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Simulation and experimental study on thermal deep drawing of carbon fiber woven composites

机译:碳纤维编织复合材料热深拉伸的模拟和实验研究

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摘要

Carbon fiber woven composites are composed of carbon fiber woven and resin matrix. To reduce the manufacture cost, thermal stamping, a new forming technology, was proposed and investigated to fabricate composite part. The mechanical properties of carbon fiber have great influence on the deformation of carbon fiber composites. In this study, shear angle-displacement curves and shear load-shear angle curves were obtained from picture frame test. Thermal deep drawing experiments and simulation were conducted, and the shear load-displacement curves under different forming temperatures and shear angle-displacement curves were obtained. The results show the compression and shear between fiber bundles are the main deformation mechanism of carbon fiber woven composite. The maximum shear angle for the composites in this study is 33. In the drawing process, the forming temperature affects the drawing force, which drops rapidly with the increasing temperature. The suitable forming temperature in deep drawing of the carbon fiber woven composite is approximately 170℃.
机译:碳纤维编织复合材料由碳纤维编织物和树脂基体组成。为了降低制造成本,提出并研究了一种热成型技术,即热冲压技术,以制造复合材料零件。碳纤维的机械性能对碳纤维复合材料的变形有很大的影响。在这项研究中,通过镜框试验获得了剪切角位移曲线和剪切载荷剪切角曲线。进行了热拉伸试验和模拟,得到了不同成形温度下的剪切载荷-位移曲线和剪切角-位移曲线。结果表明,纤维束之间的压缩和剪切是碳纤维编织复合材料的主要变形机理。在这项研究中,复合材料的最大剪切角为33。在拉伸过程中,成型温度会影响拉伸力,随着温度的升高,拉伸力会迅速下降。碳纤维织造复合材料在深冲中合适的成型温度约为170℃。

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