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将超声场引入7050铝合金半连续铸造过程中,用Leica光学显微镜观察了铸锭的组织,结合RDG热裂纹判据和凝固补缩理论分析了超声场对热裂纹形成的影响机理。结果表明:在未施加超声场的铸锭中心发现有热裂纹,而施加超声场的铸锭中没有发现热裂纹;施加超声场的铸锭组织均匀,晶粒显著细化,组织由未加超声场时的柱状晶变为等轴晶;施加超声场可有效抑制热裂纹的形成。

Ultrasonic field was applied to prepare 7050 aluminum alloy semi-casting aluminum alloy ingot, the microstructure of the ingots were observed by Leica optical microscopy and the effect mechanism of ultrasonic field on hot tearing forming was analysed by combining the RDG hot tearing criterion and solidification shrinkage theory. The result show that a crack was found in the center of the ingot without ultrasonic field and no crack was found in the ingot with ultrasonic field. The microstructure of ingot with ultrasonic field was homogeneous, the grain size was obviously refined and the microstructure was changed into equiaxed grains from dendritic crystals without ultrasonic field. The ultrasonic field could effectively depress hot tear forming.

参考文献

[1] R. Vertnik;M. Zaloznik;B. Sarler .Solution of transient direct-chill aluminium billet casting problem with simultaneous material and interphase moving boundaries by a meshless method[J].Engineering analysis with boundary elements,2006(10):847-855.
[2] Q. Du;D.G. Eskin;L. Katgerman .The effect of ramping casting speed and casting temperature on temperature distribution and melt flow patterns in the sump of a DC cast billet[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2005(0):144-150.
[3] Pan J.;Yoshida M. .Ultrasonic Insert Casting Of Aluminum Alloy[J].Scripta materialia,2000(2):155-159.
[4] ZHANG Li-hua,YU Jun,ZHANG Xiao-ming.Effect of ultrasonic power and casting speed on solidification structure of 7050 aluminum alloy ingot in ultrasonic field[J].中南大学学报(英文版),2010(03):431-436.
[5] M.Rappaz;J.M.Drezet .A new hot-tearing criterion[J].Metallurgical and materials transactions. A, physical metallurgy and materials science,1999(2):449-455.
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