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Aging behavior and thermal treatment of aluminum alloy AA6061 refined by different grain refiner master alloys

机译:不同谷物炼油厂母磨合金铝合金AA6061的老化行为及热处理

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摘要

Al-Mg alloys are excellent candidates for engineering light structure materials, and have great potential in automotive, high Performance defence and aerospace applications. The effect of grain refiner master alloys on the aging behaviour of aluminium alloys AA 6061 are investigated. The addition of grain refiner particles in AA6061 alloy does not change the aging sequence. However, the result showed that the grain refiner master alloys accelerated the aging kinetic and reduced the aging times compared to the non-grain refined alloy AA 6061. During the precipitation hardening of AI alloy 6061 at 175°C, the peak aging of AA6061 which was grain refined by Al5-Ti-1B occurs at 6 h and at 8 h for the non-grain refined AA6061. The effects of prior cold-work on the recrystallisation behaviour during annealing process was studied for AA6061 with and without grain refiner master alloys. Recrystallisation started early at 200°C for the alloys which were grain refined and at 275°C for that which was not grain refined. Full recrystallisation ended up at 350°C and 400°C for the grain refined and the non-grain refined AA6061, respectively. Thus, the recrystallisation starts early in the microstructure which contains coarse distribution of large particles of intermetallic phases TiAl_3, TiB_2 and β second phase. In recent years, aluminum alloys have attracted the attention of many researchers, engineers and designers as promising structural materials for automotive industry or aerospace applications. The first register of production of an Al-6000 alloy was in 1921 when the Al 6061 alloy was produced with levels of 1 wt.% Si and 0.5 wt.% Mg, that is one of the earliest aluminum alloy aged without copper [1].
机译:Al-Mg合金是工程光结构材料的优秀候选者,拥有汽车,高性能防御和航空航天应用的巨大潜力。研究了晶粒炼油厂主合金对铝合金AA 6061衰老行为的影响。 AA6061合金中的晶粒精细晶体的添加不会改变老化序列。然而,结果表明,与非晶粒精制合金AA 6061相比,晶粒炼油厂主合金加速了老化动力学并降低了老化时间。在175℃下AI合金6061的沉淀硬化期间,AA6061的峰老化由Al5-Ti-1b精制的晶粒在6小时和8小时内发生,对于非晶粒精制AA6061。研究了在退火过程中的结晶行为对退火过程中的反再结晶行为的影响,用于AA6061,具有晶粒炼油母合金。重结晶在200℃的早期开始,对于晶粒精制的合金,在275℃下为未晶粒精制。全重结晶在350°C和400°C的完全重结晶分别用于晶粒精制和非晶粒精制AA6061。因此,重结晶在微观结构早期开始,其含有大颗粒的金属间相TiAl_3,Tib_2和β第二阶段的大颗粒的粗糙分布。近年来,铝合金吸引了许多研究人员,工程师和设计师的关注,作为汽车工业或航空航天应用的有希望的结构材料。 Al-6000合金的第一个生产寄存器是在1921年,当Al 6061合金的水平为1重量%的Si和0.5重量%。%Mg,即没有铜的最早铝合金之一[1] 。

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