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Research on Microscopic Properties of TiBw/TC4 Composites for Drilling Process

机译:TIBW / TC4复合材料微观性能研究钻孔过程

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摘要

TiB-whisker-reinforced TiBw/TC4 composites are widely used in aviation, aerospace, automotive, and various other industries. However, the drilling force and temperature have a large effect on the drilling micromechanical properties of TiBw/TC4 composites. In order to explore the micro-mechanical properties and promote the optimization of drilling process, the representative volume elements of TiBW/TC4 composites were established in the Digimat-FE software tool to determine the micromechanical properties and failure mechanism of TiBW/TC4 composites. The results show: (1) maximum stress occurs at the whiskers, whereas the minimum stress appears within the basket matrix region of the reinforced phase. (2) When the force reached 300 N and the temperature reached 75 °C, the junction between the whiskers and the matrix firstly failed; when the force reached 525 N and the temperature reached 112 °C, the matrix began to fail; when the force reached 675 N and the temperature reached 138 °C, the whiskers failed. (3) The main reason for the failure of the junction between the matrix and the whiskers was that the shear stress exceeded the connection strength and the axial stress accelerated the failure process. Displacement and rotation of the whiskers were shown to occur at the moment of junction failure, owing to differences in the stress experienced on different sides of the material.
机译:TIB-WHISKER-COONFORCED TIBW / TC4复合材料广泛用于航空,航空航天,汽车和各种行业。然而,钻探力和温度对TIBW / TC4复合材料的钻孔微机械性能具有很大的影响。为了探讨微机械性能并促进钻孔过程的优化,在Digimat-Fe软件工具中建立了TIBW / TC4复合材料的代表性体积元素,以确定TIBW / TC4复合材料的微机械性能和故障机制。结果表明:(1)晶须发生最大应力,而最小应力出现在增强相的篮子基质区域内。 (2)当动力达到300n和温度达到75℃时,晶须和基质之间的连接首先失效;当力达到525 n并且温度达到112°C时,矩阵开始失效;当力达到675 n和温度达到138°C时,晶须失败。 (3)基质和晶须之间的连接失效的主要原因是剪切应力超过连接强度,并且轴向应力加速了故障过程。由于在材料的不同侧面所经历的差异,所示,晶须的位移和旋转发生在结失效时发生。

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