Metal component treated by putting sublayers in compression, and method of obtaining such a component

The invention relates to a metal component comprising at least a first zone treated by putting layers beneath the surface thereof in compression. It is characterized in that it comprises at least a first layer put in compression by shot peening and a deeper subjacent second layer put in compression...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: VIGNEAU JOEL OLIVIER ALFRED ABEL
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:The invention relates to a metal component comprising at least a first zone treated by putting layers beneath the surface thereof in compression. It is characterized in that it comprises at least a first layer put in compression by shot peening and a deeper subjacent second layer put in compression by laser shock peening. The component may be a turbomachine blade. According to the method, said zone is firstly treated by prestress shot peening followed by compression treatment by laser shock peening.