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Microstructure and thermal expansion of copper-based amorphous alloys during structural relaxation

机译:结构松弛过程中铜基非晶合金的微观结构和热膨胀

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(Cu43Zr48Al9)98Y2 amorphous alloy bar was prepared by the arc melting copper mold absorptioncasting method, and then, the amorphous alloy was annealed at different temperatures for different times. Theinfluence of heating rate on thermal expansion and thermal stability was studied by thermomechanical analysis(TMA), and the microstructure evolution of the amorphous alloy during structural relaxation and crystallization wasstudied by XRD and TEM. Results show that the structural evolution behavior of the (Cu43Zr48Al9)98Y2 amorphousalloy can be divided into five different stages (structural relaxation preparation stage, structural relaxation stage,first crystallization stage, second crystallization stage, and grain growth stage). When the heating rate is 20 K/min, the amorphous alloy has the smallest thermal expansion coefficient and the best thermal stability. The widthof the supercooled liquid region is 66.42 K. Samples with different relaxation states were prepared by annealingat the heating rate of 20 K/min. The structural evolution of amorphous alloys with different relaxation states isas follows: amorphous → CuZr2 + AlCu2Zr7 → CuZr2 + AlCu2Zr7 + CuZr(B2) + CuZr(M) + Cu10Zr7 → CuZr2 +AlCu2Zr7 + CuZr(B2) + CuZr(M). After annealing at 706 K and 726 K (in the supercooled liquid region) for 1.5h, the amorphous-nanocrystalline composites were obtained. When the annealing temperature is 706 K, thecrystallization process of the sample is as follows: amorphous → Cu10Zr7 → Cu10Zr7 + CuZr, and for the sampleat 726 K, it is as follows: amorphous → CuZr2 + AlCu2Zr7 + Cu10Zr7 → Cu10Zr7 + CuZr2 → CuZr2 + CuZr (B2) +Cu10Zr7.
机译:(CU43ZR48AL9)通过电弧熔化铜模具吸收法制备98毫米合金棒,然后,在不同时间的不同温度下退火非晶合金。通过热机械分析(TMA)研究了加热速率对热膨胀和热稳定性的影响,并且结构松弛期间无定形合金的微观结构演变和XRD和TEM钝化。结果表明,(CU43ZR48A19)98Y2氨基铝合金的结构演化行为可分为五个不同的阶段(结构松弛制剂阶段,结构松弛阶段,第一结晶阶段,第二结晶阶段和晶粒生长阶段)。当加热速率为20 k / min时,无定形合金具有最小的热膨胀系数和最佳的热稳定性。过冷液区域的宽度为66.42k.通过退火为20k / min的加热速率来制备具有不同弛豫状态的样品。不同弛豫状态的无定形合金的结构演变均外:无定形→CuzR2 + Alcu2ZR7→CuzR2 + Alcu2Zr7 + Cuzr(B2)+ Cuzr(M)+ Cu10Zr7→CuzR2 + Alcu2Zr7 + Cuzr(B2)+ Cuzr(M)。在706 k和726k(在过冷液区域中的726k(在过冷液区域中)进行1.5h后,得到无定形纳米晶复合材料。当退火温度为706 k时,样品的替换过程如下:无定形→Cu10ZR7→Cu10ZR7 + Cuzr,以及Sampleat 726 K,如下:无定形→CuzR2 + Alcu2Zr7 + Cu10Zr7→Cu10Zr7 + CuzR2→CuzR2 + CUZR(B2)+ CU10ZR7。

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