1. 上海理工大学,上海,200093
2. 苏州倍丰激光科技有限公司,苏州,215151
纸质出版:2024
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王林洋,黄海军,孙明丰,王皞. 薄壁构件增材制造有限元模拟及快速补偿模型[J]. 航空制造技术, 2024, 67(23/24): 126-134. WANG Linyang, HUANG Haijun, SUN Mingfeng, WANG Hao. Finite Element Simulation and Rapid Compensation Model for Additive Manufactured hin-Walled Components[J]. Aeronautical Manufacturing Technology, 2024, 67(23/24): 126-134.
WANG Linyang, HUANG Haijun, SUN Mingfeng, et al. Finite Element Simulation and Rapid Compensation Model for Additive Manufactured hin-Walled Components[J]. Aeronautical Manufacturing Technology, 2024, 67(23/24).
王林洋,黄海军,孙明丰,王皞. 薄壁构件增材制造有限元模拟及快速补偿模型[J]. 航空制造技术, 2024, 67(23/24): 126-134. WANG Linyang, HUANG Haijun, SUN Mingfeng, WANG Hao. Finite Element Simulation and Rapid Compensation Model for Additive Manufactured hin-Walled Components[J]. Aeronautical Manufacturing Technology, 2024, 67(23/24): 126-134. DOI: 10.16080/j.issn1671-833x.2024.23/24.126.
WANG Linyang, HUANG Haijun, SUN Mingfeng, et al. Finite Element Simulation and Rapid Compensation Model for Additive Manufactured hin-Walled Components[J]. Aeronautical Manufacturing Technology, 2024, 67(23/24). DOI: 10.16080/j.issn1671-833x.2024.23/24.126.
激光粉末床熔融(L-PBF)技术在复杂工件一体化成形中得到广泛应用,但打印过程中激光快速升温和冷却过程产生的热应力会影响工件的成形质量。基于有限元方法建立了细观与宏观两种尺度下TC4合金材料L-PBF成形过程模型。在细观尺度下评估三层道次扫描过程中实时温度场及应力场,探究工艺参数与打印层数对熔池等细观尺度的影响,发现熔池尺寸的增长对功率更敏感,且高功率可以释放下层积累的热应力,但同时也有更高的冷却速率使最大热应力升高。在宏观尺度下构建工件整体打印模型,并基于细观尺度结果调整成形参数,对残余应力分布和变形结果进行预测,二者吻合较好。基于部件实际的打印结果,通过构建补偿模型,将最大位移量由0.626 mm减小至0.027 mm,降低约95.7%;平均位移量由0.595 mm减小至0.024 mm,降低约95.97%,且计算时间控制在合理范围内。
Laser powder bed fusion (L-PBF) technology has been widely used in the integration forming of complex parts. However
the thermal stress generated by the rapid heating and cooling during the printing process affects the forming quality of parts. In this study
a two-scale model of TC4 alloy L-PBF forming process was established based on finite element method (FEM) at micro and macro-scale. At the micro level
the real-time temperature fields and stress distribution during three-layer scan process were evaluated
and the effects of process parameters and printing layers on the microscale such as melt pool size were explored. It was found that the growth of the melt pool size was more sensitive to power
and high power could release the accumulated thermal stress in the lower layers
but it also had a higher cooling rate which would increase the maximum thermal stress. At the macro level
the overall printing model of the part was constructed
and the forming parameters were adjusted based on the microscopic scale results. The residual stress distribution and deformation results were predicted
and good agreement was found between the two. Based on the actual printing results of the component
by constructing a compensation model
the maximum displacement was reduced from 0.626 mm to 0.027 mm
a decrease of approximately 95.7%; The average displacement was reduced from 0.595 mm to 0.024 mm
a decrease of approximately 95.97%
and the calculation time was controlled within a reasonable range.
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