2023
DOI: 10.3390/app13148308
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Cyclic Hardening and Fatigue Damage Features of 51CrV4 Steel for the Crossing Nose Design

Abstract: A crossing nose is a component of railway infrastructure subject to very severe loading conditions. Depending on the severity of these loads, the occurrence of structural fatigue, severe plastic deformation, or rolling fatigue may occur. Under fatigue conditions with high plastic deformation, cyclic plasticity approaches, together with local plasticity models, become more viable for mechanical design. In this work, the fatigue behavior in strain-controlled conditions of 51CrV4 steel, applicable to the crossing… Show more

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Cited by 4 publications
(5 citation statements)
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“…The material and mechanical properties relevant to strain life curves used to determine the observed landing gear leg RUL made from a 6150 steel alloy, also referred to as the 51CrV4 steel alloy, were determined through rigorous literature research. This involved a review of academic journals, industry publications, and technical reports [27][28][29][30][31][32][33][34], leading to the identification of key material fatigue-relevant properties. The properties of this alloy include a density of 7850 kg/m 3 , Young's modulus of 2.038 × 10 11 Pa, Poisson's ratio of 0.29, strength coefficient of 1.1 × 10 9 Pa, strength exponent of −0.093, ductility coefficient of 0.478, ductility exponent of −0.684, cyclic strength coefficient of 1.476 × 10 9 Pa, cyclic strain hardening exponent of 0.0651, tensile and compressive yield strength of 1.042 × 10 9 Pa, and tensile ultimate strength of 1.2773 × 10 9 Pa. Program-controlled element order and adaptive element sizing, with a maximum element size of 1.4 × 10 −2 m, have culminated in an acceptable RUL regarding prediction expectancy based on the recorded number of airplane landings in the airplane technical logbook.…”
Section: Case Study Resultsmentioning
confidence: 99%
“…The material and mechanical properties relevant to strain life curves used to determine the observed landing gear leg RUL made from a 6150 steel alloy, also referred to as the 51CrV4 steel alloy, were determined through rigorous literature research. This involved a review of academic journals, industry publications, and technical reports [27][28][29][30][31][32][33][34], leading to the identification of key material fatigue-relevant properties. The properties of this alloy include a density of 7850 kg/m 3 , Young's modulus of 2.038 × 10 11 Pa, Poisson's ratio of 0.29, strength coefficient of 1.1 × 10 9 Pa, strength exponent of −0.093, ductility coefficient of 0.478, ductility exponent of −0.684, cyclic strength coefficient of 1.476 × 10 9 Pa, cyclic strain hardening exponent of 0.0651, tensile and compressive yield strength of 1.042 × 10 9 Pa, and tensile ultimate strength of 1.2773 × 10 9 Pa. Program-controlled element order and adaptive element sizing, with a maximum element size of 1.4 × 10 −2 m, have culminated in an acceptable RUL regarding prediction expectancy based on the recorded number of airplane landings in the airplane technical logbook.…”
Section: Case Study Resultsmentioning
confidence: 99%
“…Comparing with tempered 51CrV4 steel at 540-650 • C [6], the ∆W t − 2N f model predicts the higher fatigue resistance of 51CrV4 steel when tempered at 450 • C, due to the coefficient κ t and exponent α t both being higher.…”
Section: Strain Energy Density Curvesmentioning
confidence: 91%
“…In the presence of plastic deformations, the fatigue strain-based models such as the CMB are suitable [53][54][55]. The CMB model relates the number of reversals to failure, 2N f , with the total strain amplitude, ε a , via Equation (6), such that…”
Section: Strain-based Life Methodsmentioning
confidence: 99%
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