The effects of laser shock processing (LSP) on the fatigue crack properties of Ti-17 titanium alloy are investigated. Surfaces on either side of a fatigue slot are subjected to LSP. The residual stress of the irradiated surface is measured by x-ray diffraction measurement and fatigue crack growth testing of the treated and untreated specimens. The fatigue fracture morphology and microstructure are examined by scanning electron microscopy and transmission electron microscopy. Proliferation and tangles of dislocations occur in the Ti-17, and the density of dislocation increases after the LSP treatment. The fine spacing of the fatigue striations indicates that LSP produces residual compressive stress on the irradiated surfaces which can delay ...
Laser shock peening (LSP) has been employed to improve the mechanical properties of repaired aerospa...
High cycle fatigue failure of titanium alloy components on the aircraft is a serious problem that af...
International audienceDuring operation, a turbojet can swallow foreign objects (birds, fragments, et...
The effects of laser shock processing (LSP) on the fatigue crack properties of Ti-17 titanium alloy ...
Ti-17 titanium alloy was treated by laser shock processing (LSP) and the high-frequency fatigue prop...
AbstractLaser shock peening (LSP) is an innovative surface treatment method, which has been shown to...
The work is devoted to experimental investigation of the laser shock peening (LSP) effect on fatigue...
Laser peening is an innovative surface treatment technique, and can significantly improve the mechan...
Laser shock processing (LSP) is increasingly applied as an effective technology for the improvement ...
In order to study the effect of laser shock processing (LSP) on mechanical properties of Ti-45.5Al-2...
Laser shock peening (LSP), an innovative surface treatment technique, generates compressive residual...
Laser shock peening is one of the best method to enhance the mechanical and fatigue properties of ti...
The effects of laser shock processing without protective coating on high-cycle fatigue crack growth ...
Ti-6Al-4V (Ti-64) simulated airfoils were laser shock processed with two laser power densities (4 an...
Laser shock peening (LSP) has been employed to improve the mechanical properties of repaired aerospa...
High cycle fatigue failure of titanium alloy components on the aircraft is a serious problem that af...
International audienceDuring operation, a turbojet can swallow foreign objects (birds, fragments, et...
The effects of laser shock processing (LSP) on the fatigue crack properties of Ti-17 titanium alloy ...
Ti-17 titanium alloy was treated by laser shock processing (LSP) and the high-frequency fatigue prop...
AbstractLaser shock peening (LSP) is an innovative surface treatment method, which has been shown to...
The work is devoted to experimental investigation of the laser shock peening (LSP) effect on fatigue...
Laser peening is an innovative surface treatment technique, and can significantly improve the mechan...
Laser shock processing (LSP) is increasingly applied as an effective technology for the improvement ...
In order to study the effect of laser shock processing (LSP) on mechanical properties of Ti-45.5Al-2...
Laser shock peening (LSP), an innovative surface treatment technique, generates compressive residual...
Laser shock peening is one of the best method to enhance the mechanical and fatigue properties of ti...
The effects of laser shock processing without protective coating on high-cycle fatigue crack growth ...
Ti-6Al-4V (Ti-64) simulated airfoils were laser shock processed with two laser power densities (4 an...
Laser shock peening (LSP) has been employed to improve the mechanical properties of repaired aerospa...
High cycle fatigue failure of titanium alloy components on the aircraft is a serious problem that af...
International audienceDuring operation, a turbojet can swallow foreign objects (birds, fragments, et...