Volume 36 Issue 5
May  2021
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CHEN Jingyang, JING Fulei, YANG Junjie. Thermo-mechanical fatigue behavior and life modelling in nickel based single crystal superalloy[J]. Journal of Aerospace Power, 2021, 36(5): 897-906. doi: 10.13224/j.cnki.jasp.2021.05.001
Citation: CHEN Jingyang, JING Fulei, YANG Junjie. Thermo-mechanical fatigue behavior and life modelling in nickel based single crystal superalloy[J]. Journal of Aerospace Power, 2021, 36(5): 897-906. doi: 10.13224/j.cnki.jasp.2021.05.001

Thermo-mechanical fatigue behavior and life modelling in nickel based single crystal superalloy

doi: 10.13224/j.cnki.jasp.2021.05.001
  • Received Date: 2020-08-21
  • Publish Date: 2021-05-28
  • Mechanical strain-controlled thermal mechanical fatigue (TMF) tests were performed on thin-walled tubular specimens made of nickel based single crystal superalloy DD6, and the effects of thermal cycles, phase shift and load-controlled mode on stress-strain behavior and fatigue lifetime were studied. The experimental results indicated that the lifetime of TMF was shorter than that of isothermal fatigue (IF) at the peak temperature due to the asymmetry of stress and additional damage induced by thermal cycles. In addition, the lifetime under out-of-phase (OP) cycles was less than that under in-phase (IP) cycles in mechanical strain-controlled mode, which was in contrast with that in stress-controlled mode. According to the results of viscoplastic analysis based on slip systems with Walker constitutive model, the correlation between the damage generated in single crystal superalloy under different TMF loadings and the microscopic parameters on slip systems was identified. Moreover, the max Schmid stress, max slip shear strain rate, cyclic Schmid stress ratio and slip shear strain range were selected as the damage parameters, and then a new life model based on microscopic parameters was proposed for the TMF life prediction. The predicted TMF life of DD6 under different phase shift and different load-controlled mode was within a factor 2 of the experimental life.

     

