| Citation: | Experiment on thermomechanical fatigue in nickel based single crystal superalloy DD6[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.017
|
| [1] |
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.
|
| [2] |
ZHANG W J.Thermal mechanical fatigue of single crystal superalloys:achievements and challenges［J］.Materials Science and Engineering:A,2016,650:389-395.
|
| [3] |
LEIDERMARK D.Evaluation of thermomechanical fatigue crack initiation in a single-crystal superalloy［R］.ASME Paper GT2015-42681,2015.
|
| [4] |
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.
|
| [5] |
HAN G M,YU J J,SUN X F,et al.Thermo-mechanical fatigue behavior of single crystal nickel-based superalloy［J］.Material Science and Engineering:A,2011,528(19/20):6217-6224.
|
| [6] |
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.
|
| [7] |
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.
|
| [8] |
STORGARDS E,SIMONSSON K,SJOSTROM S,et al.Thermomechanical fatigue crack growth modeling in a Ni-based superalloy subjected to sustained load［J］.Journal of Engineering for Gas Turbines and Power,2016,138(1):012503.1-012503.7.
|
| [9] |
GUTH S,DOLL S,LANG K H.Lifetime,cyclic deformation and damage behavior of MAR-M247 LC under thermo-mechanical fatigue loading with 0°,180°,-90°and 90°phase shift between strain and temperature［J］.Procedia Engineering,2014,74:269-272.
|
| [10] |
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.
|
| [11] |
FISSOLO A,AMIABLE S,ANCELET O,et al.Crack initiation under thermal fatigue:an overview of CEA experience：Part Ⅰ thermal fatigue appears to be more damaging than uniaxial isothermal fatigue［J］.International Journal of Fatigue,2009,31(3):587-600.
|
| [12] |
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.
|
| [13] |
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.
|
| [14] |
JOHANSSON S,MOVERARE J,LEIDERMARK D,et al.Investigation of localized damage in single crystals subjected to thermalmechanical fatigue (TMF)［J］.Procedia Engineering,2010,2(1):657-666.
|
| [15] |
BOUTAREK N,SAIDI D,ACHEHEB M A,et al.Competition between three damaging mechanisms in the fractured surface of an inconel 713 superalloy［J］.Materials Characterization,2008,59(7):951-956.
|
| [16] |
于慧臣,吴学仁.航空发动机设计用材料数据手册:第4册［M］.北京:航空工业出版社,2010.
|
| [17] |
WANG Rongqiao,JIANG Kanghe,JING Fulei,et al.Thermomechanical fatigue investigation on a single crystal nickel superalloy turbine blade［J］.Engineering Failure Analysis,2016,66(8):284-295.
|
| [18] |
荆甫雷,王荣桥,胡殿印.一种单晶涡轮叶片热机械疲劳寿命评估方法［J］.航空动力学报,2016,31(2):299-306.JING Fulei,WANG Rongqiao,HU Dianyin.A thermo-mechanical fatigue life assessment method for single crystal turbine blades［J］.Journal of Aerospace Power,2016,31(2):299-306.(in Chinese)
|
| [19] |
WEN Z,ZHANG D,LI S,et al.Anisotropic creep damage and fracture mechanism of nickel-base single crystal superalloy under multiaxial stress［J］.Journal of Alloys and Compounds,2017,692:301-312.
|
| [20] |
SEHITOGLU H,BOISMIER D A.Thermo-mechanical fatigue of Mar-M247:Part 2 life prediction［J］.Journal of Engineering Materials and Technology,1990,112(1):80-89.
|
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