首页> 外文期刊>Journal of the Aeronautical Society of India >TENSILE, FATIGUE AND IMPACT PROPERTIES OF THE AA 2618/AL_2O_(3P) COMPOSITES
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TENSILE, FATIGUE AND IMPACT PROPERTIES OF THE AA 2618/AL_2O_(3P) COMPOSITES

机译:AA 2618 / AL_2O_(3P)复合材料的拉伸,疲劳和冲击性能

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摘要

In this paper, the tensile properties (at RT and 200℃), high cycle fatigue and impact behaviour of the 2618 aluminium alloy reinforced with 5% wt. of Al_2O_3 particles (AA 2618/Al_2O_(3p)/5P) and 10% wt. of Al_2O_(3p)articles (AA 2618/Al_2O_(3p) /10P) were studied. The Composites were prepared by two-step mixing of stir casting method followed by forging. A significant increase in tensile strength of the MMCs, with respect to the unreinforced alloys was evidenced by the tensile test while the elongation to fracture decreased. Tensile property at 200℃ is higher than the unreinforced counterpart. The high cycle fatigue tests showed that fatigue life is comparable to the monolithic alloy. The SEM analysis of the fracture surfaces showed that the presence of secondary precipitates played a significant role in the mechanism of failure in composites by promoting void nucleation at the particle-matrix interfaces, interfacial decohesion and also the failure of the particles. The impact strength is reduced with respect to the unreinforced alloy.
机译:本文研究了5%wt增强的2618铝合金的拉伸性能(在室温和200℃下),高循环疲劳和冲击行为。 Al_2O_3颗粒(AA 2618 / Al_2O_(3p)/ 5P)和10%wt。研究了Al_2O_(3p)的含量(AA 2618 / Al_2O_(3p)/ 10P)。通过搅拌铸造法的两步混合然后锻造来制备复合材料。相对于未增强的合金,MMC的抗拉强度显着提高,而拉伸试验表明断裂伸长率降低。 200℃时的拉伸性能比未增强时高。高循环疲劳测试表明,疲劳寿命与整体式合金相当。断裂表面的SEM分析表明,二次沉淀的存在在复合材料的破坏机理中起着重要作用,它通过促进颗粒-基体界面处的空核,界面脱粘以及颗粒的破坏而起作用。相对于非增强合金,冲击强度降低。

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