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基于机器学习的航天筒形件铸造工艺优化设计
    Design and Optimizationof ProcessParametersfor Aerospace CylindricalCastingBased on MachineLearning
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- DOI:
- 作者:
- 盛子懿,邱昊岳,沈厚发
 SHENG Ziyi, QIU Haoyue, SHEN Houfa
- 作者单位:
- 清华大学 材料学院,北京 100084
 School of Materials Science and Engineering, Tsinghua University, Beijing 100084,China
- 关键词:
- 低压铸造;缩孔疏松;机器学习;高斯回归;遗传算法;数值模拟
 low-pressure casting; shrinkage porosity; machine learning; Gaussian regression; genetic algorithm; numerical simulation
- 摘要:
- 航天舱体等薄壁铸件厚度不均,容易产生凝固补缩困难。 采用数值模拟方法研究低压铸造铝硅合金筒形件凝固缩孔疏松。 基于高斯回归代理模型及遗传算法开发了数据驱动型机器学习程序。 结果表明,机器学习预测的低压铸造疏松结果与基于机理模型的数值模拟结果一致。 保压压力愈大、过热度愈小、充型时间愈短,铸件形成疏松的倾向性愈小。 机器学习可设计出比正交设计更优的工艺参数,使用机器学习预测疏松的效率比数值模拟更高。The thickness of thin-walled castings such as aerospace cabin bodies is uneven, which makes it difficult to feed them during solidification. The shrinkage porosity of cylindrical low-pressure aluminium-silicon alloy castings was studied via numerical simulation. A data-driven machine learning program was developed on the basis of the Gaussian regression surrogate model and genetic algorithm. The results show that the shrinkage porosity predicted by machine learning in low-pressure casting is consistent with the numerical simulation results based on the mechanism model. The higher holding pressure with the lower degree of superheating and the shorter filling time lead to a smaller tendency toward porosity formation during casting. Compared with an orthogonal design, machine learning can design reasonable process parameters. The efficiency of predicting porosity via machine learning is greater than that via numerical simulation.
    
     
 
 
         
            












