| Citation: | WANG Rong-qiao, JING Fu-lei, HU Dian-yin. Fatigue life prediction model based on critical plane of nickel-based single crystal superalloy[J]. Journal of Aerospace Power, 2013, 28(11): 2587-2592. |
| [1] |
胡壮麒,刘丽荣,金涛,等.镍基单晶高温合金的发展[J].航空发动机,2005,31(3):1-7. HU Zhuangqi,LIU Lirong,JIN Tao,et al.Development of the Ni-base single crystal superalloys[J].Aeroengine,2005,31(3):1-7.(in Chinese)
|
| [2] |
石多奇,杨晓光,于慧臣.一种镍基单晶和定向结晶的疲劳寿命模型[J].航空动力学报,2010,25(8):1871-1875. SHI Duoqi,YANG Xiaoguang,YU Huichen.Fatigue life prediction model for nickel-based single crystal and directionally solidified superalloy[J].Journal of Aerospace Power,2010,25(8):1871-1875.(in Chinese)
|
| [3] |
岳珠峰,陶仙德,尹泽勇,等.一种镍基单晶超合金高温低周疲劳的晶体取向相关性模型[J].应用数学与力学,2000,21(4):373-381. YUE Zhufeng,TAO Xiande,YIN Zeyong,et al.A crystallographic model for the orientation dependence of low cyclic fatigue property of a nickel-base single crystal superalloy[J].Applied Mathematics and Mechanics,2000,21(4):373-381.(in Chinese)
|
| [4] |
丁智平,刘义伦,尹泽勇.镍基单晶高温合金蠕变-疲劳寿命评估方法进展[J].机械强度,2003,25(3):254-259. DING Zhiping,LIU Yilun,YIN Zeyong.Development on evaluating method of creep-fatigue life of single crystal nickel-based superalloys[J].Journal of Mechanical Strength, 2003,25(3):254-259.(in Chinese)
|
| [5] |
Swanson G,Arakere N K.Effect of crystal orientation on analysis of single-crystal nickel-based turbine blade superalloys.NASA/TP-2000-210074,2000.
|
| [6] |
Arakere N K,Swanson G.Effect of crystal orientation on fatigue failure of single crystal nickel base turbine blade superalloys[J].Journal of Engineering for Gas Turbines and Power,2002,124(1):161-176.
|
| [7] |
Naik R A,DeLuca D P,Shah D M.Critical plane fatigue modeling and characterization of single crystal nickel superalloys[J].Journal of Engineering for Gas Turbines and Power,2004,126(2):391-400.
|
| [8] |
Ranjan S,Arakere N K.A fracture-mechanics-based methodology for fatigue life prediction of single crystal nickel-based superalloys[J].Journal of Engineering for Gas Turbines and Power,2008,130(3):032501.1-032501.8.
|
| [9] |
刘金龙.镍基单晶/定向凝固涡轮叶片铸造模拟及其合金低循环疲劳行为研究.北京:北京航空航天大学,2011. LIU Jinlong.Investigation on cast simulation and low cycle fatigue behavior of Ni-based single crystal and directionally solidified turbine blade.Beijing:Beijing University of Aeronautics and Astronautics,2011.
|
| [10] |
Jordan E H,Walker K P.A viscoplastic model for single crystals[J].Journal of Engineering Materials and Technology,1992,114:19-26.
|
| [11] |
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.
|
| [12] |
Nelson R S,Levan G W,Harvey P R.Creep fatigue life prediction for engine hot section materials (isotropic):final report.NASA-CR-189221,1992.
|
| [13] |
Karolczuk A,Macha E.A review of critical plane orientations in multiaxial fatigue failure criteria of metallic materials[J].Internation Journal of Fracture,2005,134(3/4):267-304.
|
| [14] |
尚德广,王德俊.多周疲劳强度[M].北京:科学出版社,2007.
|
| [15] |
李影,苏彬.DD6单晶合金高温低周疲劳机制[J].航空动力学报,2003,18(6):732-736. LI Ying,SU Bin.Mechanisms of low cyclic fatigue of DD6 alloy at elevated temperature[J].Journal of Aerospace Power,2003,18(6):732-736.(in Chinese)
|
| [16] |
Tinga T,Brekelmans W A M,Geers M G D.Time-incremental creep-fatigue damage rule for single crystal Ni-base superalloys[J].Material Science and Engineering:A,2009,508(1):200-208.
|
| [17] |
Leckovitch V,Sievert R,Svendsen B.Simulation of deformation and lifetime behavior of a fcc single crystal superalloy at high temperature under low-cycle fatigue loading[J].International Journal of Fatigue,2006,28(12):1791-1802.
|
| [18] |
Staroselsky A,Cassenti B N.Creep,plasticity,and fatigue of single crystal superalloy[J].International Journal of Solids and Structures,2011,48(13):2060-2075.
|
| [19] |
Wan J S,Yue Z F.A low-cycle fatigue life model of nickel-based single crystal superalloys under multiaxial stress state[J].Material Science and Engineering:A,2005,392(1):145-149.
|