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首页> 外文期刊>Indian Journal of Science and Technology >Analysis of Crown Shrinkage in Gravity Die Cast Aluminium Alloy LM 13 Piston
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Analysis of Crown Shrinkage in Gravity Die Cast Aluminium Alloy LM 13 Piston

机译:重力铸造铝合金LM 13活塞的凸度收缩分析

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Background/Objectives: Optimization of process parameters to obtain shrinkage free engine piston based on Al-Si casting alloy LM 13 fabricated by gravity die casting. Method/Statistical Analysis: Experimental analysis of design and process parameters like riser sleeve size, center core temperature, pouring metal temperature and solidification time was carried out on Al-Si casting alloy LM 13 based engine piston fabricated by die casting technique. The die casting experiments with different solidification time 90, 120 and 150 seconds and volume of molten metal consumed by different sleeve size were carried out to obtain optimum conditions to produce shrinkage free engine pistons. The die casted engine piston were sectioned and checked for shrinkage at different design and process parameters. Results/Findings: The results showed that there is an effect of centre core temperature towards the shifting of shrinkage from the crown to riser. The center core temperature should not be maintained below 200°C and should be in the range of 200 - 238°C. But it cannot be concluded that the crown shrinkage is only due to the centre core temperature. The molten metal Al-Si is less dense as a liquid than as a solid so castings shrink upon cooling, which can leave a void at the last point to solidify. Risers prevent this by providing molten Al-Si alloy to the casting as it solidifies, so that the shrinkage forms in the riser and not the in engine piston casting. It was found that the size of sleeve size is indirectly proportional to the occurrence of crown shrinkage and increase in size of sleeve size reduces the chances of shrinkage. Engine piston section results showed the shrinkage shifting from casting to riser side by increasing the sleeve size. However the effect of different solidification time and pouring metal temperature was not so significant on the occurrence of shrinkage. Applications/Improvements: The optimized center core pin temperature and riser sleeve size successfully prevented the shrinkage formation in the Al-Si casting alloy LM 13 engine piston casting. This not only helps in improving the casting quality but also in increasing the production.
机译:背景/目的:优化工艺参数以获得基于重力模铸的Al-Si铸造合金LM 13的无收缩发动机活塞。方法/统计分析:对通过压铸技术制造的Al-Si铸造合金LM 13基发动机活塞进行了设计和工艺参数(如冒口套筒尺寸,中心芯温度,浇注金属温度和凝固时间)的实验分析。进行了不同凝固时间90、120和150秒以及不同套筒尺寸消耗的熔融金属量的压铸实验,以获得生产无收缩发动机活塞的最佳条件。对压铸的发动机活塞进行切片,并检查其在不同设计和工艺参数下的收缩率。结果/发现:结果表明,中心核心温度对收缩率从胎冠到立管的转移有影响。中心核心温度不应保持在200°C以下,并且应在200-238°C的范围内。但是不能得出结论,冠部收缩仅是由于中心核心温度引起的。熔融金属Al-Si的液体密度小于固体密度,因此铸件在冷却时会收缩,从而在最后凝固时留下空隙。冒口通过在铸件凝固时向铸件提供熔融的Al-Si合金来防止这种情况,从而在冒口中而不是在发动机活塞铸件中形成收缩。已经发现,套筒尺寸的大小与胎冠收缩的发生成间接比例,并且套筒尺寸的增加减小了收缩的机会。发动机活塞截面结果表明,通过增加套筒尺寸,收缩率从铸件侧转移到冒口侧。但是,不同的凝固时间和浇注金属温度对收缩的发生影响不大。应用/改进:优化的中心芯销温度和冒口套筒尺寸成功防止了Al-Si铸造合金LM 13发动机活塞铸件中的收缩。这不仅有助于提高铸件质量,而且还可以提高产量。

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