2017
DOI: 10.1016/j.wear.2016.12.004
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Investigation on the fretting fatigue behaviors of Ti-6Al-4V dovetail joint specimens treated with shot-peening

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Cited by 48 publications
(27 citation statements)
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“…Due to the formation of a hardening layer on the surface of USRP-treated samples, the surface local yield strength is also improved. Enhanced surface yield strength can improve the stress concentration resistance of metallic materials [38]. Therefore, the surface of a USRP-treated sample has a lower stress concentration at the contact edge than that of the untreated sample.…”
Section: Fretting Fatigue Testmentioning
confidence: 99%
“…Due to the formation of a hardening layer on the surface of USRP-treated samples, the surface local yield strength is also improved. Enhanced surface yield strength can improve the stress concentration resistance of metallic materials [38]. Therefore, the surface of a USRP-treated sample has a lower stress concentration at the contact edge than that of the untreated sample.…”
Section: Fretting Fatigue Testmentioning
confidence: 99%
“…If the components undergo an oscillatory force, the cracks will propagate through the material that can lead to fatigue failure. This phenomenon is common in bolt and riveted joints, spline coupling, shrink‐fit connections, and dovetail joints …”
Section: Introductionmentioning
confidence: 99%
“…This phenomenon is common in bolt and riveted joints, 2 spline coupling, 3 shrink-fit connections, 4 and dovetail joints. 5 Many researchers have focused on fretting fatigue and have endeavoured to reveal different aspects of this NOMENCLATURE: _ γ α ð Þ , slipping rate; _ a, reference strain rate; D L , small grain size; D mean , mean grain size; D R , large grain size; d reg , seed spacing in regular tessellation; F * , stretching and rotation; F P , plastic deformation; g (α) , current strength of the α slip system; g ∾ , saturation stress; g 0 , critical resolved shear stress; h 0 , initial hardening modulus; h αβ , slip hardening modulus; L P , plastic velocity gradient; m (α) , normal to slip plane unit vector; p crit , critical accumulated plastic slip; p cyc , stabilized accumulated plastic slip; P r , percentage of grains within the range; s (α) , slip direction unit vector; τ (α) , resolved shear stress on α slip system; F, deformation gradient; n, rate sensitivity exponent; N, fatigue life; p, accumulated plastic slip; α, slip system index; δ, minimum seed spacing; λ, regularity parameter phenomenon. Wharton and Waterhouse 6 examined the effect of different pad materials on the fretting fatigue strength of Al-4Mg-0.7Mn alloy.…”
Section: Introductionmentioning
confidence: 99%
“…Yang et al studied the shot-peening effects on dovetail specimens’ joints of Ti-6Al-4V fretting fatigue behavior. It was reported that shot-peening altered the crack initiation mechanisms and enhanced the fretting fatigue performance for the titanium alloy [ 31 ]. Dissimilar TIG-welded joints of magnesium and titanium alloys were also subjected to high-energy shot-peening and the microstructure and mechanical properties in terms of tensile strength were evaluated by Chuan Xu et al [ 32 ].…”
Section: Introductionmentioning
confidence: 99%