scispace - formally typeset
Search or ask a question
Topic

Fatigue limit

About: Fatigue limit is a research topic. Over the lifetime, 20489 publications have been published within this topic receiving 305744 citations. The topic is also known as: endurance limit & fatigue strength.


Papers
More filters
Journal ArticleDOI
TL;DR: The results of this study revealed endurance limits for Ti- 6Al -4V alloy tested with a rotating beam system and the low-endurance limit of the porous-coated material is due to both the transition from the as-received equiaxed microst structure to a lamellar microstructure upon sintering and to the notch effect created by the porous coating.
Abstract: A porous metal coating applied to a solid substrate implant has been shown, in vivo, to offer advantages over current polymethylmethacrylate cement fixation in orthopedic devices. These advantages may be lost, however, in devices requiring a sintering heat treatment to apply the coating since these treatments may have a detrimental effect on the substrate material mechanical properties. In addition, more biocompatible interface coating materials have come of interest with recent literature reports of metal ion release. These coatings may be of particular use in porous-coated systems since the surface area of implant in contact with the surrounding tissues is greatly increased. This study investigated the effects that both a porous Ti- 6Al -4V alloy coating and a ULTI carbon coating have on the fatigue properties of a Ti- 6Al -4V alloy substrate system. The fatigue properties of uncoated as-received, uncoated sinter heat treated and notched Ti- 6Al -4V material were also investigated. The results of this study revealed endurance limits for Ti- 6Al -4V alloy tested with a rotating beam system of 617 MN/m2 (uncoated as-received), 624 MN/m2 ( ULTI carbon-coated), 377 MN/m2 ( sinter heat treated), 220 MN/m2 (notched) and 138 MN/m2 (porous-coated). No effects on fatigue properties were observed when testing the material in saline compared with air. The slight increase in fatigue strength for the carbon-coated material is thought to be due to the increase in surface hardness resulting from the formation of titanium carbides on the surface. The low-endurance limit of the porous-coated material is due to both the transition from the as-received equiaxed microstructure to a lamellar microstructure upon sintering and to the notch effect created by the porous coating.

91 citations

Journal ArticleDOI
TL;DR: In this article, the role of foreign-object damage and its effect on high-cycle fatigue (HGF) failures in a turbine engine Ti-6Al-4V alloy is examined in the context of the use of the Kitagawa-Takahashi diagram to describe the limiting conditions for such failures.

90 citations

Journal ArticleDOI
TL;DR: In this article, the effect of strain rate on the cyclic loading tests was investigated and the applicability of a constant life diagram (CLD) model to determine the fatigue limit of the alloy for different stress ratios (R).

90 citations

Journal ArticleDOI
TL;DR: In this article, the authors proposed a fracture mechanics approach to assess the fatigue life of a nodular cast iron containing casting defects, which takes into account the position and size of the defect, short crack behavior and the notch effect introduced by the defect.
Abstract: The fatigue behaviour of a a nodular cast iron containing casting defects has been investigated in the high-cycle fatigue regime. In this paper, we propose a fatigue life assessment model for flawed materials based on a fracture mechanics approach which takes into account the position and size of the defect, short crack behaviour and the notch effect introduced by the defect. The fatigue behaviour of smooth samples, and long and short crack behaviour have been experimentally determined in order to identify the relevant mechanical parameters; these being introduced into the model. An experimental study has been made both in air and in vacuum in order to account for the position of the defect, noting that internal defects are supposed to be under vacuum conditions. Experimental results, which are based on a two-crack front-marking technique specially developed for this study, show that the propagation of natural cracks is controlled by the effective stress intensity factor in air as well as in vacuum. The K calculation for a short crack in the stress field of a notch is analysed using numerical clastic-plastic results. Comparison between experimental results and the computation of fatigue life for fatigue lives less than 10 6 cycles shows that the fatigue behaviour of nodular cast iron is controlled by a propagation process. The model proposed is thus relevant for fatigue lives less than 10 6 cycles so that the defect can be considered as a crack and the initiation stage neglected. Closer to the fatigue limit, this study shows that the initiation stage should be considered in the assessment of fatigue life of nodular cast iron, because a single macroscopic propagation assessment is not enough to describe the whole fatigue life. The defect cannot be considered as a pre-existent crack in the high-cycle fatigue range (> 10 6 cycles), and the initiation stage that contains microcrack propagation around the defect should be evaluated when assessing the high-cycle fatigue life of nodular cast iron.

90 citations


Network Information
Related Topics (5)
Fracture mechanics
58.3K papers, 1.3M citations
91% related
Ultimate tensile strength
129.2K papers, 2.1M citations
88% related
Welding
206.5K papers, 1.1M citations
86% related
Alloy
171.8K papers, 1.7M citations
85% related
Microstructure
148.6K papers, 2.2M citations
84% related
Performance
Metrics
No. of papers in the topic in previous years
YearPapers
2023248
2022586
2021616
2020684
2019749
2018712