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Experimental investigation of the tension-torsion coupling behavior on needled unidirectional C/SiC composites

机译:针刺单向C / SiC复合材料拉扭耦合行为的实验研究

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摘要

Mechanical responses and failure mechanisms of ceramic matrix composites under tension-shear loading are important for structure design. In this paper, tension-torsion coupling tests were performed to study the mechanical behaviors of the needled unidirectional C/SiC composites. The results showed that the coupled tensile load decreases the torsional stiffness and failure load. The stable stage of the torsional damage with coupled tensile load was shorter than that of pure torsion. The failure mechanisms at micro level include fiber fracture, long range fiber bundle pull-out, fiber bridging, fiber/matrix interface debonding, matrix cracking, matrix fragment desquamating and matrix peeling. The failure mechanisms at macro level include delamination, axial split and irregular fracture at the root of specimens. The extent of axial split failure and the fibers distribution of the irregular fracture under pure torsion and torsion-tension coupling load were different.
机译:拉伸剪切载荷下陶瓷基复合材料的力学响应和破坏机理对结构设计很重要。在本文中,进行了拉扭耦合试验,以研究针刺单向C / SiC复合材料的力学性能。结果表明,耦合的拉伸载荷降低了扭转刚度和破坏载荷。加上拉伸载荷的扭转损伤的稳定阶段要短于纯扭转的稳定阶段。微观上的失效机制包括纤维断裂,长距离纤维束拉出,纤维桥接,纤维/基质界面剥离,基质破裂,基质碎片脱皮和基质剥离。宏观上的破坏机制包括分层,轴向分裂和试样根部的不规则断裂。在纯扭力和扭拉耦合载荷作用下,轴向断裂破坏的程度和不规则断裂的纤维分布是不同的。

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  • 来源
    《Materials Science and Engineering》 |2017年第1期|190-197|共8页
  • 作者单位

    Key Laboratory of Aero-engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, NanjingUniversity of Aeronautics and Astronautics, Nanjing 210016, PR China,Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing210016, PR China;

    Key Laboratory of Aero-engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, NanjingUniversity of Aeronautics and Astronautics, Nanjing 210016, PR China,Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing210016, PR China;

    Key Laboratory of Aero-engine Thermal Environment and Structure, Ministry of Industry and Information Technology, College of Energy and Power Engineering, NanjingUniversity of Aeronautics and Astronautics, Nanjing 210016, PR China,Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing210016, PR China,State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, PR China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Tension-torsion coupling; Torsional behavior; Failure mechanism; Damage evolution; C/SiC composite tube;

    机译:拉扭耦合扭转行为;失效机制;损害演变;C / SiC复合管;

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