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

  • Chengkun Li
  • , Yujia Cai
  • , Shouzhen Zhou
  • , Hao Chang
  • , Junfei Teng
  • , Yanlong Lv
  • , Zhibo Dong*
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Beijing Power Machinery Institute
  • China Aviation Industry Corporation

Research output: Contribution to journalArticlepeer-review

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 4-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.

Original languageEnglish
Pages (from-to)1621-1635
Number of pages15
JournalJournal of Materials Research and Technology
Volume42
DOIs
StatePublished - 1 May 2026

Keywords

  • Deformation prediction
  • Equivalent section modulus
  • Four-bar model
  • Laminated cooling plate
  • Laser butt welding
  • Out-of-plane deformation

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