2016
DOI: 10.3390/met6120297
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Nanocrystallization in the Duplex Ti-6Al-4V Alloy Processed by Multiple Laser Shock Peening

Abstract: Laser shock peening of titanium alloys has been widely applied in the aerospace industry. However, little is known of the nanocrystalline formation characteristics and mechanisms. In this investigation, a nanocrystalline layer was formed in the duplex Ti-6Al-4V titanium alloy surface region by means of multiple pulsed laser shock peening (LSP). The phase transition and residual stress characteristics of LSP samples were analyzed with X-ray diffraction (XRD) and scanning electron microscopy (SEM). Transmission … Show more

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Cited by 25 publications
(23 citation statements)
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“…An example is shown here by Zhou et al [3] of microstructural modifications at the nanoscale range obtained on a Ti-6Al-4V (α + β) titanium alloy. Using the Scherrer-Wilson method for analyzing X-ray diffraction peak broadening, microstrains and average grain sizes of laser-peened diffracting zones were estimated and subjected to TEM microstructural observations.…”
Section: Lsp-induced Nano-recrystallization Effectsmentioning
confidence: 99%
See 2 more Smart Citations
“…An example is shown here by Zhou et al [3] of microstructural modifications at the nanoscale range obtained on a Ti-6Al-4V (α + β) titanium alloy. Using the Scherrer-Wilson method for analyzing X-ray diffraction peak broadening, microstrains and average grain sizes of laser-peened diffracting zones were estimated and subjected to TEM microstructural observations.…”
Section: Lsp-induced Nano-recrystallization Effectsmentioning
confidence: 99%
“…They provide interesting insights into the beneficial effects of temperature on laser-shock-induced plastic deformations. Considering LSP temperature ranges up to 160 • C and a 6061 (Al0.9Mg0.6Si) alloy, warm laser peening (WLP) trials were carried out with 2 mm diameter impacts, a 50% overlap, and a glass confining medium [3]. Such WLP trials evidence a 20% decrease of surface compressive stresses, but deeper affected layers and large hardening effect (up to +55% HV for a WLP at 130 • C).…”
Section: Warm Laser Peening Applied To Aluminum Alloysmentioning
confidence: 99%
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“…This generally results in high residual tensile stress on the surface [2,3], which is not conducive to the improvement of fatigue life. Laser shock peening at room temperature (RT-LSP) has been proved to be an effective technology to improve the fatigue resistance of materials by the high compressive residual stress (CRS) [4,5].…”
Section: Introductionmentioning
confidence: 99%
“…These materials commonly exhibit excellent properties, such as high strength to weight ratio, excellent toughness, and outstanding corrosion resistance [1,2]. TC17 titanium alloy has been widely used to manufacture aero-engine fans, compressor disks, jetengine blades, and other important parts of advanced aircrafts [3,4].…”
Section: Introductionmentioning
confidence: 99%