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The effect of composite orientation on the mechanical properties of hybrid joints strengthened by surfi-sculpt

机译:复合造型对表面造型强化混合接头力学性能的影响

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摘要

Advanced hybrid joints strengthened by surfi-sculpt (manufactured by electron beam surfi-sculpt (EBS)) have been developed to address the challenges in joining fibre reinforced polymer (FRP) composites to metals. In the present work, the effect of composite orientation on the mechanical properties of the joints is experimentally studied. In the study, the thickness of the composite adherend is kept constant and the volume content of 45 ply is increased from 11.1% to 88.9%. Joints without surfi-sculpts are manufactured as reference joints. The result indicates that surfi-sculpt is able to delay the damage initiation and improve the joints ultimate failure load, failure strain, and absorbed energy. Composite orientation is able to vary joints mechanical properties significantly. With the volume content of 45 ply increase, joints damage mechanisms change from bare composite matrix crush to the combination of surfi-sculpts bending, surfi-sculpts breakage and composite compression. With optimum composite orientation, the joints damage initiation load is increased by 24.84%, the joints ultimate failure load is increased by 134.5% and the joint energy absorption is increased by 257.39%. Scanning electron microscope (SEM) observation shows that surfi-sculpts experience three damage stages. (C) 2015 Elsevier Ltd. All rights reserved.
机译:已经开发出通过表面雕刻(由电子束表面雕刻(EBS)制造)增强的高级混合接头,以解决将纤维增强聚合物(FRP)复合材料与金属连接起来的挑战。在目前的工作中,实验研究了复合取向对接头力学性能的影响。在研究中,复合被粘物的厚度保持恒定,45层的体积含量从11.1%增加到88.9%。没有表面造型的关节被制造为参考关节。结果表明,surfi-sculpt能够延迟损伤的产生,并改善关节的最终破坏载荷,破坏应变和吸收能量。复合材料的取向能够显着改变接头的机械性能。随着45层板的体积含量的增加,接头的损坏机理从裸露的复合材料基体破碎变为sur-sculpts弯曲,surfi-sculpts断裂和复合材料压缩的组合。在最佳的复合取向下,关节损伤的初始载荷增加了24.84%,关节的极限破坏载荷增加了134.5%,关节的能量吸收提高了257.39%。扫描电子显微镜(SEM)的观察表明,表面雕刻经历了三个损坏阶段。 (C)2015 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures》 |2015年第12期|587-592|共6页
  • 作者单位

    Univ London Imperial Coll Sci Technol & Med, Dept Mech Engn, London SW7 2AZ, England|Aviat Ind Corp China, Aircraft Inst 1, Xian 710089, Peoples R China;

    Univ London Imperial Coll Sci Technol & Med, Dept Mech Engn, London SW7 2AZ, England;

    Univ London Imperial Coll Sci Technol & Med, Dept Mech Engn, London SW7 2AZ, England;

    Beijing Aeronaut Mfg Technol Res Inst, Beijing 100024, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Composite; Advanced hybrid joint; Surfi-sculpt; EBM; Composite orientation;

    机译:复合材料;高级混合接头;Surfi雕刻;EBM;复合材料取向;
  • 入库时间 2022-08-17 13:07:56

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