火药复合焊条焊接接头的微观组织及性能

为提高战场装备的应急抢修能力,以火药和2Al/3CuO系高热剂为焊接热源,开发了一种新型的便携式焊接材料——火药复合焊条,对其焊缝的组织形貌及性能进行研究.试验结果表明,火药复合焊条的焊接属于熔化焊,焊缝与基体之间存在明显的过渡区,焊缝成形良好,焊缝的抗拉强度大于400MPa,高于母材本身强度,能够满足战场应急抢修能力的需要.     

球磨时间对纳米SiO_2/Cu复合材料摩擦学性能的影响

采用球磨法与热压烧结工艺制备了添加w（n-SiO2）=1.0%的铜基纳米复合材料。通过球盘式摩擦磨损试验机测试了复合材料的摩擦磨损性能,采用排水法和场发射扫描电镜（FSEM）研究了复合材料的致密度、显微组织和磨损形貌。结果表明：球磨可提高复合材料的致密度,改善n-SiO2在铜基体中的分散均匀性;随球磨时间的增加,复合材料的动摩擦因数和磨损量先减小后增加,球磨10 h复合材料具有较低的摩擦因数和磨损量,磨损机理主要为磨料磨损。     

陶瓷基复合装甲防12.7mm穿甲燃烧弹的靶试研究（Ⅱ）

基于对材料特性和防弹机理的认识,设计了由（SiC＋Si）陶瓷、616装甲钢和高强PE材料构成的陶瓷基复合靶板,靶板防护面密度为118 kg/m2,尺寸为500 mm×500 mm×25 mm。利用现役12.7 mm穿甲燃烧弹考核靶板在6发弹打击下的防护能力,检验靶板设计思路。结果表明：靶板结构是可行的,可防住V25为818 m/s的现役12.7 mm穿甲燃烧弹。     

Bending and stress analysis of polymeric composite plates reinforced with functionally graded graphene platelets based on sinusoidal shear-deformation plate theory

The bending and stress analysis of a functionally graded polymer composite plate reinforced with gra-phene platelets are studied in this paper. The governing equations are derived by using principle of virtual work for a plate which is rested on Pasternak's foundation. Sinusoidal shear deformation theory is used to describe displacementfield. Four different distribution patterns are employed in our analysis. The analytical solution is presented for a functionally graded plate to investigate the influence of important parameters. The numerical results are presented to show the deflection and stress results of the problem for four employed patterns in terms of geometric parameters such as number of layers, weight fraction and two parameters of Pasternak's foundation.     

复合材料层合板疲劳寿命形状参数与门槛值分析方法

复合材料性能具有较大的分散性,在表征复合材料疲劳寿命时,必须考虑分散性的影响。以M21C复合材料开孔层合板为研究对象,采用Sendeckyj等效静强度模型和随机变量函数的概率分布方法推导了复合材料层合板疲劳寿命形状参数和剩余强度形状参数的关系,通过试验和统计的方法获得了M21C复合材料开孔层合板的疲劳寿命形状参数和疲劳门槛值,对载荷放大系数以及低载截除水平的确定提供了数据支持。     

A comprehensive review on material selection for polymer matrix composites subjected to impact load

Polymer matrix composites (PMC) are extensively been used in many engineering applications. Various natural fibers have emerged as potential replacements to synthetic fibers as reinforcing materials composites owing to their fairly better mechanical properties, low cost, environment friendliness and biodegradability. Selection of appropriate constituents of composites for a particular application is a tedious task for a designer/engineer. Impact loading has emerged as the serious threat for the composites used in structural or secondary structural application and demands the usage of appropriate fiber and matrix combination to enhance the energy absorption and mitigate the failure. The objective of the present review is to explore the composite with various fiber and matrix combination used for impact applications, identify the gap in the literature and suggest the potential naturally available fiber and matrix combination of composites for future work in the field of impact loading. The novelty of the present study lies in exploring the combination of naturally available fiber and matrix combination which can help in better energy absorption and mitigate the failure when subjected to impact loading. In addition, the application of multi attributes decision making (MADM) tools is demonstrated for selection of fiber and matrix materials which can serve as a benchmark study for the researchers in future.     

基于ANSYS的大型复合材料风力机叶片结构分析

基于ANSYS软件,对某款应用于GL3A风场的1500kW大型复合材料风力机叶片进行了结构分析。分析结果表明:该叶片的振型以一阶挥舞和一阶摆振为主,其频率分别为0.86Hz和1.59Hz;在极限挥舞载荷作用下,该叶片有限元模型计算得到的叶尖挠度为8.445m,而该叶片全尺寸静力试验得到的极限挥舞载荷作用下的叶尖挠度为8.12m,计算值与试验值的误差只有3.8%;另外,该叶片的最大计算拉应力和压应力分别为228MPa和201MPa,而该叶片玻纤/环氧复合材料实测拉伸强度和实测压缩失稳强度分别为720MPa和380MPa,其计算最大应力只有对应实测极限强度的31.7%和52.9%。     

边界条件对复合材料层合板准静态压痕损伤的影响

在实际的服役过程中,飞机用复合材料层合板通过四边铆接的方式与飞机金属框架进行连接,其受力时的边界条件为四边固支。以实际应用背景为基础,分别从分层损伤扩展模式、接触力、凹坑深度、损伤宽度四个方面系统地比较了四边固支和四边简支两种边界条件下,复合材料层合板准静态压痕损伤的区别。结果表明以上四种变量在两种边界条件下均存在明显差异,可为基于实际应用的复合材料准静态压痕损伤研究提供实验依据。     

氧化铝气凝胶复合材料的制备与隔热性能

以仲丁醇铝为先驱体,采用溶胶一凝胶工艺制备氧化铝溶胶,并将其与无机陶瓷纤维毡复合经超临界流体干燥得到氧化铝气凝胶隔热复合材料.利用扫描电子显微镜(SEM)和氮气吸附等方法对样品微观结构进行分析,利用热平板法对材料的隔热性能进行测试,并分析了氧化铝气凝胶隔热复合材料隔热机理.研究表明:与氧化硅气凝胶相比,氧化铝气凝胶具有更好的耐高温性能,经1000℃热处理后仍然能够较好地保持其纳米多孔结构;将气凝胶与纤维复合后,充分发挥了氧化铝气凝胶优良的隔热特性,使得复合材料的隔热性能较纯纤维毡有了明显的改善,其热面温度1000℃时导热系数为0.0685 W/m·K.     

高重频双波长复合干扰激光器设计

为解决基频光高重频与倍频光高平均功率之间的矛盾,设计了一台干扰用高重频双波长复合输出激光器。静态仿真了泵浦源效率、激光晶体受热和受力分布、激光高斯模式特征,得到了该激光器的复合输出特性。动态仿真调Q频率、倍频晶体长度对复合输出的影响以及分析倍频晶体热效应,发现在泵浦功率和谐振腔结构不变的前提下,需先满足基频光高重频工作,再优化倍频晶体长度和控制倍频晶体温度可提高倍频光的输出功率。按上述仿真结论开展的验证实验结果表明:当磷酸氧钛钾晶体长度为12 mm、输出镜透过率为10%、重复频率为50 k Hz时,设计的激光器基频光平均功率为18. 98 W,倍频光平均功率为2. 22 W,与仿真结论一致。