Deformation mechanisms and prediction of laser butt-welded thin-walled laminated cooling plates with equivalent section-modulus modeling and experimental verification

Welding-induced out-of-plane deformation is a critical issue for thin-walled laminated cooling plates used in aero-engine hot-section components, where internal channels and supporting pillars markedly reduce bending resistance. This work investigates laser butt welding of GH3230 laminated plates through deformation and residual-stress measurements combined with directly coupled thermo-mechanical finite element simulations in MSC Marc. To model the complex internal architecture efficiently, the pin-fin pillars are simplified using a section-modulus-matching strategy that preserves the bending section modulus of the original cylindrical pillars. Two implementations are assessed. The square-pillar equivalence reduces computation time by more than 50% relative to the hexagonal scheme while maintaining comparable accuracy. Under identical heat input, laminated and solid plates exhibit similar longitudinal and transverse residual-stress distributions, whereas laminated plates develop much larger longitudinal warping and angular deformation. This contrast indicates that deformation is governed primarily by the spatial distribution and through-thickness gradient of welding-induced plastic strain rather than by the peak residual-stress level. A longitudinal four-bar model relates the longitudinal plastic-zone width to a stiffness-related parameter and through-thickness thermal asymmetry, and a transverse-section model shows that non-uniform transverse heating shifts the neutral plane and strengthens the through-thickness gradient of longitudinal plastic strain. Based on these mechanisms, heat-input-dependent amplification relationships are formulated to predict laminated-plate deformation from solid-plate FE results and validated on an additional plate-size pair, achieving a maximum relative error within 10% for both longitudinal warping and angular deformation.

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Publication Details

Journal
Journal of Materials Research and Technology
Published
2026-03-24
DOI
https://doi.org/10.1016/j.jmrt.2026.03.121
Primary Topic
Laser and Thermal Forming Techniques
Type
article
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article

Deformation mechanisms and prediction of laser butt-welded thin-walled laminated cooling plates with equivalent section-modulus modeling and experimental verification

Journal of Materials Research and Technology
Laser and Thermal Forming Techniques
article

Deformation mechanisms and prediction of laser butt-welded thin-walled laminated cooling plates with equivalent section-modulus modeling and experimental verification

article en

Abstract

Welding-induced out-of-plane deformation is a critical issue for thin-walled laminated cooling plates used in aero-engine hot-section components, where internal channels and supporting pillars markedly reduce bending resistance. This work investigates laser butt welding of GH3230 laminated plates through deformation and residual-stress measurements combined with directly coupled thermo-mechanical finite element simulations in MSC Marc. To model the complex internal architecture efficiently, the pin-fin pillars are simplified using a section-modulus-matching strategy that preserves the bending section modulus of the original cylindrical pillars. Two implementations are assessed. The square-pillar equivalence reduces computation time by more than 50% relative to the hexagonal scheme while maintaining comparable accuracy. Under identical heat input, laminated and solid plates exhibit similar longitudinal and transverse residual-stress distributions, whereas laminated plates develop much larger longitudinal warping and angular deformation. This contrast indicates that deformation is governed primarily by the spatial distribution and through-thickness gradient of welding-induced plastic strain rather than by the peak residual-stress level. A longitudinal four-bar model relates the longitudinal plastic-zone width to a stiffness-related parameter and through-thickness thermal asymmetry, and a transverse-section model shows that non-uniform transverse heating shifts the neutral plane and strengthens the through-thickness gradient of longitudinal plastic strain. Based on these mechanisms, heat-input-dependent amplification relationships are formulated to predict laminated-plate deformation from solid-plate FE results and validated on an additional plate-size pair, achieving a maximum relative error within 10% for both longitudinal warping and angular deformation.

Journal of Materials Research and TechnologyVol. 42
Commercial Aircraft Corporation of China (China) (CN), Harbin Institute of Technology (CN), Beijing Institute of Power Machinery (China) (CN)
Sustainable cities and communities
Openalex Percentile: Top 8%
Laser and Thermal Forming Techniques
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