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Effect of superimposed high cycle fatigue loadings on the out-of-phase thermal-mechanical fatigue behaviour of CoCr22Ni22W14

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TLDR
In this paper, the thermal-mechanical fatigue (TMF) behavior of CoCr22Ni22W14 was investigated under total strain controlled out-of-phase (OP) experiments without and with superimposed high cycle fatigue (HCF) loadings.
Abstract
The thermal-mechanical fatigue (TMF) behaviour of CoCr22Ni22W14 was investigated under total strain controlled out-of-phase (OP) experiments without and with superimposed high cycle fatigue (HCF) loadings. The minimum temperature T min was 200 °C and the maximum temperature T max was varied between 750 and 1200 °C. The mechanical strain amplitude e me a, during pure TMF tests was kept equal to the thermal strain amplitude e th 1 and the superimposed HCF amplitude e HCF a,t was varied between 0.05 and 0.2%. In both loading conditions cyclic hardening is observed, which is the less pronounced the higher T max is. Only at T max = 1200 °C, cyclic softening appears after cyclic hardening in the first cycles as a result of creep damage accumulation. With increasing superimposed HCF amplitudes, the cyclic deformation behaviour is obviously more and more determined by the superimposed HCF loadings. Due to the dynamic relaxation processes at higher temperatures, tensile mean stresses develop during all TMF tests performed. Under TMF-OP conditions a significant lifetime reduction is observed as a result of superimposed HCF loadings. This lifetime reduction increases with growing HCF amplitudes and may approach 90% of the fatigue lifetime obtained from pure OP experiments. For each T max the dependence between the total strain amplitude (e a.t = e me a.t + e HCF a.t ) and the number of cycles to failure can be described as a potential function (e a.t = A × N B b ) with an exponent b which decreases with increasing T max and which depends on the material properties at different temperatures.

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Citations
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Mechanisms and modelling of fatigue crack growth under combined low and high cycle fatigue loading

TL;DR: In this article, a mechanism-based model is presented, which is able to describe the evolution of microcracks under pure low cycle fatigue and combined LCF and high cycle fatigue (HCF) loading conditions.
Journal ArticleDOI

Lifetime prediction of cast iron materials under combined thermomechanical fatigue and high cycle fatigue loading using a mechanism-based model

TL;DR: In this article, a mechanism-based model is used, which is based on micro-crack growth, to predict the fatigue life of three cast iron materials (EN-GJS-700, EN-GJV-450 and ENGJL-250) for combined thermomechanical and high cycle fatigue loading.
Journal ArticleDOI

Damage Mechanisms in Silicon-Molybdenum Cast Irons Subjected to Thermo-mechanical Fatigue

TL;DR: The damage mechanisms active in silicon-molybdenum cast irons, namely EN-GJS-SiMo5-1 and SiMo1000, under thermo-mechanical fatigue and combined thermal and high-cycle fatigue conditions were investigated in this article.
Journal ArticleDOI

Thermomechanical fatigue behavior and lifetime prediction of niobium-bearing ferritic stainless steels

TL;DR: In this article, the thermomechanical fatigue and isothermal low-cycle-fatigue (LCF) behaviors of niobium-containing ferritic stainless steels are presented for the temperature range from 100°C to the maximum temperatures between 500 and 800°C.
Journal ArticleDOI

Experimental and analytical investigation of the TMF-HCF lifetime behavior of two cast iron alloys

TL;DR: In this paper, the combined loading of Thermomechanical Fatigue (TMF) with high cycle fatigue (HCF) has been experimentally investigated for two cast iron alloys.
References
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Journal ArticleDOI

Cyclic deformation and precipitation behaviour of NiCr22Co12Mo9 during thermal fatigue

TL;DR: In this paper, the NiCr22Co12Mo9 (corresponding to Inconel 617) is shown to be thermally fatigued with a constant minimum temperature Tmin = 473 K and maximum temperatures Tmax = 873, 1123, 1323, and 1473 K.
Journal ArticleDOI

Non‐isothermal fatigue crack growth in hastelloy‐x

TL;DR: In this paper, non-isothermal fatigue crack growth tests were performed on Hastelloy-X single edge notch specimens in which strain and temperature were varied simultaneously, and the results were rationalized using a corrected stress-intensity factor computed from the actual load, the closing bending moment caused by the increase compliance with crack length, and with the effective opening stress.
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