Life Prediction of IN738LC Considering Creep Damage under Low Cycle Fatigue
As growing attention on greenhouse gas reduction, developing an eco-friendly power generation system of power plants and enhancing its efficiency has been actively researched. In order to increase the efficiency, the operating temperature has been raised, and hence the application of Ni-base super-a...
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Published in | International Journal of Precision Engineering and Manufacturing-Green Technology, 5(2) Vol. 5; no. 2; pp. 311 - 316 |
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Main Authors | , , , , , , |
Format | Journal Article |
Language | English |
Published |
Seoul
Korean Society for Precision Engineering
01.04.2018
Springer Nature B.V 한국정밀공학회 |
Subjects | |
Online Access | Get full text |
ISSN | 2288-6206 2198-0810 |
DOI | 10.1007/s40684-018-0033-6 |
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Abstract | As growing attention on greenhouse gas reduction, developing an eco-friendly power generation system of power plants and enhancing its efficiency has been actively researched. In order to increase the efficiency, the operating temperature has been raised, and hence the application of Ni-base super-alloy has increased to a core component of the power generation system like a turbine blade, a rotor and a boiler. Especially, turbine blades are exposed to high-temperature and high-pressure, and they bear mechanical loads due to the centrifugal force of the high-speed rotation. Thus, the durability of the blade material should be tested under high temperature conditions. In high temperature LCF tests, damage occurs in specimens because of creep. Hence, the aim of this study is to estimate the life of LCF precisely by considering the creep damage in specimens generated during the LCF test. We conducted the LCF tests to propose a new life prediction method considering the fatigue and creep damage. Finally, this study demonstrates the reliability of the prediction method by comparing the predicted life with the actual fatigue life. Through this, we expect to predict the fatigue life more accurately by predicting the fatigue life under different fatigue strain frequencies considering the creep damage. |
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AbstractList | As growing attention on greenhouse gas reduction, developing an eco-friendly power generation system of power plants and enhancing its efficiency has been actively researched. In order to increase the efficiency, the operating temperature has been raised, and hence the application of Ni-base super-alloy has increased to a core component of the power generation system like a turbine blade, a rotor and a boiler. Especially, turbine blades are exposed to high-temperature and high-pressure, and they bear mechanical loads due to the centrifugal force of the high-speed rotation. Thus, the durability of the blade material should be tested under high temperature conditions. In high temperature LCF tests, damage occurs in specimens because of creep. Hence, the aim of this study is to estimate the life of LCF precisely by considering the creep damage in specimens generated during the LCF test. We conducted the LCF tests to propose a new life prediction method considering the fatigue and creep damage. Finally, this study demonstrates the reliability of the prediction method by comparing the predicted life with the actual fatigue life. Through this, we expect to predict the fatigue life more accurately by predicting the fatigue life under different fatigue strain frequencies considering the creep damage. KCI Citation Count: 4 As growing attention on greenhouse gas reduction, developing an eco-friendly power generation system of power plants and enhancing its efficiency has been actively researched. In order to increase the efficiency, the operating temperature has been raised, and hence the application of Ni-base super-alloy has increased to a core component of the power generation system like a turbine blade, a rotor and a boiler. Especially, turbine blades are exposed to