Research on the residual stress distribution of aircraft engine blades repaired by laser shock peening and laser cladding composite process
The traditional laser cladding (LC) repair process for aircraft blades introduces residual tensile stress near the heat affected zone, which causes a decrease in the strength of the joint interface of the repaired part. This study proposes laser shock peening (LSP) before LC to improve the residual...
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| Главные авторы: | , , , , |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
EDP Sciences
2025-01-01
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| Серии: | MATEC Web of Conferences |
| Предметы: | |
| Online-ссылка: | https://www.matec-conferences.org/articles/matecconf/pdf/2025/02/matecconf_iddrg2025_01083.pdf |
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