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Life Modeling Of Notched Cm247lc Ds Nickel Base Superalloy


Life Modeling Of Notched Cm247lc Ds Nickel Base Superalloy
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Life Modeling Of Notched Cm247lc Ds Nickel Base Superalloy


Life Modeling Of Notched Cm247lc Ds Nickel Base Superalloy
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Author : Zachary Joseph Moore
language : en
Publisher:
Release Date : 2008

Life Modeling Of Notched Cm247lc Ds Nickel Base Superalloy written by Zachary Joseph Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008 with Gas-turbines categories.


Directionally solidified (DS) nickel-base superalloys are used in high temperature gas turbine engines because of their high yield strength at extreme temperatures and strong low cycle fatigue (LCF) and creep resistance. Costly inspecting, servicing, and replacing of damaged components has precipitated much interest in developing models to better predict service life. Turbine blade life modeling is complicated by the presence of notches, dwells, high temperatures and temperature gradients, and highly anisotropic material behavior. This work seeks to develop approaches for predicting the life of hot sections of gas turbines blade material CM247LC DS subjected to LCF, dwells, and stress concentrations while taking into consideration orientation and notch effects. Experiments were conducted on an axial servo-hydraulic MTS® testing machine. High temperature LCF tests were performed on smooth and notched round-bar specimens in both longitudinal and transverse orientations with and without dwells. Experimental results were used to develop and validate an analytical life prediction model. An analytical model based on a multiaxial Neuber approach predicts the local stress-strain response at a notch and other geometric stress concentrations. This approach captures anisotropy through a multiaxial generalization of the Ramberg-Osgood relation using a Hill's type criterion. The elastic notch response is determined using an anisotropic elastic finite element analysis (FEA) of the notch. The limitations of the simpler analytical life-modeling method are discussed in light of FEA using an anisotropic elastic-crystal viscoplastic material model. This life-modeling method provides a quick alternative to time demanding elastic-plastic FEA allowing engineers more design iterations to improve reliability and service life.



Thermomechanical Fatigue Behavior Of The Directionally Solidified Nickel Base Superalloy Cm247lc


Thermomechanical Fatigue Behavior Of The Directionally Solidified Nickel Base Superalloy Cm247lc
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Author : Robert Anthony Kupkovits
language : en
Publisher:
Release Date : 2009

Thermomechanical Fatigue Behavior Of The Directionally Solidified Nickel Base Superalloy Cm247lc written by Robert Anthony Kupkovits and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2009 with Alloys categories.


Due to the extreme operating conditions present in the combustion sections of gas turbines, designers have relied heavily on specialized engineering materials. For blades, which must retain substantial strength and resistance to fatigue, creep, and corrosion at high temperatures, directionally-solidified (DS) nickel-base superalloys have been used extensively. Complex thermomechanical loading histories makes life prediction for such components difficult and subjective. Costly product inspection and refurbishment, as well as capital expense required in turbine forced outage situations, are significant drains on the resources of turbine producers. This places a premium on accurate endurance prediction as the foundation of viable long-term service contracts with customers. In working towards that end, this work characterizes the behavior of the blade material CM247LC DS subjected to a variety of in-phase (IP) and out-of phase (OP) loading cycles in the presence of notch stress concentrations. The material response to multiaxial notch effects, highly anisotropic material behavior, time-dependent deformation, and waveform and temperature cycle characteristics is presented. The active damage mechanisms influencing crack initiation are identified through extensive microscopy as a function of these parameters. This study consisted of an experimental phase as well as a numerical modeling phase. The first involved conducting high temperature thermomechanical fatigue (TMF) tests on both smooth and notched round-bar specimens to compile experimental results. Tests were conducted on longitudinal and transverse material grain orientations. Damage is characterized and conclusions drawn in light of fractography and microscopy. The influences of microstructure morphology and environmental effects on crack initiation are discussed. The modeling phase utilized various finite element (FE) simulations. These included an anisotropic-elastic model to capture the purely elastic notch response, and a continuum-based crystal visco-plastic model developed specifically to compute the material response of a DS Ni-base superalloy based on microstructure and orientation dependencies. These FE simulations were performed to predict and validate experimental results, as well as identify the manifestation of damage mechanisms resulting from thermomechanical fatigue. Finally, life predictions using simple and complex analytical modeling methods are discussed for predicting component life at various stages of the design process.



Generic Behavior Framework Of Sx And Ds Nickel Base Superalloys With Applications To Constitutive And Life Prediction Modeling


Generic Behavior Framework Of Sx And Ds Nickel Base Superalloys With Applications To Constitutive And Life Prediction Modeling
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Author : Firat Irmak
language : en
Publisher:
Release Date : 2022

Generic Behavior Framework Of Sx And Ds Nickel Base Superalloys With Applications To Constitutive And Life Prediction Modeling written by Firat Irmak and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2022 with categories.


