针刺C/C复合材料高温力学性能
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TB33;V25

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Analysis of High Temperature Mechanical Properties of Needled Felt C/C Composite Material
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    摘要:

    采用材料超高温力学性能设备及高温应变测试系统,对针刺C/C复合材料拉伸、压缩性能进行了研究。结果表明:针刺C/C复合材料具有明显的拉、压双模量特性,拉、压模量均随着温度的升高而线性下降,且拉伸模量下降更快;针刺C/C复合材料拉伸、压缩强度均随温度升高而先升高后降低,1 600℃时拉伸强度达到最大值,1 200℃时压缩强度达到最大值;其拉伸破坏为脆性断裂,断口呈现45°豁口;其压缩破坏为典型剪应力引起的压缩失效,破坏面倾角为40°~50°。

    Abstract:

    The tensile and compressive properties of needled felt C/C composite material at the temperature range of 20℃ to 1800℃ have been studied by test system of ultra-high temperature material performance and strain measurement system under high temperature. The results show that needled felt C/C composite material has different elastic modulus for tension and compression obviously, and the tensile and compressive modulus decrease linearly with the rise of temperature, but the tensile modulus decreases more quickly. At the same time, the tensile and compressive strength increase first then decrease with the rise of temperature, and the tensile strength reach to the maximum value at the temperature of 1600℃, then the compressive strength reach to the maximum value at the temperature of 1200℃. Needled felt C/C composite material shows fiber tensile brittle damage and fracture angle of 45° by high temperature tensile. On the other hand, needled felt C/C composite material shows compression failure caused by typical shear stress and the oblique angle of fracture plane is 45° under high temperature compression conditions.

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郑伟,林志远,刘芹,李耿,侯晓.针刺C/C复合材料高温力学性能[J].宇航材料工艺,2017,47(6):43-45.

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历史
  • 收稿日期:2017-03-02
  • 最后修改日期:2017-06-27
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  • 在线发布日期: 2017-12-12
  • 出版日期:
第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

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