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  • [1]
    ZHANG W J.Thermal mechanical fatigue of single crystal superalloys:achievements and challenges[J].Materials Science and Engineering A,2016,650:389-395.
    [2]
    JONES J,WHITTAKER M,LANCASTER R,et al.The influence of phase angle,strain range and peak cycle temperature on the TMF crack initiation behaviour and damage mechanisms of the nickel based superalloy,RR1000[J].International Journal of Fatigue,2017,98:279-285.
    [3]
    荆甫雷,蒋康河,张斌,等.镍基单晶高温合金DD6热机械疲劳试验[J].航空动力学报,2018,33(12):2965-2971. JING Fulei,JIANG Kanghe,ZHANG Bin,et al.Experimental research on thermomechanical fatigue in nickel based single crystal superalloy DD6[J].Journal of Aerospace Power,2018,33(12):2965-2971.(in Chinese)
    [4]
    AMARO R L,ANTOLOVICH S D,NEU R W,et al.On thermo-mechanical fatigue in single crystal Ni-base superalloys[J].Procedia Engineering,2010,2(1):815-824.
    [5]
    HONG H U,KANG J G,CHOI B G,et al.A comparative study on thermomechanical and low cycle fatigue failures of a single crystal nickel-based superalloy[J].International Journal of Fatigue,2011,33(12):1592-1599.
    [6]
    YU J J,HAN G M,CHU Z K,et al.High temperature thermo-mechanical and low cycle fatigue behaviors of DD32 single crystal superalloy[J].Materials Science and Engineering A,2014,592:164-172.
    [7]
    蒋康河.镍基单晶高温合金热机械疲劳损伤机理及寿命预测[D].北京:北京航空航天大学,2017. JIANG Kanghe.Thermomechanical fatigue damage mechanism and life prediction of a single crystal nickel superalloy[D].Beijing:Beijing University of Aeronautics and Astronautics,2017.(in Chinese)
    [8]
    CUNHA F J,DAHMER M T.CHYU M K.Thermal-mechanical life prediction system for anisotropic turbine components[J].Journal of Turbomachinery,2006,128(2):240-250.
    [9]
    GOMEZ T,AWARKE A,PISCHINGER S.A new low cycle fatigue criterion for isothermal and out-of-phase thermomechanical loading[J].International Journal of Fatigue,2010,32(4):769-779.
    [10]
    AMARO R L,ANTOLOVICH S D,NEU R W,et al.Thermomechanical fatigue and bithermal-thermomechanical fatigue of a nickel-base single crystal superalloy[J].International Journal of Fatigue,2012,42:165-171.
    [11]
    VACCHIERI E,HOLDSWORTH S R,POGGIO E,et al.Service-like TMF tests for the validation and assessment of a creep-fatigue life procedure developed for GT blades and vanes[J].International Journal of Fatigue,2017,99:216-224.
    [12]
    VOSE F,BECKER M,FISCHERSWORRING B A,et al.An approach to life prediction for a nickel-base superalloy under isothermal and thermo-mechanical loading conditions[J].International Journal of Fatigue,2013,53:49-57.
    [13]
    ABDULLAHI O A,SAMIR E,PANAGIOTIS L,et al.Aero-engine turbine blade life assessment using the Neu/Sehitoglu damage model[J].International Journal of Fatigue,2014,61:160-169.
    [14]
    WANG R Q,JIANG K H,JING F L,et al.Thermomechanical fatigue failure investigation on a single crystal nickel superalloy turbine blade[J].Engineering Failure Analysis,2016,66(8):284-295.
    [15]
    ASTM International.Standard practice for strain controlled thermomechanical fatigue testing:E2368-10[S].United States:ASTM,2010:1-10.
    [16]
    KERSEY R K,STAROSELSKY A,DUDZINSKI D C,et al.Thermomechanical fatigue crack growth from laser drilled holes in single crystal material[J].International Journal of Fatigue,2013,55:183-193.
    [17]
    JORDAN E H,WALKER K P.A Viscoplastic model for single crystals[J].Journal of Engineering Materials and Technology,1992,114(1):19-26.
    [18]
    JORDAN E H,SHI S X,WALKER K P.The viscoplastic behavior of Hastelloy-X single crystal[J].International Journal of Plasticity.1993,9(1):119-139.
    [19]
    王荣桥,荆甫雷,胡殿印.基于临界平面的镍基单晶高温合金疲劳寿命预测模型[J].航空动力学报,2013,28(11):2587-2592. WANG Rongqiao,JING Fulei,HU Dianyin.Fatigue life prediction model based on critical plane of nickel-based single crystal superalloy[J].Journal of Aerospace Power,2013,28(11):2587-2592.(in Chinese)
    [20]
    于慧臣,吴学仁.航空发动机设计用材料数据手册(第四册)[M].北京:航空工业出版社,2010.
    [21]
    TINGA T,BREKELMANS W A M,GEERS M G D.Time-incremental creep-fatigue damage rule for single crystal Ni-base superalloys[J].Materials Science and Engineer-ing A,2009,508(1/2):200-208.
    [22]
    WANG R Q,ZHANG B,HU D Y,et al.A critical-plane-based thermomechanical fatigue lifetime prediction model and its application in nickel-based single-crystal turbine blades[J].Materials at High Temperatures,2019,36(4):325-334.
    [23]
    SHI D Q,HUANG J,YANG X G,et al.Effects of crystallographic orientations and dwell types on low cycle fatigue and life modeling of a SC superalloy[J].International Journal of Fatigue,2013,49:31-39.
    [24]
    荆甫雷,王荣桥,胡殿印,等.单晶高温疲劳损伤参量的选取与寿命建模[J].航空学报,2016,37(9):2749-2756. JING Fulei,WANG Rongqiao,HU Dianyin,et al.Damage parameter determination and life modeling for high temperature fatigue of nickel-based single crystal superalloys[J].Acta Aeronautica et Astronautica Sinica,2016,37(9):2749-2756.(in Chinese)
    [25]
    王荣桥,蒋康河,胡殿印,等.基于主成分分析的镍基单晶高温疲劳寿命模型[J].航空动力学报,2016,31(6):1359-1367. WANG Rongqiao,JIANG Kanghe,HU Dianyin,et al.High temperature fatigue life model for single crystal nickel superalloy based on principal component analysis[J].Journal of Aerospace Power,2016,31(6):1359-1367.(in Chinese)
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