Evaluation of the Microstructure, Tribological Characteristics, and Crack Behavior of a Chromium Carbide Coating Fabricated on Gray Cast Iron by Pulsed-Plasma Deposition
At a Glance
Section titled âAt a Glanceâ| Metadata | Details |
|---|---|
| Publication Date | 2021-06-19 |
| Journal | Materials |
| Authors | Yu. G. Chabak, V. G. Efremenko, Miroslav DĆŸupon, Kazumichi Shimizu, V.I. Fedun |
| Institutions | Pryazovskyi State Technical University, Muroran Institute of Technology |
| Citations | 10 |
| Analysis | Full AI Review Included |
Executive Summary
Section titled âExecutive SummaryâThis research validates the use of Pulsed-Plasma Deposition (PPD) followed by heat treatment (HT) to significantly enhance the wear resistance of Gray Cast Iron (GCI) via a high-chromium carbide coating.
- Coating Structure and Hardness: A 210-250 ”m thick composite coating was formed, consisting of 48 vol.% Cr-rich carbides (M7C3, M3C) embedded in a martensite/retained austenite matrix (48 vol.% martensite, 4 vol.% austenite). Microhardness was dramatically increased to 980-1180 HV.
- Metallurgical Bonding: PPD induced melting of the GCI substrate, creating a strong metallurgical bond via an 8-25 ”m transitional layer formed by the counter-diffusion of C, Cr, and Mn atoms.
- Abrasive Wear Performance: The coating exhibited 3.0-3.2 times higher abrasive wear resistance compared to both non-heat-treated and heat-treated GCI substrates.
- Dry-Sliding Performance: Volume loss under dry-sliding was reduced by factors ranging from 1.2 times (vs. steel ball) up to 1208.8 times (vs. diamond cone), demonstrating superior performance against hard counter-bodies.
- Critical Limitation: The as-deposited coating, initially mostly austenitic, generated high internal tensile stress (calculated at 5832 MPa) upon cooling, leading to solidification cracking. These cracks locally accelerate wear under high-stress contact.
Technical Specifications
Section titled âTechnical Specificationsâ| Parameter | Value | Unit | Context |
|---|---|---|---|
| Substrate Material | Gray Cast Iron (GCI) | N/A | Composition: 2.95 wt.% C, 1.45 wt.% Si, 0.95 wt.% Mn. |
| Cathode Material | High-Cr White Cast Iron | N/A | Source material: 27.39 wt.% Cr, 2.34 wt.% C. |
| Coating Thickness | 210-250 | ”m | After Pulsed-Plasma Deposition (PPD). |
| Transitional Layer Width | 8-25 | ”m | Formed at coating/substrate interface. |
| PPD Discharge Voltage | 4.0 | kV | Stored in 1.5 mF capacitor. |
| PPD Discharge Current | ~18 | kA | Peak current during pulsed arc discharge. |
| Post-Plasma Heat Treatment | 950 | °C | Holding temperature for 2 hours, followed by oil-quenching. |
| Coating Microhardness (HT) | 980-1180 | HV | Range from top surface to interface. |
| Substrate Microhardness (Initial) | 223 ± 25 | HV | Average microhardness of ferrite grains. |
| Carbide Volume Fraction (HT) | 48.2 | vol.% | Cr-rich carbides (M7C3, M3C) in the final coating. |
| Martensite Volume Fraction (HT) | 47.6 | vol.% | Matrix phase in the final coating. |
| Abrasive Wear Resistance Increase | 3.0-3.2 | times | Compared to GCI substrate (stable wear process). |
| Dry-Sliding Volume Loss (vs. Diamond Cone) | 0.49 x 10-3 | ”m3 | Lowest volume loss achieved by the coating. |
| Calculated Tensile Stress (As-Deposited) | 5832 | MPa | Stress attributed to the mostly austenitic structure causing cracking. |
Key Methodologies
Section titled âKey Methodologiesâ- Substrate and Cathode Selection: GCI specimens were used as the substrate. The cathode for the Electrothermal Axial Plasma Accelerator (EAPA) was a 5 mm rod of high-Cr white cast iron (27.4 wt.% Cr) to ensure a high-chromium coating.
