Research on Coordinative Deformation Mechanism Between Layers of 304/Q235 Composite Plate under Thermal/Mechanical Coupling
Source abstract
Abstract
When the dissimilar metal composite plate accumulates inconsistent deformation to a certain degree during the heat treatment process, it indicates bad plate morphology such as warpage. Therefore, it is crucial to explore the mechanism of coordinated deformation between layers under thermal–mechanical coupling during heat treatment. This study investigates the interlayer coordinated deformation mechanism of the stainless-steel clad plate (304/Q235 stainless-steel clad plate) under thermal–mechanical coupling by using three heat treatment methods: rapid cooling process, rapid cooling in the high-temperature stage + slow cooling in the low-temperature stage, and rapid cooling + tempering process. And this study enlightens that the temperature field distribution and the longitudinal stress–strain distribution are obtained by using the Abaqus software. The effects of different tensile and thickness ratios on the residual stress are analyzed. The final experiment found that the maximum longitudinal stress and plastic strain appear on the upper and lower surfaces during heat treatment. The rapid cooling heat treatment process has light warpage and good shape. When the thickness ratio of the composite plate is 1:4, the warpage is the lightest. The increase of set tension will increase the compressive stress value in the residual stress. In contrast, the tensile stress value will decrease.
Source: expertdata · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: High-Velocity Impact and Material Behavior · Welding Techniques and Residual Stresses · Titanium Alloys Microstructure and Properties
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
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