首页/文章/ 详情

【新文速递】2023年10月27日复合材料SCI期刊最新文章

18天前浏览280

今日更新:Composites Part A: Applied Science and Manufacturing 1 篇,Composites Part B: Engineering 1 篇

Composites Part A: Applied Science and Manufacturing

A new test for characterization of interlaminar tensile strength of tape-laminate composites

Fisher John, Czabaj Michael W.

doi:10.1016/j.compositesa.2023.107868

表征胶带层压复合材料层间拉伸强度的新试验

Interlaminar tensile strength (ZT) is an important property of polymer matrix composites used for material screening, failure analysis, and design. Current methods for determining ZT suffer from drawbacks that prevent an unambiguous measurement of this property. This study proposes a new flexure-based specimen, previously used to measure intralaminar tensile strength (YT), which allows for a straightforward characterization of ZT. The proposed test is used to measure both ZT and YT of two microstructurally distinct carbon/epoxy systems. Overall, the experimental data demonstrates that the new test provides a reliable measure of ZT that is independent of the specimen manufacturing method. Importantly, a direct comparison between ZT and YT demonstrates that ZT tends to be lower than YT . Although no direct links between lower values of ZT and the specimen microstructure are discovered, this effect is likely influenced by the presence and location of resin-rich regions relative to the tensile stresses.

层间拉伸强度(ZT)是聚合物基复合材料的一项重要性能,用于材料筛选、失效分析和设计。目前测定 ZT 的方法存在一些缺陷,无法对该特性进行明确测量。本研究提出了一种新的基于挠曲的试样,这种试样以前用于测量层内拉伸强度(YT),可直接表征 ZT .所提议的测试可用于测量 ZT  和 YT 的 ZT 和 YT。总之,实验数据表明,新测试可提供可靠的 ZT 测量值,且不受试样制造方法的影响。 与试样制造方法无关。重要的是,直接比较 ZT 和 YT 之间的直接比较表明,ZT 往往低于 YT .虽然没有发现较低的 ZT 值与试样的微观结构有直接联系,但这种影响很可能受到树脂的存在和位置的影响。和试样微观结构之间没有直接联系,但这种影响很可能受到相对于拉伸应力的富树脂区域的存在和位置的影响。


Composites Part B: Engineering

Fabrication of TiB whiskers reinforced Ti6242 matrix composites by direct laser deposition: Powder preparation, microstructure and mechanical property

Li Lian, Ma Panpan, Zhang Ling, Tan Hua, Li Miaoquan

doi:10.1016/j.compositesb.2023.111068

用激光直接沉积法制造 TiB 晶须增强 Ti6242 基复合材料:粉末制备、微观结构和机械性能

Direct laser deposition (DLD) technique has great potential in manufacturing titanium matrix composites (TMCs) components with complicated shape. The TiB whiskers reinforced Ti6242 matrix composites were fabricated from the premixed TiB2/Ti6242 powders via DLD technique. Quantitative characterization of the extent of mixing uniformity and the deformation rate of the ball milled TiB2/Ti6242 powders was performed so as to select the optimal ball milling parameters. The TiB2/Ti6242 powders with two different weight fractions of TiB2 (2 wt%TiB2/Ti6242 and 5 wt%TiB2/Ti6242) were used to obtain different distributions of TiB whiskers in the composites due to the change in the solidification path in DLD process. The TiB whiskers in the TMCs-Ⅰ obtained from the 2 wt%TiB2/Ti6242 powders exhibited a discontinuous network structure following solidification in hypoeutectic zone, while the TiB whiskers were randomly distributed in the TMCs-Ⅱ obtained from the 5 wt%TiB2/Ti6242 powders due to the solidification in hypereutectic zone. In comparison with the DLDed Ti6242, the α colonies and β grains of the TMCs-Ⅰ and TMCs-Ⅱ were significantly refined. In addition, both equiaxed and lamellar α phase were formed in the TMCs-Ⅱ, in which various orientation relationships (ORs) between TiB and α phase occurred and the presence or absence of OR between TiB and β phase was responsible for the different morphologies of α phase. The yield strength of the DLDed TMCs-Ⅰ and TMCs-Ⅱ increased by 10.7 % and 38.8 % in comparison with that of the DLDed Ti6242, and both the load-bearing strengthening and fine-grain strengthening effects effectively enhanced the strength of the composites.

