Technical Progress of Laser Cladding Composite Powders and Ceramic Coatings

Jun 16, 2025 Leave a message

​Technical Progress of Laser Cladding Composite Powders and Ceramic Coatings

 

 

With the continuous improvement of material performance requirements in aerospace and energy equipment, traditional single-material systems can no longer meet the needs. Composite powder and ceramic coating technology, through the collaborative design of "metal toughness + ceramic hardness", is breaking through the performance limits of laser cladding technology. This paper systematically expounds the latest progress in this field from material design, process optimization to engineering verification.

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Strengthening Mechanism of Composite Powders

Coated powders use a core-shell structure to solve the oxidation problem of carbides. In typical Ni-coated WC powders, a 5-15μm nickel shell forms a (W,Ni) solid solution transition layer under laser action, reducing the carbon loss rate from 28% in mechanical mixing to below 5%. The more advanced in-situ synthesis technology uses the Ti+C→TiC reaction. When the power density >3×10⁴ W/cm², 50-100nm TiC particles can be obtained. A bearing ring application of this technology reduced the wear rate to 1.8×10⁻⁶ mm³/N·m.

Performance Comparison of Carbide-reinforced Systems

 

Comparison tests show that the interfacial bonding strength of coated powders reaches 580 MPa, an increase of 65% compared with mechanical mixing. Particle size distribution design is particularly critical: 50-150μm coarse particles bear the main load, and 5-20μm fine particles fill the gaps. A steam turbine blade using the Ni60+35%WC (coated type) scheme extended its service life from 8,000 hours to 15,000 hours, verifying the engineering value of this technology.

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Preparation Challenges of Ceramic Coatings

Zirconia gradient coatings reduce thermal stress by 60% through transitional design from metal→70% metal+30% ceramic→pure ceramic. Process parameter optimization shows that a power of 2-4kW with a scanning speed of 5-15mm/s and a lap rate of 30-50% can make the crack density <0.5 pieces/mm. An aero-engine combustor applied with this technology has a thermal cycle life of 3,000 times (the original technology only had 800 times).

Breakthroughs in Biomedical Applications

 

Hydroxyapatite (HAP) coatings increase crystallinity (XRD half-peak width 0.38°→0.25°) through 3%F⁻ substitution, and adding 3%MgO promotes osteoblast adhesion. Animal experiments show that the bone integration time of the modified FHA coating is shortened to 8 weeks (original 12 weeks), and the interfacial bonding strength reaches 35 MPa. This technology has been applied to clinical trials of dental implants with an initial success rate of 98.5%.

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Core Components of laser Cladding System
 
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Laser cladding Head
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fiber laser machine
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powder feeder
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laser water chiller

 

Conclusion

 

Composite coating technology faces three major research directions: ①developing a multi-scale collaborative strengthening theoretical model; ②establishing service performance evaluation standards (such as thermal shock test methods); ③reducing the preparation cost of coated powders. It is recommended to form an "industry-university-research-medical" consortium to focus on breaking through bottleneck technologies such as Ta coatings for cardiovascular stents and ZrO₂-HAP gradient materials for artificial joints.