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CLADDING · BIMETAL PRODUCT · BIMETAL PRESSURE VESSEL TECHNICAL STUDY

Wear Resistance and Wear Mechanism of Metal Overlay Deposits Containing Inherent Hard Carbide Particles

Literature Overview

This study, published in 2004 in the Journal of Tribology, investigates the tribological behavior of weld overlay deposits that contain in-situ formed hard carbide particles. The research team, led by Yang Shanglai and Lu Xueqin from Shanghai Jiao Tong University's Institute of Welding, with contributions from Zou Zengda at Shandong University and Lou Songnian, was supported by the Shandong Provincial Natural Science Foundation (Z2000F02). The work addresses a critical engineering need: extending the service life of components subjected to severe abrasive and erosive wear by leveraging the intrinsic formation of carbide phases within the overlay microstructure rather than relying solely on externally added hard particles.

Core Technical Content

The fundamental premise of this research is that certain alloy compositions, when deposited through welding processes, naturally form hard carbide phases during solidification and subsequent heat treatment. These in-situ carbides—typically Cr7C3, Cr3C2, or mixed carbides involving Mo and W—act as wear-resistant second-phase particles dispersed within a relatively ductile matrix. The authors systematically examined how the morphology, distribution, and volume fraction of these carbides influence the overall wear performance of the overlay layer.

The study employed standard pin-on-disk and block-on-ring wear testing configurations to characterize abrasive wear behavior under controlled conditions. The key finding is that the wear resistance is governed by a synergistic interaction between the hard carbide particles and the surrounding matrix. When the carbide volume fraction is too low, the matrix alone cannot withstand abrasive contact. When the volume fraction is excessively high, the brittleness of the carbide-rich microstructure leads to spalling and catastrophic failure. The optimal window typically falls within a carbide volume fraction of 15% to 35%, depending on the specific alloy system and service conditions.

Parameter Typical Range Effect on Wear Resistance
Carbide volume fraction 15–35% Optimal wear resistance in this range
Carbide hardness (HV) 1600–2200 Higher hardness correlates with lower wear rate
Matrix hardness (HV) 300–500 Provides toughness to prevent spalling
Test load (pin-on-disk) 20–50 N Higher loads shift wear mechanism from mild to severe
Sliding distance 500–5000 m Wear rate stabilizes after initial run-in period

Wear Mechanism Analysis

The authors identified three primary wear mechanisms operating in the overlay deposits: abrasive wear, adhesive wear, and fatigue wear. The relative contribution of each mechanism depends on the contact conditions, carbide distribution, and matrix ductility. Under mild abrasive conditions, the hard carbide particles resist material removal by ploughing and micro-cutting resistance, while the ductile matrix accommodates deformation without cracking. Under severe conditions, the carbides may fracture and detach, exposing the softer matrix to accelerated material loss.

A particularly insightful observation from this work is the concept of the "protective tribofilm." During sliding, fine debris from the carbide-matrix interface accumulates on the wear track surface, forming a thin film that can reduce direct contact between the counterpart and the overlay. This tribofilm effect is most pronounced when the carbide particles are uniformly distributed and the matrix has sufficient ductility to prevent large-scale spalling. The study also highlights that the orientation and shape of the carbides matter: plate-like carbides aligned perpendicular to the wear surface provide superior resistance to ploughing, while equiaxed carbides offer more uniform protection against multi-directional sliding.

Engineering Practice Implications

From a practical standpoint, this research has direct relevance to the selection of overlay alloys for mining equipment, cement mill liners, and slurry pump components. The in-situ carbide approach offers advantages over externally added carbide composites because the bonding between the carbide and the matrix is metallurgical rather than mechanical, resulting in better resistance to particle pull-out during service. For engineers specifying overlay alloys, the key actionable takeaway is that alloy design should target the formation of a specific carbide type and morphology rather than simply maximizing carbon content. Excessive carbon leads to continuous carbide networks that embrittle the deposit and promote intergranular cracking.

Study Insights and Reflections

After reviewing this literature, I reflect that the work represents a mature understanding of carbide-based wear protection that emerged in the early 2000s. The methodology is rigorous, combining microstructural characterization with quantitative wear testing. One area that subsequent research has expanded upon is the role of residual stress in the overlay layer, which can significantly influence the initiation of fatigue cracks at the carbide-matrix interface. Additionally, modern high-entropy alloy concepts have opened new avenues for in-situ carbide formation with broader compositional windows. Nevertheless, the fundamental principles established in this study—optimal carbide volume fraction, morphology control, and matrix-carbide synergy—remain the cornerstone of wear-resistant overlay design. Engineers working on component repair and protection should always verify the actual carbide morphology through metallographic examination rather than relying solely on chemical composition analysis.