Heat Treatment Process Study of Multi-Element Alloy Iron-Based Overlay Layer
Literature Overview
This 2008 study by Fan Ping and Mu Yunchao, published in Hot Working Technology (热加工工艺) and conducted at the School of Materials and Chemical Engineering at Zhongyuan University of Technology, investigates the effects of heat treatment on the microstructure, hardness, and wear resistance of multi-element alloy iron-based overlay layers. Multi-element alloy iron-based overlay materials are widely used in applications requiring high wear resistance, including mining equipment, material handling systems, and heavy industrial machinery.
The study addresses a critical gap in overlay welding practice: while the as-deposited overlay layer often provides adequate wear resistance, the presence of residual stresses, coarse microstructures, and retained austenite can limit the long-term performance and reliability of the overlay. Post-weld heat treatment is therefore essential for optimizing overlay performance, but the optimal heat treatment parameters depend on the specific alloy composition and application requirements.
Core Technical Findings
Overlay Material Composition
The multi-element alloy iron-based overlay material investigated in this study contained the following key alloying elements:
| Element | Content (wt%) | Role |
|---|---|---|
| Cr | 12 to 16 | Carbide formation, solid solution strengthening |
| Mo | 2 to 4 | Carbide formation, high-temperature strength |
| W | 1 to 3 | High-temperature strength, carbide stability |
| V | 1 to 2 | Fine carbide precipitation, wear resistance |
| Ni | 3 to 6 | Austenite stabilization, toughness |
| Mn | 1 to 3 | Austenite stabilization, hardenability |
| C | 2.5 to 4.0 | Carbide formation, hardness |
The high carbon content (2.5 to 4.0 wt%) is characteristic of wear-resistant overlay materials, providing the carbon necessary for forming hard carbides such as M7C3 and M23C6. The combination of chromium, molybdenum, tungsten, and vanadium provides multiple carbide-forming elements, resulting in a complex carbide population that contributes to high hardness and wear resistance.
As-Deposited Microstructure
The as-deposited overlay layer exhibited the following microstructural characteristics:
- Matrix: Predominantly martensite with retained austenite, resulting from the rapid solidification during welding.
- Carbides: Coarse primary carbides of M7C3 and M23C6 type, distributed throughout the martensitic matrix.
- Hardness: 650 to 720 HV, primarily due to the martensitic matrix and coarse carbide population.
- Retained austenite: 8 to 15% by volume, which can transform during service and cause dimensional instability.
- Residual stresses: Tensile residual stresses in the range of 200 to 350 MPa, which can lead to cracking and spalling under cyclic loading.
Heat Treatment Effects
The study investigated several heat treatment conditions and their effects on the overlay microstructure and properties:
| Treatment Condition | Temperature (°C) | Time (h) | Cooling Method | Hardness (HV) | Retained Austenite (%) |
|---|---|---|---|---|---|
| As-deposited | - | - | - | 680 | 12 |
| Stress relief | 550 | 2 | Air cooling | 620 | 10 |
| Temper 1 | 600 | 2 | Air cooling | 580 | 5 |
| Temper 2 | 650 | 2 | Air cooling | 520 | 2 |
| Temper 3 | 700 | 2 | Air cooling | 480 | 1 |
| Tempering + quench | 600/800 | 2/1 | Oil quench | 650 | 3 |
| Double temper | 600/600 | 2/2 | Air cooling | 560 | 4 |
Microstructural Evolution During Heat Treatment
The heat treatment caused the following microstructural changes:
- Stress relief (550°C): Reduced residual stresses by approximately 60% while maintaining the martensitic matrix and carbide population. Hardness decreased slightly due to carbide coarsening.
- Tempering (600 to 700°C): Transformed retained austenite to martensite, which subsequently tempered. The tempering temperature determined the final microstructure and hardness:
- At 600°C: Fine tempered martensite with dispersed carbides, providing good toughness and wear resistance.
- At 650°C: Coarser tempered martensite with larger carbides, providing higher toughness but lower hardness.
- At 700°C: Spheroidized carbides in a ferritic matrix, providing maximum toughness but significantly reduced hardness.
- Double tempering (600/600°C): The first temper eliminated retained austenite, and the second temper further stabilized the microstructure, providing a good balance of hardness and toughness.
Wear Resistance Evaluation
The wear resistance was evaluated using a pin-on-disc test under dry sliding conditions, and the results are summarized as follows:
| Treatment Condition | Hardness (HV) | Wear Volume Loss (mm³) | Wear Rate (10⁻⁶ mm³/N·m) |
|---|---|---|---|
| As-deposited | 680 | 1.2 | 0.8 |
| Stress relief | 620 | 1.5 | 1.0 |
| Temper 600°C | 580 | 1.8 | 1.2 |
| Temper 650°C | 520 | 2.5 | 1.7 |
| Temper 700°C | 480 | 3.8 | 2.6 |
| Tempering + quench | 650 | 1.1 | 0.75 |
| Double temper | 560 | 1.9 | 1.3 |
The results demonstrate that the as-deposited overlay provides the highest wear resistance, but the tempering plus quench treatment offers a good compromise between wear resistance and toughness, while the double temper treatment provides the best balance of properties for applications requiring moderate wear resistance and high toughness.
Process Recommendations
Based on the study findings, the following heat treatment recommendations are provided for different application scenarios:
| Application Requirement | Recommended Treatment | Rationale |
|---|---|---|
| Maximum wear resistance | As-deposited or temper + quench | Highest hardness and wear resistance |
| Balanced wear and toughness | Stress relief or double temper | Good balance of hardness and toughness |
| Maximum toughness | Temper at 650 to 700°C | Maximum toughness, acceptable wear resistance |
| Dimensional stability | Stress relief or double temper | Eliminates retained austenite and reduces stresses |
| Fatigue resistance | Stress relief or double temper | Reduces residual stresses and improves fatigue life |
Integration with Engineering Practice
This study provides practical guidance for the heat treatment of multi-element alloy iron-based overlay layers in engineering applications. The following key points are relevant for practitioners:
- Heat treatment is not optional: Even when the as-deposited overlay provides adequate hardness, heat treatment is essential for eliminating residual stresses, stabilizing the microstructure, and ensuring long-term performance reliability.
- Treatment selection depends on application: The optimal heat treatment condition depends on the specific application requirements, balancing wear resistance, toughness, and dimensional stability.
- Retained austenite must be controlled: Retained austenite can transform during service, causing dimensional changes and potential cracking. Heat treatment should be designed to minimize or eliminate retained austenite.
- Residual stress reduction is critical: Tensile residual stresses in the overlay can lead to cracking and spalling under cyclic loading. Stress relief or tempering treatments should be applied to reduce residual stresses to acceptable levels.
Study Insights and Reflections
This study underscores the importance of post-weld heat treatment in overlay welding practice, a step that is sometimes overlooked in favor of simply relying on the as-deposited properties of the overlay material. The systematic investigation of heat treatment effects on microstructure, hardness, and wear resistance provides a clear framework for treatment selection based on application requirements. The finding that tempering plus quenching can restore hardness after tempering is particularly valuable, as it provides a practical approach to achieving both high wear resistance and improved toughness. For engineers working on overlay applications in heavy industry, this study reinforces the principle that the optimal overlay performance is achieved through the careful integration of welding process parameters, alloy composition, and post-weld heat treatment, rather than through any single factor alone. The study also highlights the trade-offs inherent in overlay engineering: increasing toughness necessarily reduces hardness, and vice versa, and the optimal balance must be determined by the specific application requirements.
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