Selection of materials to be used for components experiencing extreme conditions is a critical process in the design phase. Nickel-base superalloys have been frequently used for hot gas path components in the turbomachinery industry. These components are required to withstand both fatigue and creep at extreme temperatures during their service time. In general, the extreme temperature materials mostly embody polycrystalline, directionally solidified, and single crystal superalloys. It is essential for design engineers to predict accurate damage behavior and lifespan for these components to prevent catastrophic failures. This dissertation presents a new framework to represent mechanical behavior of Nickel-base superalloys under variety of loading conditions. A set of constitutive and lifing models that can be applied broadly are developed based on observed trends. Despite the development of over 30 variations of single crystal and directionally solidified Nickel-base superalloys, the behavior of these alloys nominally follows similar trends with respect to temperature and orientation. Temperature-, rate-, and orientation- dependence of these materials are studied. The goal is to eliminate extensive time and cost of experiments by creating parameters to be used in strength and life calculations for generic single crystal and directionally solidified Nickel-base alloys. In order to apply generic constants to deformation modeling, a crystal-plasticity model is modified to create stress-strain hysteresis loops. Strain, stress and multi-axial life models are developed to represent the lifing behavior of the candidate alloys under uniaxial and multiaxial environments. Tensile and low-cycle fatigue experiments are conducted to measure the accuracy of these models. Parameters for the models are built on regression fits in comparison with a comprehensive material database. This database includes elastic, plastic, creep, and fatigue properties.



International Aerospace Abstracts


International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1999

International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Aeronautics categories.




Metals Abstracts Index


Metals Abstracts Index
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Author :
language : en
Publisher:
Release Date : 1995

Metals Abstracts Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Metallurgy categories.




Modelling Of Tmf Crack Growth In Polycrystalline Gas Turbine Alloys


Modelling Of Tmf Crack Growth In Polycrystalline Gas Turbine Alloys
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Author : Jordi Loureiro-Homs
language : en
Publisher: Linköping University Electronic Press
Release Date : 2020-10-07

Modelling Of Tmf Crack Growth In Polycrystalline Gas Turbine Alloys written by Jordi Loureiro-Homs and has been published by Linköping University Electronic Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2020-10-07 with categories.


The main objective of the work presented in this Licentiate of Engineering thesis is to investigate and model the fatigue crack propagation behaviour of the nickel-based superalloy Inconel 792, with special attention to the industrial lifing of high-temperature components. In-phase (IP) crack propagation tests have been performed at different temperatures and loading regimes, including extended hold times. The observations from these tests have been the basis for establishing several hypotheses to describe the crack growth behaviour, which progressively have been verified experimentally and numerically. Most prominently, it has been observed that crack closure has a substantial impact on crack growth and can explain, to a large degree, the crack growth behaviour for this material under the conditions studied. This phenomenon has been observed experimentally and modelled numerically to extend further the precision of the methodology. Huvudsyftet med arbetet som presenteras i denna licentiat avhandling är att undersöka och modellera utmattnings sprickväxtbeteendet hos den nickelbaserade superlegeringen Inconel 792, med särskild uppmärksamhet riktad mot liuslängsdmodellering av högtemperaturkomponenter i en industriell kontext. I-fas (IP) sprickväxtprov har utförts vid olika temperaturer och belastningsregimer, inklusive hålltider. Observationerna från dessa tester har legat till grund för hypoteser för att förklara spricktillväxtbeteende, vilka successivt har verifierats experimentellt och numeriskt. Mest framträdande har det observerats att sprickslutning har en väsentlig inverkan på sprickväxten, och kan i stor utsträckning förklara sprickväxten för detta material under studerade förhållanden. Detta fenomen har observerats experimentellt och modellerats numeriskt för att förbättra metodens precision.



Superalloys 2012


Superalloys 2012
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Author : Eric S. Huron
language : en
Publisher: John Wiley & Sons
Release Date : 2012-10-02

Superalloys 2012 written by Eric S. Huron and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-10-02 with Technology & Engineering categories.


A superalloy, or high-performance alloy, is an alloy that exhibits excellent mechanical strength at high temperatures. Superalloy development has been driven primarily by the aerospace and power industries. This compilation of papers from the Twelfth International Symposium on Superalloys, held from September 9-13, 2012, offers the most recent technical information on this class of materials.



Cooperative Investigation Of Relationship Between Static And Fatigue Properties Of Wrought N 155 Alloy At Elevated Temperatures


Cooperative Investigation Of Relationship Between Static And Fatigue Properties Of Wrought N 155 Alloy At Elevated Temperatures
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Author : Clyde C. Swett
language : en
Publisher:
Release Date : 1956

Cooperative Investigation Of Relationship Between Static And Fatigue Properties Of Wrought N 155 Alloy At Elevated Temperatures written by Clyde C. Swett and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamic load categories.




Metals Abstracts


Metals Abstracts
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Author :
language : en
Publisher:
Release Date : 1993

Metals Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Metallurgy categories.




The Superalloys


The Superalloys
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Author : Roger C. Reed
language : en
Publisher: Cambridge University Press
Release Date : 2008-07-31

The Superalloys written by Roger C. Reed and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008-07-31 with Technology & Engineering categories.


Superalloys are unique high-temperature materials used in gas turbine engines, which display excellent resistance to mechanical and chemical degradation. This book introduces the metallurgical principles which have guided their development. Suitable for graduate students and researchers, it includes exercises and additional resources at www.cambridge.org/9780521859042.