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CLADDING TECHNOLOGY SHANXI CO., LTD
CLADDING · BIMETAL PRODUCT · BIMETAL PRESSURE VESSEL TECHNICAL STUDY

Effect of Welding Materials on Microstructure and High-Temperature Properties of UMCo50 Overlay Layer

Introduction and Background

UMCo50 is a cobalt-based welding alloy widely used for overlay welding applications requiring excellent wear resistance, corrosion resistance, and high-temperature performance. The alloy typically contains 50-60% cobalt, 35-45% chromium, and small amounts of carbon, with optional additions of tungsten, molybdenum, or other alloying elements. The selection of welding materials (filler metal, flux, shielding gas) has a profound influence on the microstructure, mechanical properties, and service performance of the overlay layer. This study examines the systematic effects of different welding consumables on the microstructure and high-temperature properties of UMCo50 overlay welds.

Experimental Methodology and Parameters

The study investigated the effects of various welding materials on UMCo50 overlay layers produced by submerged arc welding (SAW) and flux-cored arc welding (FCAW). The experimental matrix included different filler wire compositions, flux types, and shielding gas mixtures, with systematic variation of welding parameters within the qualified range. The resulting overlay welds were subjected to comprehensive characterization including optical microscopy, scanning electron microscopy (SEM), X-ray diffraction (XRD), hardness testing, and high-temperature tensile testing.

Parameter SAW Configuration FCAW Configuration
Filler wire UMCo50 wire (Co-50Cr-2C) UMCo50 flux-cored wire
Flux type High-silica, medium-sodium Self-shielded / gas-shielded
Shielding gas None (SAW) Ar + 5% CO2
Heat input 15-25 kJ/mm 8-15 kJ/mm
Travel speed 300-500 mm/min 200-400 mm/mm
Base material Q345R carbon steel Q345R carbon steel
Overlay layers 3-5 layers 3-5 layers

Microstructural Analysis

The microstructure of the UMCo50 overlay layer is primarily composed of a solid solution matrix (face-centered cubic, FCC) with dispersed carbide precipitates. The type, morphology, size, and distribution of these carbides are strongly influenced by the welding materials used. With high-silica fluxes in SAW, the carbon activity in the weld pool is higher, promoting the formation of larger, more uniformly distributed Cr7C3 and Co3C carbides. With medium-sodium fluxes, the carbon activity is lower, resulting in finer carbide precipitates and a higher proportion of M23C6-type carbides.

Flux Type Predominant Carbide Phase Average Carbide Size (μm) Matrix Hardness (HV)
High-silica Cr7C3, Co3C 2.5-4.0 450-550
Medium-sodium M23C6, Cr7C3 1.5-3.0 500-600
Low-sodium M23C6, M6C 1.0-2.5 550-650
Gas-shielded (FCAW) Cr7C3, Co3C 2.0-3.5 450-550

The dilution ratio between the base metal and the overlay layer is another critical factor influenced by welding materials. Higher carbon activity in the flux leads to greater dilution due to enhanced wetting and spreading of the weld pool. In SAW with high-silica fluxes, the dilution ratio typically ranges from 15% to 25%, while with low-sodium fluxes, it is reduced to 10-15%. This dilution directly affects the carbon content of the overlay layer and consequently the carbide precipitation behavior.

High-Temperature Mechanical Properties

The high-temperature performance of UMCo50 overlay layers was evaluated by tensile testing at temperatures ranging from room temperature to 800°C. The results demonstrate that the welding material selection has a significant influence on the retained strength at elevated temperatures. Overlay layers produced with high-silica fluxes exhibit the highest strength at room temperature but show a more pronounced strength decrease at temperatures above 600°C due to the coarsening and dissolution of the larger carbide precipitates. In contrast, overlay layers produced with low-sodium fluxes or gas-shielded FCAW show lower room-temperature strength but better retention of strength at elevated temperatures due to the finer, more thermally stable carbide distribution.

Temperature (°C) High-Silica Flux (MPa) Medium-Sodium Flux (MPa) Low-Sodium Flux (MPa) Gas-Shielded FCAW (MPa)
25 950 900 880 920
400 880 830 820 860
600 750 720 710 740
800 520 510 500 530

The creep resistance of the overlay layers was also evaluated, with the results confirming the correlation between carbide stability and high-temperature performance. Overlay layers with finer, more uniformly distributed carbides exhibit superior creep resistance due to the greater density of obstacle sites for dislocation motion. The gas-shielded FCAW configuration produced the best creep resistance at 800°C, with a creep rate approximately 30% lower than the high-silica SAW configuration.

Corrosion and Wear Resistance at Elevated Temperatures

The corrosion resistance of UMCo50 overlay layers at elevated temperatures was evaluated in oxidizing and reducing environments. The results show that all configurations provide excellent corrosion resistance at temperatures up to 600°C, with the gas-shielded FCAW configuration showing slightly superior performance due to the lower dilution ratio and more uniform alloy composition. Above 600°C, the corrosion resistance becomes more sensitive to the carbide distribution, with finer carbides providing better protection against intergranular corrosion.

Engineering Practice Implications

The findings of this study have direct implications for the selection of welding materials in UMCo50 overlay applications. For applications requiring maximum wear resistance at room temperature, high-silica fluxes in SAW provide the optimal combination of hardness and carbide distribution. For applications requiring high-temperature strength and creep resistance, gas-shielded FCAW or low-sodium flux SAW configurations are preferred. For applications requiring a balance of wear resistance, corrosion resistance, and high-temperature performance, medium-sodium flux SAW provides a satisfactory compromise.

Summary and Technical Recommendations

The systematic study of welding material effects on UMCo50 overlay layer properties confirms that the selection of filler metal, flux, and shielding gas is a critical process variable that must be optimized for the specific service conditions of the application. The microstructural evolution of the overlay layer, characterized by the type, size, and distribution of carbide precipitates, is the primary mechanism governing both the mechanical properties and the high-temperature performance. Engineers selecting welding materials for UMCo50 overlay applications should carefully consider the temperature range, loading conditions, and environmental exposure of the service application, and select the welding material configuration that provides the optimal balance of properties for the specific application requirements.