high-temperature and high-pressure, and they bear mechanical loads due to the centrifugal force of the high-speed rotation. Thus, the durability of the blade material should be tested under high temperature conditions. In high temperature LCF tests, damage occurs in specimens because of creep. Hence, the aim of this study is to estimate the life of LCF precisely by considering the creep damage in specimens generated during the LCF test. We conducted the LCF tests to propose a new life prediction method considering the fatigue and creep damage. Finally, this study demonstrates the reliability of the prediction method by comparing the predicted life with the actual fatigue life. Through this, we expect to predict the fatigue life more accurately by predicting the fatigue life under different fatigue strain frequencies considering the creep damage. |
Author | Lee, Jeong-Min Seok, Chang-Sung Koo, Jae-Mean Yun, Junghan Wee, Sunguk Song, Hyunwoo Kim, Yongseok |
Author_xml | – sequence: 1 givenname: Jeong-Min surname: Lee fullname: Lee, Jeong-Min organization: Graduate School of Mechanical Engineering, Sungkyunkwan University – sequence: 2 givenname: Sunguk surname: Wee fullname: Wee, Sunguk organization: Graduate School of Mechanical Engineering, Sungkyunkwan University – sequence: 3 givenname: Junghan surname: Yun fullname: Yun, Junghan organization: Graduate School of Mechanical Engineering, Sungkyunkwan University – sequence: 4 givenname: Hyunwoo surname: Song fullname: Song, Hyunwoo organization: Graduate School of Mechanical Engineering, Sungkyunkwan University – sequence: 5 givenname: Yongseok surname: Kim fullname: Kim, Yongseok organization: Railroad Type Approval Team, Korea Railroad Research Institute – sequence: 6 givenname: Jae-Mean surname: Koo fullname: Koo, Jae-Mean organization: School of Mechanical Engineering, Sungkyunkwan University – sequence: 7 givenname: Chang-Sung orcidid: 0000-0002-1205-9996 surname: Seok fullname: Seok, Chang-Sung email: seok@skku.edu organization: School of Mechanical Engineering, Sungkyunkwan University |
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Cites_doi | 10.1016/j.ijfatigue.2007.01.042 10.1007/s12541-016-0095-8 10.1177/0309324711407707 10.1016/j.ijfatigue.2016.11.021 10.1016/j.ijhydene.2006.08.049 10.3795/KSME-A.2010.34.10.1403 10.1016/j.ijfatigue.2013.08.009 10.1007/s12541-015-0041-1 10.5545/sv-jme.2010.108 10.1007/s12541-014-0494-7 10.1007/s40684-015-0005-z 10.1361/105994901770345394 |
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Keywords | Life prediction Gas turbine blade Inconel 738LC Creep Low cycle fatigue |
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PublicationTitle | International Journal of Precision Engineering and Manufacturing-Green Technology, 5(2) |
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References_xml | – reference: ŠerugaD.FajdigaM.NagodeM.Creep Damage Calculation for Thermo Mechanical FatigueJournal of Mechanical Engineering201157537137810.5545/sv-jme.2010.108 – reference: ZhuX.-L.LiuD.XingL.-J.HuY.YangY.-H.Microstructure Evolution of Inconel 718 Alloy during Ring Rolling ProcessInt. J. Precis. Eng. Manuf.201617677578310.1007/s12541-016-0095-8 – reference: WrightI. G.GibbonsT. B.Recent Developments in Gas Turbine Materials and Technology and their Implications for Syngas FiringInternational Journal of Hydrogen Energy2007323610362110.1016/j.ijhydene.2006.08.049 – reference: LarsonF. R.MillerE. J.Time-Temperature Relationship for Rupture and Creep StressesTransactions of ASME195274765775 – reference: HeB.HuangS.WangJ.Product Low-Carbon Design Using Dynamic Programming AlgorithmInt. J. Precis. Eng. Manuf.-Green Tech.201521374210.1007/s40684-015-0005-z – reference: ViswanathanR.Gas Turbine Blade Superalloy Material Property Handbook2001 – reference: ViswanathanR.BakkerW.Materials for Ultrasupercritical Coal Power Plants-Boiler Materials: Part 1Journal of Materials Engineering and Performance200110819510.1361/105994901770345394 – reference: KimT.-W.LeeC.-M.Determination of the Machining Parameters of Nickel-Based Alloys by High-Power Diode LaserInt. J. Precis. Eng. Manuf.201516230931410.1007/s12541-015-0041-1 – reference: HwangK.