Author/Authors :
Ivetic، نويسنده , , Goran and Meneghin، نويسنده , , Ivan and Troiani، نويسنده , , Enrico and Molinari، نويسنده , , Gianluca and Ocaٌa، نويسنده , , José and Morales، نويسنده , , Miguel and Porro، نويسنده , , Juan and Lanciotti، نويسنده , , Agostino and Ristori، نويسنده , , Vjola and Polese، نويسنده , , Claudia and Plaisier، نويسنده , , Jasper and Lausi، نويسنده , , Andrea، نويسنده ,
Abstract :
An experimental study was performed in order to determine the influence of the sequence of operations on the effectiveness of Laser Shock Peening (LSP) treatment in increasing the fatigue performances of open-hole aluminium specimens.
al stress measurements, fractographic analysis and FEM analysis were performed, indicating the presence of compressive residual stresses on the surface of the treated specimens and tensile residual stresses in the mid-section along the thickness of the specimens. Negative effects on fatigue lives were encountered on the specimens with the hole already present, while positive effect were observed in specimens in which the hole was drilled after LSP treatment.
results indicate that LSP can be a good solution for “in production” application, in which open holes are to be drilled after the LSP treatment. The application in which LSP is used “in service” on structures with pre-existing cut-outs, has proven to be impracticable in the investigated configuration.
Keywords :
Laser shock peening , Fatigue , Synchrotron X-ray diffraction , Finite element method , Aluminium alloys