- Pulsed-Plasma Deposition (PPD): Performed in air using an EAPA. The process involved 10 high-current pulses (~18 kA, 4.0 kV) which eroded the cathode. The erosion products (microdroplets and ions) were transferred by the plasma flow to the GCI target surface (50 mm distance).
- Plasma-Induced Melting: Numerical modeling confirmed that the plasma flow heated the substrate surface rapidly (up to 2350 °C), causing melting to a depth of up to 15 ”m. This molten layer mixed with the plasma material, ensuring strong metallurgical bonding.
- Post-Plasma Heat Treatment (HT): Specimens were held at 950 °C for two hours, covered in coal to prevent oxidation, and then oil-quenched. This HT promoted the precipitation of stable Cr-rich M7C3 carbides and the transformation of austenite to hard martensite.
- Microstructural Analysis: X-ray Diffraction (XRD) confirmed the phase transformation (austenite to martensite/carbides). Scanning Electron Microscopy (SEM) and EDS mapping revealed the elemental gradient (Cr and Mn decreasing, C increasing toward the substrate) and the formation of the carbide network.
- Tribological Testing:
- Three-Body Abrasion: Tested using Al2O3 particles (0.5-0.6 mm diameter) under a 20 N load against a rubber roller.
- Dry-Sliding: Reciprocating tests (5 N load) were conducted against three counter-bodies: 100Cr6 steel balls, SiC balls, and diamond cones, to evaluate performance under varying contact stresses and hardnesses.
Commercial Applications
Section titled âCommercial Applicationsâ- Tooling and Die Manufacturing: Strengthening wear-loaded tool steels, die forms, and molds used in cold stamping and forming processes, particularly for hybrid car bodies, where GCI is commonly utilized.
- High-Performance Sliding Components: Application in mechanical engineering components, such as cylinder liners or sliding bearings, where GCIâs inherent low abrasive resistance is a limitation.
- Rolling Equipment: Components subjected to high friction and abrasive conditions, leveraging the coatingâs high hardness and superior resistance to three-body abrasion.
- Hard-on-Hard Contact Systems: Use in systems where contact occurs against hard ceramic materials (like SiC), as the coating demonstrated significantly lower adhesion and volume loss against SiC compared to steel.
- Surface Hardening of Castings: General surface modification technique for structural GCI components where increased service life is required due to wear, offering a composite structure superior to simple case hardening.
View Original Abstract
The structural and tribological properties of a protective high-chromium coating synthesized on gray cast iron by air pulse-plasma treatments were investigated. The coating was fabricated in an electrothermal axial plasma accelerator equipped with an expandable cathode made of white cast iron (2.3 wt.% C-27.4 wt.% Cr-3.1 wt.% Mn). Optical microscopy, scanning electron microscopy, energy-dispersive spectroscopy, X-ray diffraction analysis, microhardness measurements, and tribological tests were conducted for coating characterizations. It was found that after ten plasma pulses (under a discharge voltage of 4 kV) and post-plasma heat treatment (two hours of holding at 950 °C and oil-quenching), a coating (thickness = 210-250 ”m) consisting of 48 vol.% Cr-rich carbides (M7C3, M3C), 48 vol.% martensite, and 4 vol.% retained austenite was formed. The microhardness of the coating ranged between 980 and 1180 HV. The above processes caused a gradient in alloying elements in the coating and the substrate due to the counter diffusion of C, Cr, and Mn atoms during post-plasma heat treatments and led to the formation of a transitional layer and different structural zones in near-surface layers of cast iron. As compared to gray cast iron (non-heat-treated and heat-treated), the coating had 3.0-3.2 times higher abrasive wear resistance and 1.2-1208.8 times higher dry-sliding wear resistance (depending on the counter-body material). The coating manifested a tendency of solidification cracking caused by tensile stress due to the formation of a mostly austenitic structure with a lower specific volume. Cracks facilitated abrasive wear and promoted surface spalling under dry-sliding against the diamond cone.
Tech Support
Section titled âTech SupportâOriginal Source
Section titled âOriginal SourceâReferences
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