-T.KimJ.-H.YooK.-B.LeeH.-S.YooY.-S.Low-Cycle Fatigue in Ni-base Superalloy IN738LC at Elevated TemperatureJournal of the Korean Society of Mechanical Engineers A.201034101403140910.3795/KSME-A.2010.34.10.1403 – reference: BeddoesJ.Prediction of Creep Properties for Two Nickel-Base Superalloys from Stress Relaxation TestingJournal of Strain Analysis20154641642710.1177/0309324711407707 – reference: MahobiaG. S.PauloseN.MannanS. L.SudhakarR. G.ChattopadhyayK.Effect of Hot Corrosion on Low Cycle Fatigue Behavior of Superalloy IN718International Journal of Fatigue20145927228110.1016/j.ijfatigue.2013.08.009 – reference: ChoT. Y.ChunH. C.JooY. K.YoonJ. H.A Study on HVOF Coating of WC-Metal Powder on Super Alloy IN718 of Magnetic Bearing Shaft Material of Turbo-BlowerInt. J. Precis. Eng. Manuf.20141571479148410.1007/s12541-014-0494-7 – reference: PahlavanayaliS.DrewG.RaymentA.RaeC. M. F.Thermo-Mechanical Fatigue of a Polycrystalline Superalloy: The Effect of Phase Angle on TMF Life and FailureInternational Journal of Fatigue20083033033810.1016/j.ijfatigue.2007.01.0421140.74394 – reference: SieminskiA.International Energy Outlook2013 – reference: WangR.-Z.ZhangX.-C.GongJ.-G.ZhuX.-M.TuS.-T.Creep-Fatigue Life Prediction and Interaction Diagram in Nickel-Based GH4169 Superalloy at 650°C based on Cycle-by-Cycle ConceptInternational Journal of Fatigue20179711412310.1016/j.ijfatigue.2016.11.021 – volume-title: International Energy Outlook year: 2013 ident: 33_CR1 – volume: 30 start-page: 330 year: 2008 ident: 33_CR10 publication-title: International Journal of Fatigue doi: 10.1016/j.ijfatigue.2007.01.042 – volume: 17 start-page: 775 issue: 6 year: 2016 ident: 33_CR4 publication-title: Int. J. Precis. Eng. Manuf. doi: 10.1007/s12541-016-0095-8 – volume: 46 start-page: 416 year: 2015 ident: 33_CR12 publication-title: Journal of Strain Analysis doi: 10.1177/0309324711407707 – volume: 97 start-page: 114 year: 2017 ident: 33_CR15 publication-title: International Journal of Fatigue doi: 10.1016/j.ijfatigue.2016.11.021 – volume: 32 start-page: 3610 year: 2007 ident: 33_CR8 publication-title: International Journal of Hydrogen Energy doi: 10.1016/j.ijhydene.2006.08.049 – volume: 34 start-page: 1403 issue: 10 year: 2010 ident: 33_CR7 publication-title: Journal of the Korean Society of Mechanical Engineers A. doi: 10.3795/KSME-A.2010.34.10.1403 – volume: 59 start-page: 272 year: 2014 ident: 33_CR9 publication-title: International Journal of Fatigue doi: 10.1016/j.ijfatigue.2013.08.009 – volume-title: Gas Turbine Blade Superalloy Material Property Handbook year: 2001 ident: 33_CR13 – volume: 16 start-page: 309 issue: 2 year: 2015 ident: 33_CR3 publication-title: Int. J. Precis. Eng. Manuf. doi: 10.1007/s12541-015-0041-1 – volume: 57 start-page: 371 issue: 5 year: 2011 ident: 33_CR11 publication-title: Journal of Mechanical Engineering doi: 10.5545/sv-jme.2010.108 – volume: 74 start-page: 765 year: 1952 ident: 33_CR14 publication-title: Transactions of ASME – volume: 15 start-page: 1479 issue: 7 year: 2014 ident: 33_CR2 publication-title: Int. J. Precis. Eng. Manuf. doi: 10.1007/s12541-014-0494-7 – volume: 2 start-page: 37 issue: 1 year: 2015 ident: 33_CR5 publication-title: Int. J. Precis. Eng. Manuf.-Green Tech. doi: 10.1007/s40684-015-0005-z – volume: 10 start-page: 81 year: 2001 ident: 33_CR6 publication-title: Journal of Materials Engineering and Performance doi: 10.1361/105994901770345394 |
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SubjectTerms | Centrifugal force Creep (materials) Damage Electric power generation Energy Efficiency Engineering Fatigue failure Fatigue life Fatigue tests Greenhouse gases High temperature Industrial and Production Engineering Life prediction Low cycle fatigue Materials fatigue Nickel base alloys Operating temperature Power plants Predictions Regular Paper Superalloys Sustainable Development Turbine blades Turbines 기계공학 |
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Title | Life Prediction of IN738LC Considering Creep Damage under Low Cycle Fatigue |
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