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Microstructural observations of porosity in A319.2 alloy: effect of mold type/cooling rate

机译:A319.2合金中气孔的显微组织观察:模具类型/冷却速率的影响

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摘要

A parametric study of porosity formation in A319.2 aluminum alloy was carried out, as a function of hydrogen con tent, melt additives (Sr modifier and Al-Ti-B grain refiner) and cooling rate, using two different types of molds: an end-chill mold that provided unidirectional solidification, and in which the solidification rate decreased with increasing distance from the chill end; and a cooling fin sand mold whose different sized fins provided different cooling rates, and the means of isolating the effect of hydrogen in each fin, in the same casting. The effects of inclusions and intermetallics on porosity formotion were also studied. This paper highlights the main micro-structural observations of porosity formation and pore characteristics noted in the two cases. It is found that, under directional solidification conditions, the hydrogen gas present in the melt is pushed upward by the moving solidification front, resulting in a gradient in the porosity observed (percentage porosity and pore size) along the height of the casting. Thus, the porosity observed at any given level above the chill end is dependent upon the hydrogen accumulated in the region just below. In the sand mold case, however, the hydrogen gas is trapped within the cast fins, and results in much greater pore sizes and porosity, compared to the end-chilled cast samples. This effect is more pronounced at the highest cooling rate (DAS~25μm). Inclusions andβ-Al{sub}5FeSi intermetallics were frequently observed in connection with both microshrinkage and gas-type porosities. The nature 0f the moving solidification front in the sand mold fins causes pore coalescence due to the impingement of the gas bubbles that evolve within the liquid alloy during the solidification process. Similar effects are also observed for shrinkage pores. This linking of pores is particularly detrimental to casting soundness and strength.
机译:使用两种不同类型的模具,根据氢含量,熔融添加剂(Sr改性剂和Al-Ti-B晶粒细化剂)和冷却速率对A319.2铝合金中的孔隙形成进行了参数研究:提供单向凝固的端冷模具,其凝固速率随与冷端距离的增加而降低;冷却翅片砂型,其尺寸不同的翅片提供不同的冷却速率,以及在同一铸件中隔离每个翅片中的氢影响的方法。还研究了夹杂物和金属间化合物对孔隙度的影响。本文重点介绍了这两种情况下孔隙形成和孔隙特征的主要微观结构观察结果。已发现,在定向凝固条件下,熔体中存在的氢气通过移动的凝固前沿被向上推动,导致沿铸件高度观察到的孔隙率(孔隙率和孔径百分比)出现梯度。因此,在冷却端以上任何给定水平上观察到的孔隙度取决于在下方区域中积累的氢。但是,在砂模的情况下,与最终冷却的铸件样品相比,氢气被捕集在铸件翅片中,并导致更大的孔径和孔隙率。在最高冷却速度(DAS〜25μm)下,这种效果更加明显。在微收缩率和气孔率方面都经常观察到夹杂物和β-Al{sub} 5FeSi金属间化合物。砂模翅片中移动的凝固前沿的性质0f导致孔凝结,这是由于在凝固过程中在液态合金内产生的气泡的撞击所致。对于收缩孔也观察到类似的效果。孔的这种连接特别不利于铸件的稳固性和强度。

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