Tufting缝合C/C复合材料制备与力学性能

Preparation and mechanical properties of tufting C/C composites

  • 摘要: 采用Tufting缝合机器人研制碳纤维缝合预制体,通过改变预制体结构与致密化方式,制备具有不同结构的缝合C/C复合材料,探讨基体类型、网胎引入、针刺工艺等对缝合C/C复合材料力学性能的影响规律,并探讨力学性能影响机理。结果表明:在完全相同的预制体结构条件下,采用化学气相沉积工艺致密的缝合C/C拉伸模量和拉伸强度更高,采用化学气相沉积+糠酮树脂浸渍碳化工艺制备的缝合C/C具有更加优异的层间剪切性能与弯曲性能。在完全相同的复合致密条件下,网胎层的加入对于提高C/C复合材料弯曲、剪切性能有积极的作用,逐层针刺+缝合C/C复合材料强度性能优于缝合C/C复合材料,但因针刺工艺的引入削弱了缝合C/C复合材料的“假塑形”变形能力。

     

    Abstract: Using Tufting robot, carbon fiber tufted perform was developed. By changing the parameters of tufting and needle punching processes, tufted C/C composites with different structures and a combination of tufting and needle punching C/C composites were prepared. The effects of parameters such as matrix type, mesh felt and needle punching process on the mechanical properties of tufted C/C composites were studied, and the mechanism for the influence of preform structure on the mechanical properties of C/C composites were explored. The results showed that the addition of mesh layer or resin carbon matrix had a positive effect on improving the bending and shear performance of C/C composites. The strength performance of needle punched and tufted C/C composites was better than that of tufted C/C composites, but the introduction of needle punching technology weakened the “pseudo plastic” deformation of stitched C/C composites.

     

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