,仍接近厚度400 nm的单层DLC膜在Si基上的附着性能；Cu基多层DLC膜的纳米硬度逐渐提高,同时,耐磨性接近纯DLC膜。     

国防知识产权运营市场化研究

提高国防知识产权转化应用水平,关键是解决制约国防知识产权转化应用的体制机制问题。可借鉴普通知识产权运营经验,以市场化方式促进国防知识产权运营工作。针对当前运营中出现的市场失灵现象,从创新政府治理模式、引入市场机制、增强法律法规建设、搭建公共服务平台等途径入手,逐步理顺政府与市场的关系,进行国防知识产权运营市场化改革。     

Effect of tool rotational speed on the particle distribution in friction stir welding of AA6092/17.5 SiCp-T6 composite plates and its consequences on the mechanical property of the joint

This study investigates the effect of tool rotational speed (TRS) on particle distribution in nugget zone (NZ) through quantitative approach and its consequences on the mechanical property of friction stir welded joints of AA6092/17.5 SiC_p-T6 composite. 6 mm thick plates are welded at a constant tool tilt angle of 2° and tool traverse speed of 1 mm/s by varying the TRS at 1000 rpm, 1500 rpm and 2000 rpm with a taper pin profiled tool. Microstructure analysis shows large quantity of uniformly shaped smaller size SiC particle with lower average particle area which are homogeneously distributed in the NZ. The fragmentation of bigger size particles has been observed because of abrading action of the hard tool and resulting shearing effect and severe stress generation due to the rotation of tool. The particles occupy maximum area in the matrix compared to that of the base material (BM) due to the redistribution of broken particles as an effect of TRS. The migration of particles towards the TMAZ-NZ transition zone has been also encountered at higher TRS (2000 rpm). The microhardness analysis depicts variation in average hardness from top to bottom of the NZ, minimum for 1500 rpm and maximum for 2000 rpm. The impact strength at 1000 rpm and 1500 rpm remains close to that of BM (21.6 J) while 2000 rpm shows the accountable reduction. The maximum joint efficiency has been achieved at 1500 rpm (84%) and minimum at 1000 rpm (68%) under tensile loading. Fractographic analysis shows mixed mode of failure for BM, 1000 rpm and 1500 rpm, whereas 2000 rpm shows the brittle mode of failure.     

Effect of transverse compression on the residual tensile strength of ultrahigh molecular weight polyethylene (Dyneema® SK-76) yarns

Ballistic impact induces complex stress states on fiber-based armor systems. During impact fibers undergo multiaxial loading which includes axial tension, axial compression, transverse compression, and transverse shear. Transverse compression induced by the projectile leads to permanent deformation and fibrillation of fibers resulting in degradation of material tensile strength. Previous work (Sockalingam et al. Textile Res. J 2018) has shown a reduction of 20% in the tensile strength of Dyneema® SK76 single fibers subjected to 77% nominal transverse compressive strains. Experimental investigation of quasi-static transverse compression on Dyneema® SK-76 yarns, unconstrained in the lateral direction, indicate an average of 4% reduction in tensile strength of yarns compressed to 77% nominal strains. In this work we use finite element modeling techniques to understand the difference in residual tensile strength between single fibers and yarns observed in laterally unconstrained transverse compression experiments. Finite element study of the transverse compression response of single fibers and yarns indicate that local strains developed in fibers within the yarn are much lower than the local strains developed in single fibers subjected to a given nominal strain and may explain the less reduction in strength observed in yarns.