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CLADDING · BIMETAL PRODUCT · BIMETAL PRESSURE VESSEL TECHNICAL STUDY

Effect of Post-Weld Tempering on Microstructure and Hardness Gradient of ZG15MnMoVCu Overlay Fusion Zone

Literature Overview

This 2015 study by Xiao Xinhua and Xing Zhigang from Hubei Polytechnic University and Henan Polytechnic University investigates the effects of post-weld tempering on the microstructure and hardness gradient in the fusion zone of ZG15MnMoVCu overlay weld deposits. Funded by the Hubei Provincial Department of Education Science and Technology Research Project (B2014028), this research addresses a critical quality concern in the manufacture of wear-resistant cast steel components where overlay welding is applied to enhance surface properties while maintaining the toughness of the base material.

The ZG15MnMoVCu base material is a medium-carbon cast steel alloyed with manganese, molybdenum, vanadium, and copper, designed for applications requiring a combination of strength, toughness, and moderate wear resistance. The overlay welding process introduces a dilution zone at the fusion line where the overlay material mixes with the base metal, creating a region with unique compositional and microstructural characteristics that often represent the weakest link in the component's performance.

Core Technical Findings

The study systematically examined the effects of tempering temperatures ranging from 500 °C to 700 °C on the fusion zone microstructure and hardness profile. Without post-weld tempering, the fusion zone typically exhibits a hard, brittle martensitic structure due to the high cooling rates inherent in welding processes and the alloying elements that promote hardenability. This untreated condition results in extremely high hardness values at the fusion line that can exceed 600 HV, creating a severe hardness mismatch with the adjacent base metal.

The tempering treatment was found to significantly modify the microstructure of the fusion zone. At 500 °C tempering, the martensite began to decompose, forming tempered martensite with dispersed carbides, reducing hardness by approximately 100-150 HV while maintaining acceptable strength. At 600 °C tempering, the decomposition was more complete, producing fine bainite-like structures with lower hardness but improved ductility. At 700 °C tempering, coarsening of carbides became evident, and while toughness improved further, the hardness reduction was more pronounced, potentially compromising wear resistance in the fusion zone.

Technical Parameter Analysis

Tempering Temperature (°C) Fusion Zone Hardness (HV) Base Metal Hardness (HV) Hardness Gradient (HV/mm) Microstructure
As-welded 580-650 250-300 40-55 Martensite + retained austenite
500 °C 450-520 250-280 25-35 Tempered martensite
600 °C 350-420 250-280 15-25 Fine bainite
700 °C 280-350 250-280 5-15 Coarse bainite + pearlite

The hardness gradient analysis revealed that without tempering, the transition from overlay hardness to base metal hardness occurs over a very short distance, creating a steep gradient that can act as a stress concentrator under cyclic loading. Post-weld tempering at 600 °C was identified as the optimal condition, reducing the hardness gradient to a more manageable level while maintaining sufficient hardness in the overlay layer for wear resistance applications.

Standards and Quality Control Considerations

From a standards perspective, the hardness gradient in the fusion zone is a critical parameter that affects the acceptance criteria for overlay welds. According to NB/T 47014 and related qualification standards, the hardness of the fusion zone should not exceed a specified multiple of the base metal hardness, typically limited to 1.5 times the base metal hardness for carbon and low-alloy steel systems. The as-welded condition of ZG15MnMoVCu overlay welds frequently violates this criterion, making post-weld tempering not merely beneficial but often mandatory for code compliance.

The study also implicitly addresses the issue of temper embrittlement, which is a concern for low-alloy steels tempered in the range of 400-600 °C. While the ZG15MnMoVCu composition does not contain significant amounts of embrittling elements such as antimony, tin, or phosphorus, the presence of molybdenum and vanadium can contribute to temper embrittlement susceptibility if the cooling rate through the embrittlement range is too slow. The study recommended rapid cooling after tempering to minimize this risk.

Engineering Practice Integration

In practical manufacturing of wear-resistant components using ZG15MnMoVCu base material, the post-weld tempering operation must be carefully controlled to achieve uniform treatment of the entire component. For large castings with significant thickness variations, achieving uniform tempering temperature distribution can be challenging, and thermocouple monitoring at multiple locations is recommended. The tempering cycle should include a preheat stage to reduce thermal gradients, a soak period at the target temperature for a duration proportional to the maximum section thickness, and a controlled cooling rate not exceeding 100 °C/h for components thicker than 50 mm.

The research findings support the adoption of a 600 °C tempering temperature as the default condition for ZG15MnMoVCu overlay welds, with adjustments made for specific application requirements. For applications where maximum wear resistance is required and the component is not subjected to significant impact loading, a lower tempering temperature of 500 °C may be acceptable. For applications requiring maximum toughness such as components operating in cold environments or under severe impact conditions, tempering at 650-700 °C may be appropriate, accepting the associated reduction in overlay hardness.

Key Reflections and Insights

The most significant insight from this study is the recognition that the fusion zone, rather than the overlay layer itself, often represents the critical region for component failure. While engineers frequently focus on achieving maximum hardness in the overlay layer, the fusion zone's mechanical properties and microstructural characteristics determine the long-term reliability of the component. The steep hardness gradient in the as-welded condition creates conditions favorable for crack initiation and propagation, and the brittle martensitic microstructure lacks the ductility necessary to accommodate plastic deformation under service loading.

The study also highlights the importance of considering the entire component's mechanical properties rather than focusing solely on the overlay layer. The base metal, heat-affected zone, fusion zone, and overlay layer form a continuum of properties, and the weakest link in this chain determines the component's overall performance. Post-weld tempering is the most effective means of optimizing this property distribution, and its parameters should be selected based on comprehensive consideration of all zones rather than the overlay layer alone.

Summary

This study demonstrates that post-weld tempering is essential for optimizing the microstructure and hardness gradient in the fusion zone of ZG15MnMoVCu overlay welds. A tempering temperature of 600 °C provides the best balance between wear resistance and toughness, reducing the hardness gradient to acceptable levels while maintaining adequate overlay hardness. Engineers should incorporate post-weld tempering as a standard practice in the manufacture of wear-resistant components using this base material, with careful attention to temperature control, soak time, and cooling rate to achieve uniform treatment and avoid temper embrittlement.