Authors: X.J. Cao, Luo Peng Xu, Chong Wang, Jiang Jin, Qingyuan Wang
Abstract: In order to investigate the effect of shot peening on the long life fatigue properties of Ti6Al4V (TC4), ultrasonic fatigue tests were performed with a frequency of 20 kHz. According to different heat treatment, two groups of specimens were surface modified by shot peening with an Almen intensity of 0.10 mmA~ 0.15 mmA and an overlapping rate of 100%. One group was stress-relief annealed at 650 °C, and the other was then treated with solution-aging. With the shot peening, both the depth of the residual stress layer and the maximum compressive residual stress are increased. Surface hardness is also increased. The fatigue strength is increased, but enhancement is no more than 5% because of the increase of surface roughness. Noticeably, all of the TC4 specimens after shot peening show inner crack initiations. Oxide inclusion is always the core of cracks, and the small crack propagation in crack initiation area acts as the slip of α-phase.
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Authors: Zhi Yong Huang, Chong Wang, Qingyuan Wang
Abstract: Very high cycle fatigue is often implemented with high test frequency to save time. The thermal dissipation accompanied with the high frequency appears and induces the temperature increment in the speicmen’s surface. The dissipation power is important and closely related with VHCF performance. The infrared camera is used to acquire the temperature distribution and evolution with a lot noisy which bring difficulties for the calculation. In the article, a thermal dissipation power calculation with time and space filtering method is proposed to give out the thermal dissipation. The two stages dissipation phenomenon with large difference is found out in the process of VHCF test.
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Authors: Antoine Blanche, Chong Wang, Ngoc Lam Phung, Nicolas Ranc, Véronique Favier, Danièle Wagner, Claude Bathias, André Chrysochoos
Abstract: This paper aims at a deeper understanding of microplastic mechanisms leading to crack initiation in ductile metals in Very High Cycle Fatigue (VHCF). Fatigue tests were conducted using an ultrasonic technique at loading frequency of 20 kHz. The microplastic mechanisms are revealed via observations of slip markings at the specimen surface and self-heating measurements due to intrinsic dissipation. Pure copper and Armco iron (which contains a very low amount of carbon) were investigated. Both are single-phase ductile materials but the crystallographic structure of copper is face-centered cubic while it is body centered cubic for Armco iron. A good correlation was found between slip markings initiation and dissipation for both materials. The dissipation for both materials is of the same order of magnitude but the location, the morphology and the evolution over cycles of slip markings were found different.
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Authors: Chong Wang, Danièle Wagner, Claude Bathias
Abstract: Pariss law of fatigue crack propagation rate is well applied in the defect-tolerance fatigue approach. When carry out same approach in the very high cycle fatigue domain, the understanding of mechanism about fatigue crack propagation threshold which is obviously important, is helped. In the present work here, the fatigue crack propagation threshold of a surface crack for an Armco iron loaded in the VHCF regime was investigated by a new approach which combines the fracture surface analysis and the temperature recording on the surface during the test by an infra-red camera. The experiments were carried out on a sheet specimen under a 20 kHz ultrasonic frequency loading with IR images registration. Three stages of fatigue crack were identified with different mechanisms. It is found that the transition between initiation and crack propagation corresponds to the intrinsic fatigue threshold. It takes more than 99% of the gigacycle fatigue life to achieve this transition size.
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Authors: Tang Li, Qing Yuan Wang, Q.F. Dou, Chong Wang, M.R. Sriraman
Abstract: Very high cycle fatigue (VHCF) properties of high-pressure die cast Magnesium alloy
AZ91HP have been investigated. Ultrasonic fatigue tests up to 109 cycles were conducted at the
loading frequency of 20 kHz, under R=-1 condition and in ambient air. The experimental results
show that specimens fail even after 107 cycles although the scatter seems to be large probably due
to the presence of materials defects. However, there seems to be a fatigue limit at about 109 cycles.
The fractures contain typical brittle features, with the fatigue cracks seen to initiate from the
porosity in the material, either from the surface or beneath.
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