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Microstructure Evolution and Mechanical Properties of 20%SiC(p)/Al Joint Prepared via Laser Welding

SiC particles-reinforced Al matrix composites (SiC(p)/AMCs) have been widely used in the aerospace structural components. In this work, 20 vol% SiC(p)/2A14 joint was fabricated by laser welding technology. The effects of different laser power/welding velocity on the 20 vol% SiC(p)/2A14 joint forming...

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Detalles Bibliográficos
Autores principales: Li, Fei, Jiang, Yiming, Mi, Gaoyang, Zhang, Mingyang, Wang, Chunming
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9457176/
https://www.ncbi.nlm.nih.gov/pubmed/36079430
http://dx.doi.org/10.3390/ma15176046
Descripción
Sumario:SiC particles-reinforced Al matrix composites (SiC(p)/AMCs) have been widely used in the aerospace structural components. In this work, 20 vol% SiC(p)/2A14 joint was fabricated by laser welding technology. The effects of different laser power/welding velocity on the 20 vol% SiC(p)/2A14 joint forming, microstructure evolution and mechanical properties were studied in detail. The results showed that, under the same heat input, the high power/high welding velocity was beneficial to reduce the porosity of SiC(p)/2A14 joint and inhibited the formation of brittle phase of Al(4)C(3). At 8 kW-133 mm/s welding parameters, the maximum tensile strength of the SiC(p)/2A14 joint reached 199 MPa, which is ~64% higher than that of the SiC(p)/2A14 joint prepared at 4 kW-66 mm/s welding parameters. By analyzing the fracture morphology and SEM image of SiCp/2A14 joint section, it is was found that the porosity of weld and Al(4)C(3) brittle phase were the important factors limiting the strength of SiCp/2A14 joint. This work provides a reference for the process window design of laser welding SiC(p)/2A14 composites.