Laser-shock processing effects on mechanical properties of Ti-6Al-4V alloy
LU Jin-zhon
Abstract
LU Jin-zhon
Abstract
In this paper,laser shock processing technology was employed on Ti6AI4V and the change of mechani- cal properties was investigated.The experiments show that a uniform hardened layer with the thickness of al- most 0.25mm and hardness of 510Hv is obtained on the Ti6Al4V surface when we select proper technologic pa- rameters in laser shock processing.The influence of laser power density on residual stress in the titanium alloy was analyzed and it is found that the higher laser power density,the greater compressive residual stresses at the surface of the sample were obtained.The maximal compressive residual stresses at the surface of the sample is a- bout—264MPa and the distribution of the residual stresses below the surface increased to lmm,which are valu- able effects to aeronautic titanium alloy.With the increase of laser densities,the material tensile strength and hardness in shocked area increase,while the plastic property decreases.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
In this paper,laser shock processing technology was employed on Ti6AI4V and the change of mechani- cal properties was investigated.The experiments show that a uniform hardened layer with the thickness of al- most 0.25mm and hardness of 510Hv is obtained on the Ti6Al4V surface when we select proper technologic pa- rameters in laser shock processing.The influence of laser power density on residual stress in the titanium alloy was analyzed and it is found that the higher laser power density,the greater compressive residual stresses at the surface of the sample were obtained.The maximal compressive residual stresses at the surface of the sample is a- bout—264MPa and the distribution of the residual stresses below the surface increased to lmm,which are valu- able effects to aeronautic titanium alloy.With the increase of laser densities,the material tensile strength and hardness in shocked area increase,while the plastic property decreases.
Key concepts: Materials science, Residual stress, Titanium alloy, Shock (circulatory), Ultimate tensile strength, Laser, Alloy, Composite material