直接激光沉积(DLD)技术在制造形状复杂的钛基复合材料(TMC)部件方面具有巨大潜力。通过 DLD 技术,用预混合的 TiB2/Ti6242 粉末制造出了 TiB 晶须增强的 Ti6242 基复合材料。对混合均匀度和球磨 TiB2/Ti6242 粉末的变形率进行了定量表征,以选择最佳球磨参数。使用两种不同重量分数的 TiB2/Ti6242 粉末(2 wt%TiB2/Ti6242 和 5 wt%TiB2/Ti6242),以获得由于 DLD 过程中凝固路径的变化而导致复合材料中 TiB 晶须的不同分布。由 2 wt%TiB2/Ti6242 粉末制得的 TMCs-Ⅰ 中的 TiB 晶须在低共晶区凝固后呈现出不连续的网络结构,而由 5 wt%TiB2/Ti6242 粉末制得的 TMCs-Ⅱ 中的 TiB 晶须则由于在高共晶区凝固而随机分布。与 DLDed Ti6242 相比,TMCs-Ⅰ 和 TMCs-Ⅱ 的 α 晶粒和 β 晶粒明显细化。此外,TMCs-Ⅱ中还形成了等轴和片状α相,其中TiB和α相之间存在各种取向关系(OR),TiB和β相之间是否存在OR是造成α相形态不同的原因。与 DLDed Ti6242 相比,DLDed TMCs-Ⅰ 和 TMCs-Ⅱ 的屈服强度分别提高了 10.7% 和 38.8%,承载增强效应和细晶粒增强效应都有效地提高了复合材料的强度。



来源:复合材料力学仿真Composites FEM
ACTMechanicalSystemDeform复合材料UG材料试验
著作权归作者所有,欢迎分享,未经许可,不得转载
首次发布时间:2024-11-03
最近编辑:18天前
Tansu
签名征集中
获赞 3粉丝 0文章 690课程 0
点赞
收藏
作者推荐

Abaqus 中粘弹性材料 Prony series 模型的参数输入 - Part 1

本文简述了粘弹性材料的 Prony seires 模型,以及其在 Abaqus 中输入的方式及要点。Prony series 模型Prony series 是工程中较常使用的线性粘弹性材料本构模型,其松弛(Relaxation) 形式可以表达为 其中 为松弛时间, 为对应的松弛模量, 表示平衡模量。Prony series 模型等价于 Generalized Maxwell 模型,即 其中 。因此,常用的 Maxwell 模型 可以看作只有一项的 Prony series 方程。Abaqus 中的 Prony series 参数在方程(1)中,我们注意到 时, 。引入 ,方程(1) 可以写做 相似地,剪切模量方程 和压缩模量方程 可以写作 其中 , 。因为一般粘弹性材料具有不可压缩性,我们可以假定 。Abaqus 使用方程(3)形式的 Prony series 模型计算粘弹性材料。该方程中 和 由输入的弹性参数 和 计算得到,其余的参数 ( , , ) 即为所需输入的 Prony series 参数。在 Abaqus 中使用 Maxwell 模型下面我们来计算 Maxwell 模型 ( ) 在 Abaqus 中使用所需要的参数。首先假设材料的泊松比为 ,则输入的弹性参数即为 和 。Prony series 的参数我们有 。因为 ,所以 ,相似地, 。另外这里有两点需要注意:Abaqus 无法计算 的材料,所以我们输入 Prony series 参数时可以取 ;在输入弹性参数时, moduli time scale 选择 Instantaneous。ReferenceABAQUS/Standard User's Manual, Version 6.9. Dassault Systèmes Simulia Corp, Providence, RI.Barbero, E.J., 2013. Finite element analysis of composite materials using AbaqusTM. CRC press.来源:复合材料力学仿真Composites FEM

未登录
还没有评论
课程
培训
服务
行家
VIP会员 学习 福利任务 兑换礼品
下载APP
联系我们
帮助与反馈