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Hard Anodizing of Aerospace AA7075-T6 Aluminum Alloy for Improving Surface Properties

机译:航空航天AA7075-T6铝合金的硬阳极氧化,改善表面特性

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In the current research work undertaken, an oxide film was grown by performing hard anodizing process on a pure aluminum layer deposited by PVD magnetron sputtering process on AA7075-T6 alloy. The corresponding tribo-mechanical properties were evaluated and compared with those of the base alloy. The dry sliding wear experiments were carried out to investigate wear resistance of anodized AA7075-T6 against the AISI SS316 counter-body by means of a reciprocating tribo-testing setup. The hardness of AA7075-T6 after the anodizing process exhibited an enhancement of about 1.94 times. Results revealed that the wear of anodized coating was exceptionally less when compared with the substrate. Based on morphology and chemistry changes of worn-out surfaces and debris, it was determined that severe abrasive and oxidative wear was the primary wear mechanism for AA7075-T6. The anodizing process increased the friction coefficient from 0.33 to 0.46 but reduced the wear severity by altering the wear mechanism into mild polishing and abrasion. Anodizing enhanced the wear resistance of AA7075-T6 to about three times, and the wear rate decreased to around 4.3 times.
机译:在目前进行的研究工作中,通过在AA7075-T6合金上对PVD磁控溅射工艺沉积的纯铝层进行硬阳极氧化过程来生长氧化膜。评价相应的摩擦机械性能并与基础合金的相应的摩擦机械性能进行评价。进行干滑动磨损实验,以通过往复摩擦测测试来研究阳极氧化AA7075-T6对AISI SS316对应体的耐磨性。阳极氧化过程后AA7075-T6的硬度表现出约1.94倍的增强。结果表明,与基材相比,阳极氧化涂层的磨损较少。基于磨损表面和碎片的形态和化学变化,确定严重的磨料和氧化磨损是AA7075-T6的初级磨损机制。阳极氧化过程将摩擦系数从0.33增加到0.46,但通过将磨损机构改变为温和的抛光和磨损来降低耐磨性程度。阳极氧化增强了AA7075-T6至约三次的耐磨性,磨损率降至约4.3倍。

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