2015
DOI: 10.1016/j.surfcoat.2015.05.014
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Fatigue and wear properties of Ti–6Al–4V alloy with Cr/CrN multilayer coating

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Cited by 65 publications
(14 citation statements)
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“…It can be seen that the wear mechanism was corrosion wear at the wear loads of 0.5 and 1.0 N. There were strip-worn tracks and small scaly flakes on the worn tracks at the wear load of 1.5 N, as shown in Figure 9 c. The new abrasive particles were always produced in the wear process, and ground the Al coating to form the striped furrows on the Al coating surface, causing the Al particles on the Al coating surface to fall off; the wear mechanism was abrasive wear [ 32 ]. Due to the stress concentration at the contact point between the Al coating surface and the ceramic ball, the fatigue cracks and worn debris appeared under the action of circular stress, and such cracks mainly appeared in the form of scaly flakes, at the same time, the hardness of worn track increased, resulting in fatigue wear [ 33 , 34 , 35 ]. There were flaky debris appearing on the worn track, and the hardness on the worn track was 71.10 HV, larger than the Al coating surface, which was the specific feature of fatigue wear.…”
Section: Analysis and Discussion Of Resultsmentioning
confidence: 99%
“…It can be seen that the wear mechanism was corrosion wear at the wear loads of 0.5 and 1.0 N. There were strip-worn tracks and small scaly flakes on the worn tracks at the wear load of 1.5 N, as shown in Figure 9 c. The new abrasive particles were always produced in the wear process, and ground the Al coating to form the striped furrows on the Al coating surface, causing the Al particles on the Al coating surface to fall off; the wear mechanism was abrasive wear [ 32 ]. Due to the stress concentration at the contact point between the Al coating surface and the ceramic ball, the fatigue cracks and worn debris appeared under the action of circular stress, and such cracks mainly appeared in the form of scaly flakes, at the same time, the hardness of worn track increased, resulting in fatigue wear [ 33 , 34 , 35 ]. There were flaky debris appearing on the worn track, and the hardness on the worn track was 71.10 HV, larger than the Al coating surface, which was the specific feature of fatigue wear.…”
Section: Analysis and Discussion Of Resultsmentioning
confidence: 99%
“…In order to prevent the corrosion of studs, an electrodeposited coating of cadmium or zinc-nickel is essential for oil and gas applications, to improve wear and corrosion properties [1,2]. However, coatings influence the fatigue behavior of components [3,4]. Although surface treatments may have some positive impacts on the fatigue strength, such as high mechanical strength, compressive residual stresses, and good adhesion, the coatings frequently reduce the fatigue life of components through the effect on the fatigue crack initiation period [5,6].…”
Section: Introductionmentioning
confidence: 99%
“…[19][20][21][22] However, the influence and its mechanism of texture patterns on the anti-wear performance or tribological behavior of GCI parts under dry sliding are still unclear, especially when the surface texturing combines with Zr/ZrN composite coatings. [23][24][25][26][27][28][29][30] Therefore, based on previous publications on the wear performance of pits textured GCI parts, 31,32 the same GCI ring model with linearly distributed pits in the radial direction (LDRD) was introduced in this work. The pits texture GCI rings with Zr/ZrN coatings were prepared sequentially by laser marking system and PVD equipment.…”
Section: Introductionmentioning
confidence: 99%