Suppr超能文献

三维机织物增强复合加劲肋构件的失效机理

The Failure Mechanism of Composite Stiffener Components Reinforced with 3D Woven Fabrics.

作者信息

Hu Qiaole, Memon Hafeezullah, Qiu Yiping, Wei Yi

机构信息

Key Laboratory of Textile Science & Technology, Ministry of Education, College of Textiles, Donghua University, 2999 North Renmin Road, Shanghai 201620, China.

Center for Civil Aviation Composites, Donghua University, 2999 North Renmin Road, Shanghai 201620, China.

出版信息

Materials (Basel). 2019 Jul 10;12(14):2221. doi: 10.3390/ma12142221.

Abstract

Composite industry has long been seeking practical solutions to boost laminate through-thickness strengths and interlaminar shear strengths (ILSS), so that composite primary structures, such as stiffeners, can bear higher complex loadings and be more delamination resistant. Three dimensional (3D) woven fabrics were normally employed to render higher transverse and shear strengths, but the difficulty and high expense in producing such fabrics make it a hard choice. Based on a novel idea that the warp yarns that interlock layers of the weft yarns might provide adequate fiber crimps that would allow the interlaminar shear or radial stresses to be transferred and borne by the fibers, rather than by the relatively weaker matrix resin, thus improving the transverse strengths, this work provided a two point five dimensional (2.5D) approach as a practical solution, and demonstrated the superior transverse performances of an economical 2.5D shallow-bend woven fabric (2.5DSBW) epoxy composites, over the conventional two dimensional (2D) laminates and the costly 3D counterpart composites. This approach also produced a potential candidate to fabricate high performance stiffeners, as shown by the test results of L-beams which are common structural components of any stiffeners. This study also discovered that an alternative structure, namely a 2.5D shallow-straight woven fabric (2.5DSSW), did not show any advantages over the two control structures, which were a 2D plain weave (2DPW) and a 3D orthogonal woven fabric (3DOW) made out of the same carbon fibers. Composites of these structures in this study were conveniently fabricated using a vacuum-assisted resin infusion process (VARI). The L-beams were tested using a custom-made test fixture. The strain distribution and failure mode analysis of these beams were conducted using Digital Image Correlation (DIC) and X-ray Computed Tomography Scanning (CT). The results demonstrated that the structures containing Z-yarns or having high yarn crimps or waviness, such as in cases of 3DOW and 2.5DSBW, respectively, were shown to withstand high loadings and to resist delamination, favorable for the applications of high-performance structural composites.

摘要

复合材料行业长期以来一直在寻求切实可行的解决方案,以提高层压板的厚度方向强度和层间剪切强度(ILSS),从而使诸如加强筋之类的复合材料主要结构能够承受更高的复杂载荷并具有更强的抗分层能力。三维(3D)机织物通常用于提供更高的横向和剪切强度,但其生产难度大且成本高昂,这使其成为一个艰难的选择。基于一种新颖的想法,即联锁纬纱层的经纱可能提供足够的纤维卷曲,使层间剪切应力或径向应力能够由纤维而非相对较弱的基体树脂传递和承受,从而提高横向强度,本研究提供了一种二点五维(2.5D)方法作为切实可行的解决方案,并证明了一种经济的2.5D浅弯机织物(2.5DSBW)环氧复合材料在横向性能方面优于传统的二维(2D)层压板和昂贵的3D对应复合材料。正如任何加强筋的常见结构部件L形梁的测试结果所示,这种方法还产生了一种制造高性能加强筋的潜在候选材料。本研究还发现,另一种结构,即2.5D浅直机织物(2.5DSSW),与由相同碳纤维制成的两种对照结构(2D平纹织物(2DPW)和3D正交机织物(3DOW))相比,没有显示出任何优势。本研究中这些结构的复合材料使用真空辅助树脂灌注工艺(VARI)方便地制造出来。L形梁使用定制的测试夹具进行测试。使用数字图像相关(DIC)和X射线计算机断层扫描(CT)对这些梁进行应变分布和失效模式分析。结果表明,分别含有Z向纱线或具有高纱线卷曲或波纹的结构,如3DOW和2.5DSBW的情况,能够承受高载荷并抵抗分层,有利于高性能结构复合材料的应用。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/2f57/6678398/4617e8ab4c53/materials-12-02221-g001.jpg

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验