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Manufacturing Titanium Metal Matrix Composites by Consolidating Matrix Coated Fibres

机译:通过固结基体涂覆的纤维制造钛金属基复合材料

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Titanium metal matrix composites (TiMMCs) reinforced by continuous silicon carbide fibres are being developed for aerospace applications. TiMMCs manufactured by the consolidation of matrix-coated fibre (MCF) method offer optimum properties because of the resulting uniform fibre distribution, minimum fibre damage and fibre volume fraction control. In this paper, the consolidation of Ti-6Al-4V matrix-coated SiC fibres during vacuum hot pressing has been investigated. Experiments were carried out on multi-ply MCFs under vacuum hot pressing (VHP). In contrast to most of existing studies, the fibre arrangement has been carefully controlled either in square or hexagonal arrays throughout the consolidated sample. This has enabled the dynamic consolidation behaviour of MCFs to be demonstrated by eliminating the fibre re-arrangement during the VHP process. The microstructural evolution of the matrix coating was reported and the deformation mechanisms involved were discussed.
机译:由连续碳化硅纤维增强的钛金属基复合材料(TiMMC)正在为航空航天应用开发。通过固结基质涂层纤维(MCF)的方法制造的TiMMC具有最佳的性能,这是因为可以实现均匀的纤维分布,最小的纤维损伤和纤维体积分数控制。本文研究了Ti-6Al-4V基体包覆SiC纤维在真空热压过程中的固结。实验是在真空热压(VHP)下在多层MCF上进行的。与大多数现有研究相反,在整个合并样品中,纤维排列均以正方形或六边形阵列进行了精心控制。通过消除VHP过程中的光纤重新排列,可以证明MCF的动态整合行为。报告了基体涂层的微观结构演变,并讨论了所涉及的变形机理。

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