Microstructure and Properties of ZrB2-SiC Reinforced Copper Matrix Composite Coatings Prepared by Laser Cladding

• Published in: Materials Vol. 15; no. 19; p. 6777
• Main Authors: Zhao, Yuehong, Zhan, Zaiji, Lv, Xiangzhe, Cao, Haiyao
• Format: Journal Article
• Language: English
• Published: Basel MDPI AG 30.09.2022; MDPI
• Subjects: Ablation; Abrasive wear; Boron carbide; Chemical reactions; Composite materials; Continuous coating; Copper; Energy; High temperature; in-situ synthesis; Laser beam cladding; laser cladding; Lasers; Metal matrix composites; Microhardness; Microstructure; Morphology; Protective coatings; Refractory materials; Reinforcement; Silicon carbide; Substrates; Surface hardness; Synthesis; Titanium alloys; wear; Wear mechanisms; Wear rate; Wear resistance; Zirconium compounds; ZrB2-SiC; Beijing China; China
• ISSN: 1996-1944; 1996-1944
• DOI: 10.3390/ma15196777

With the use of electrolytic Cu powder, Zr powder, Si powder and nickel-coated B4C powder as cladding powders, in-situ synthesized ZrB2-SiC reinforced copper matrix composite coatings were prepared by laser cladding on the surface of the copper substrate to improve the surface hardness and wear resistance. Under the condition of a laser energy density at 60 kJ/cm2, the macroscopic surface of the composite coating was continuously flat. The microstructure and phase of the cladding coating were analyzed by means of XRD and SEM. The reinforcements with nano-scale particle and micron-scale needle-like structures were in-situ synthesized in the cladding coating, and the content of the reinforcement phase decreased slightly from the coating surface to the substrate. The phase analysis results showed that the reinforcements included ZrB2 and SiC. When the content of the reinforcement was increased to 30 wt%, microhardness also increased from 48 HV0.2 to 309 HV0.2, which was about 5.6 times that of the copper matrix. The wear resistance of the composite coatings was characterized by current-carrying wear tests. By keeping the sliding speed and load constant, the wear rate decreased with an increase in the reinforcement content, and the wear mechanism changed from adhesive wear to abrasive wear. The wear rate of the composite coating with the current was higher than that without the current due to its electric ablation and high temperature.