A parametric study of laser spot size and coverage on the laser shock peening induced residual stress in thin aluminium samples
- Author(s): M. Sticchi 1 ; P. Staron 1 ; Y. Sano 2 ; M. Meixer 3 ; M. Klaus 3 ; J. Rebelo-Kornmeier 4 ; N. Huber 1 ; N. Kashaev 1
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View affiliations
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Affiliations:
1:
Helmholtz-Zentrum Geesthacht, Institute of Materials Research , Max-Planck-Straße 1, D-21502 Geesthacht , Germany ;
2: Toshiba Corporation , Power and Industrial Systems Research and Development Center, 8 Shinsugita-cho , Isogo-ku, 235-8523 Yokohama , Japan ;
3: Helmholtz-Zentrum Berlin , Department of Microstructure and Residual Stress Analysis , Hahn-Meitner-Platz 1, D-14109 Berlin , Germany ;
4: Heinz Maier-Leibnitz Zentrum (MLZ), Technische Universität München , Lichtenbergstr. 1, 85748 Garching , Germany
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Affiliations:
1:
Helmholtz-Zentrum Geesthacht, Institute of Materials Research , Max-Planck-Straße 1, D-21502 Geesthacht , Germany ;
- Source:
Volume 2015, Issue 13,
May
2015,
p.
97 – 105
DOI: 10.1049/joe.2015.0106 , Online ISSN 2051-3305
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Laser Shock Peening is a fatigue enhancement treatment using laser energy to induce compressive Residual Stresses (RS) in the outer layers of metallic components. This work describes the variations of introduced RS-field with peen size and coverage for thin metal samples treated with under-water-LSP. The specimens under investigation were of aluminium alloy AA2024-T351, AA2139-T3, AA7050-T76 and AA7075-T6, with thickness 1.9 mm. The RS were measured by using Hole Drilling with Electronic Speckle Pattern Interferometry and X-ray Diffraction. Of particular interest are the effects of the above mentioned parameters on the zero-depth value, which gives indication of the amount of RS through the thickness, and on the value of the surface compressive stresses, which indicates the magnitude of induced stresses. A 2D-axisymmetrical Finite Element model was created for a preliminary estimation of the stress field trend. From experimental results, correlated with numerical and analytical analysis, the following conclusions can be drawn: increasing the spot size the zero-depth value increases with no significant change of the maximum compressive stress; the increase of coverage leads to significant increase of the compressive stress; thin samples of Al-alloy with low Hugoniot Elastic Limit (HEL) reveal deeper compression field than alloy with higher HEL value.
Inspec keywords: laser materials processing; shot peening; finite element analysis; stress analysis; elasticity; fatigue; compressive strength; electronic speckle pattern interferometry; X-ray diffraction; internal stresses; aluminium alloys
Other keywords: peen size; HEL value; spot size; fatigue enhancement treatment; outer layers; stress field; analytical analysis; AA2139-T3 aluminium alloy; numerical analysis; under-water-LSP; compression field; laser energy; compressive residual stresses; RS-field; induced stress magnitude; surface compressive stresses; laser shock peening induced residual stress; AA7050-T76 aluminium alloy; electronic speckle pattern interferometry; AA2024-T351 aluminium alloy; metallic components; RS measurement; thin-aluminium metal; AA7075-T6 aluminium alloy; zero-depth value; 2D-axisymmetrical finite element model; Hugoniot elastic limit; X-ray diffraction; compressive stress; hole drilling; laser spot size
Subjects: Elasticity (mechanical engineering); Finite element analysis; Laser materials processing; Numerical approximation and analysis; Surface treatment and coating techniques; Engineering materials; Laser materials processing; Fracture mechanics and hardness (mechanical engineering); Numerical analysis; Plasticity (mechanical engineering)
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