Mathematical simulation of low cycle fatigue of high-loaded engine parts

The paper discusses main aspects of low cycle fatigue influence on the lifetime of engine parts. The importance and history of the problem, the main experiments and the effects impacting the low cycle fatigue of structural materials are described. A hypothesis about the existence of a thermomechanic...

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Main Author: Yury M. Temis
Format: Article
Language:English
Published: Elsevier 2018-12-01
Series:Propulsion and Power Research
Online Access:http://www.sciencedirect.com/science/article/pii/S2212540X18300610
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spelling doaj-87f284d25edd405fae4ce618286143ba2020-11-24T22:01:26ZengElsevierPropulsion and Power Research2212-540X2018-12-0174277287Mathematical simulation of low cycle fatigue of high-loaded engine partsYury M. Temis0Central Institute of Aviation Motors, 2 Aviamotornaya st., Moscow 111116, RussiaThe paper discusses main aspects of low cycle fatigue influence on the lifetime of engine parts. The importance and history of the problem, the main experiments and the effects impacting the low cycle fatigue of structural materials are described. A hypothesis about the existence of a thermomechanical surface of structural material, generalized to the case of a cyclical loading was used to approximate the loops of cyclic nonisothermal elastoplastic deformation curves. The cyclic deformation curve model is based on the following three parameters: the elastic modulus during unloading, the Bauschinger effect and the conversion parameter of the nonlinear part of its first halfcycle. This model also accounts for the accumulated plastic strain, as well as the testing temperature. The criterion of durability is formulated, based on the dependence between the number of halfcycles to failure and the accumulated plastic deformation. Deformation theory of plasticity, generalized to the case of cyclic deformation, in combination with the durability model and technology of ''dying'' elements is applied to the finite element analysis of low cycle fatigue of gas turbine engine parts. The results of calculations are demonstrated. Keywords: Gas turbine engine, Low cycle fatigue, Nonisothermal plasticity, Finite element modeling, Durability modeling, Cyclic loadinghttp://www.sciencedirect.com/science/article/pii/S2212540X18300610
collection DOAJ
language English
format Article
sources DOAJ
author Yury M. Temis
spellingShingle Yury M. Temis
Mathematical simulation of low cycle fatigue of high-loaded engine parts
Propulsion and Power Research
author_facet Yury M. Temis
author_sort Yury M. Temis
title Mathematical simulation of low cycle fatigue of high-loaded engine parts
title_short Mathematical simulation of low cycle fatigue of high-loaded engine parts
title_full Mathematical simulation of low cycle fatigue of high-loaded engine parts
title_fullStr Mathematical simulation of low cycle fatigue of high-loaded engine parts
title_full_unstemmed Mathematical simulation of low cycle fatigue of high-loaded engine parts
title_sort mathematical simulation of low cycle fatigue of high-loaded engine parts
publisher Elsevier
series Propulsion and Power Research
issn 2212-540X
publishDate 2018-12-01
description The paper discusses main aspects of low cycle fatigue influence on the lifetime of engine parts. The importance and history of the problem, the main experiments and the effects impacting the low cycle fatigue of structural materials are described. A hypothesis about the existence of a thermomechanical surface of structural material, generalized to the case of a cyclical loading was used to approximate the loops of cyclic nonisothermal elastoplastic deformation curves. The cyclic deformation curve model is based on the following three parameters: the elastic modulus during unloading, the Bauschinger effect and the conversion parameter of the nonlinear part of its first halfcycle. This model also accounts for the accumulated plastic strain, as well as the testing temperature. The criterion of durability is formulated, based on the dependence between the number of halfcycles to failure and the accumulated plastic deformation. Deformation theory of plasticity, generalized to the case of cyclic deformation, in combination with the durability model and technology of ''dying'' elements is applied to the finite element analysis of low cycle fatigue of gas turbine engine parts. The results of calculations are demonstrated. Keywords: Gas turbine engine, Low cycle fatigue, Nonisothermal plasticity, Finite element modeling, Durability modeling, Cyclic loading
url http://www.sciencedirect.com/science/article/pii/S2212540X18300610
work_keys_str_mv AT yurymtemis mathematicalsimulationoflowcyclefatigueofhighloadedengineparts
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