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High cycle fatigue life prediction of A16061-TiB2 in-situ composites

机译:A16061-TIB2原位复合材料的高循环疲劳寿命预测

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Fatigue characterization of metal matrix composites by experimental methods are being pursued seriously by several researchers. This is tedious and time consuming especially for complex shaped components. In recent years, finite element analysis is being exploited to predict the fatigue life of metallic components with good success. However no information is available as regards the prediction of fatigue life of metal matrix composites. Al6061-TiB2 in-Situ Composites possess high specific modulus and strength coupled with excellent wear resistance and high fatigue life as reported by several researchers. In the light of the above this paper focuses on prediction of high cycle fatigue life of A16061 TiB2 in-situ composites by using commercial FEA software (MSC-Patran, MSC-Nastran and MSC-Fatigue). The predicted result of high cycle fatigue life of matrix alloy Al-6061 is compared with standard data available in military data handbook. The test specimen as per ASTM standard for fatigue tests was modeled and FEA mesh was created. Fatigue analysis was preceded by static analysis run. The material properties data for the insitu composites were experimentally determined.
机译:几个研究人员严重追求了实验方法疲劳表征金属基质复合材料。这对于复杂形状的组件特别令人疑惑和耗时。近年来,正在利用有限元分析来预测金属部件的疲劳寿命良好的成功。然而,关于金属基质复合材料的疲劳寿命的预测没有任何信息。 AL6061-TIB2原位复合材料具有高特异性模量和强度,其具有优异的耐磨性和高疲劳寿命,如几个研究人员所述。根据上述本文,通过使用商业FEA软件(MSC-PUTAN,MSC-NASTRAN和MSC-DIRIGUE),专注于预测A16061 TIB2原位复合材料的高周期疲劳寿命。将矩阵合金AL-6061的高循环疲劳寿命的预测结果与军事数据手册中可用的标准数据进行比较。根据ASTM疲劳试验标准测试样品被建模,并创建了FEA网。疲劳分析前面是静态分析运行。实验确定了Insitu复合材料的材料属性数据。

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