C/ SiC 与TC4 钎焊接头的热震性能
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航天材料及工艺研究所

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Thermal Shock Resistance of Carbon/ Silicon CarbideComposite and TC4 Titanium Alloy Joints
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    摘要:

    采用AgCuTi+10vol% ~30vol%SiC 对C/ SiC 与TC4 进行钎焊,后对钎焊接头进行室温~600益热
    震试验。使用扫描电镜观察了不同钎焊工艺下,钎焊接头的界面微观组织和热震裂纹的产生情况。结果表明:
    随着连接材料中SiC 粉末含量的增加,接头残余应力降低;采用较大间隙值钎焊工艺,当中间层内SiC 颗粒含
    量较高时(20vol% ~30vol%),经过30 次热震试验后,钎焊试样未发现热震裂纹。

    Abstract:

    C/ SiC composites and TC4 titanium alloy were joined by brazing technique, using AgCuTi+10vol%
    to 30vol%SiC composite filler metals and the thermal shock behavior of the joints were investigated between 600益
    and room temperature. Interface microstructures and fracture cracks were investigated by scanning electron microscopy (with EDS energy spectrum). The results showed the thermal stress of the joints reduces evidently, with the increase
    of the amount of SiC particle. In the brazing joints, thermal shock cracks can be found in the SiC ceramics near bond鄄
    ing layer or in the fillet. It seems that wide鄄gap brazing samples have better thermal shock resistance, and no cracks
    were obseured for filler metals containing 20vol% to 30vol% SiC particle, after 30 times thermal shock testing.

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吴永智. C/ SiC 与TC4 钎焊接头的热震性能[J].宇航材料工艺,2012,42(5).

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  • 在线发布日期: 2016-11-28
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