초록 ▼

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

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.

대표청구항 ▼

The invention claimed is: 1. A method of treating a metal component comprising at least a first zone treated by putting layers beneath the surface thereof in compression, wherein said first zone comprises at least a first layer put in compression by shot peening and a deeper subjacent second layer

The invention claimed is: 1. A method of treating a metal component comprising at least a first zone treated by putting layers beneath the surface thereof in compression, wherein said first zone 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, said method comprising a first treatment step of treating said first zone by shot peening, followed by a second treatment step of treating said first zone by laser shock peening, wherein said second treatment step comprises performing a first scan of the first zone with a laser beam thereby forming a plurality of first laser impact spots on the first zone such that the first zone is subject to both shot peening and laser shock peening, and wherein said first laser impact spots do not overlap each other. 2. the method as claimed in claim 1, wherein said second treatment step further comprises performing a second scan of the first zone with the laser beam thereby forming a plurality of second laser impact spots on the first zone, wherein said second laser impact spots do not overlap each other but overlap said first laser impact zones. 3. The method as claimed in claim 1, wherein said first and second treatment steps are performed so to produce a same level of residual compressive stresses in said first and second layers. 4. The method as claimed in claim 1, wherein the shot peening is an ultrasonic peening. 5. The method as claimed in claim 1, wherein both said first zone and a second zone different than the first are treated by shot peening, and then only the first zone is treated by laser shock peening. 6. The method as claimed in claim 5, wherein said first and second zones are adjacent. 7. The method as claimed in claim 1, wherein the first layer has a thickness of 0.2 to 0.3 mm. 8. The method as claimed in claim 7, wherein the residual stresses of the first layer are between 500 and 700 MPa.