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    Thermal Modeling and Feedforward Control for Defect Mitigation in Laser Powder Bed Fusion Process

    Source: Journal of Manufacturing Science and Engineering:;2026:;volume( 148 ):;issue:003
    Author:
    Spadaccia, David
    ,
    Darji, Mihir
    ,
    Deshmukh, Kaustubh
    ,
    Carrington, Antonio
    ,
    Kudale, Swayam
    ,
    Riensche, Alex
    ,
    Williams, Christopher
    ,
    Rao, Prahalada
    DOI: 10.1115/1.4070940
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Modeling and control of the spatiotemporal temperature distribution (thermal history) in laser powder bed fusion (LPBF) is critical because the thermal history governs defects, such as porosity, poor surface finish, cracking, and deformation. This article presents a coupled physics-based computational modeling and feedforward process control framework for regulating the thermal history in LPBF-processed parts. Existing LPBF process optimization relies on empirical parameter tuning by manufacturing and testing of simple, standardized coupon geometries. Empirical coupon-based optimization inherently disregards the geometry-dependent effect of thermal history on defect formation. Consequently, process parameters optimized based on coupon studies, when used for manufacturing real-world components, often result in build failures and defects. To address this limitation, a rapid graph theory-based computational model was coupled to a feedforward control (FFC) algorithm. The approach is implemented for manufacturing a topology-optimized Inconel 718 aerospace component (GE bracket). The model-guided FFC approach maintains a constant end-of-cycle (interpass or interlayer) temperature across layers by adjusting the laser power and velocity. The processing parameters are adjusted in silico—offline and prior to manufacturing—within the thermal model. Compared to its empirically optimized counterpart, the FFC-processed GE bracket exhibited three characteristics favorable to functional integrity and production: (i) meltpool instability-induced porosity was not observed; (ii) thermal-induced deformation, dross formation, and recoater contact damage were significantly mitigated; and (iii) FFC-induced improvements enabled the part to be manufactured with 45% less support mass, resulting in a 20% reduction in the as-built part weight (with the part design unchanged). This work thus underscores the potential of physics-based control, as opposed to empirical optimization, to mitigate defects in LPBF parts and accelerate their practical deployment.
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      Thermal Modeling and Feedforward Control for Defect Mitigation in Laser Powder Bed Fusion Process

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    contributor authorSpadaccia, David
    contributor authorDarji, Mihir
    contributor authorDeshmukh, Kaustubh
    contributor authorCarrington, Antonio
    contributor authorKudale, Swayam
    contributor authorRiensche, Alex
    contributor authorWilliams, Christopher
    contributor authorRao, Prahalada
    date accessioned2026-08-23T08:17:26Z
    date available2026-08-23T08:17:26Z
    date copyright2026/03/01
    date issued2026
    identifier issn1087-1357
    identifier othermanu-25-1530.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316335
    description abstractAbstract. Modeling and control of the spatiotemporal temperature distribution (thermal history) in laser powder bed fusion (LPBF) is critical because the thermal history governs defects, such as porosity, poor surface finish, cracking, and deformation. This article presents a coupled physics-based computational modeling and feedforward process control framework for regulating the thermal history in LPBF-processed parts. Existing LPBF process optimization relies on empirical parameter tuning by manufacturing and testing of simple, standardized coupon geometries. Empirical coupon-based optimization inherently disregards the geometry-dependent effect of thermal history on defect formation. Consequently, process parameters optimized based on coupon studies, when used for manufacturing real-world components, often result in build failures and defects. To address this limitation, a rapid graph theory-based computational model was coupled to a feedforward control (FFC) algorithm. The approach is implemented for manufacturing a topology-optimized Inconel 718 aerospace component (GE bracket). The model-guided FFC approach maintains a constant end-of-cycle (interpass or interlayer) temperature across layers by adjusting the laser power and velocity. The processing parameters are adjusted in silico—offline and prior to manufacturing—within the thermal model. Compared to its empirically optimized counterpart, the FFC-processed GE bracket exhibited three characteristics favorable to functional integrity and production: (i) meltpool instability-induced porosity was not observed; (ii) thermal-induced deformation, dross formation, and recoater contact damage were significantly mitigated; and (iii) FFC-induced improvements enabled the part to be manufactured with 45% less support mass, resulting in a 20% reduction in the as-built part weight (with the part design unchanged). This work thus underscores the potential of physics-based control, as opposed to empirical optimization, to mitigate defects in LPBF parts and accelerate their practical deployment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermal Modeling and Feedforward Control for Defect Mitigation in Laser Powder Bed Fusion Process
    typeJournal Paper
    journal volume148
    journal issue3
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.4070940
    treeJournal of Manufacturing Science and Engineering:;2026:;volume( 148 ):;issue:003
    contenttypeFulltext
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