Modeling and effect analysis on crack growth behavior of Hastelloy X under high temperature creep-fatigue interaction

被引:15
作者
Liu, Nuohao [1 ]
Dai, Huwei [1 ]
Xu, Lianyong [1 ,2 ]
Tang, Zhengxin [2 ]
Li, Chenyang [1 ]
Zhang, Junhong [1 ,3 ]
Lin, Jiewei [1 ]
机构
[1] Tianjin Univ, State Key Lab Engines, Tianjin 300354, Peoples R China
[2] Tianjin Univ, Sch Mat Sci & Engn, Tianjin 300350, Peoples R China
[3] Tianjin Univ, Mech Engn Dept, RenAi Coll, Tianjin 301636, Peoples R China
基金
中国国家自然科学基金;
关键词
Creep-fatigue interaction; Damage model; Equivalent stress; Crack growth; Hastelloy X; Hold time;
D O I
10.1016/j.ijmecsci.2020.106219
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The crack growth behavior of Hastelloy X under creep-fatigue interaction at high temperature is investigated by a nonlinear creep-fatigue interaction damage model. Multiaxial stress is considered both in the fatigue and creep damage models. The effect of the variance of fatigue damage parameters is analyzed in a quantitative method and some linear effects were observed. The influence of hold time, crack depth ratio and load level on the crack growth behavior are studied and results under different hold time indicate that the increase of hold time, crack depth ratio and load level enhances the creep damage and accelerates the time-dependent crack growth rate. When the hold time varies from 1 to 60 min, the creep damage always dominates the damage accumulation, which can explain the overlap of the curves between da/dt and (C-t)(avg) observed in the experiment very well. The damage contributions of creep, fatigue, and their interaction are quantized thanks to the independent damage model for each part (1) when the hold time increases from 1 min to 60 min, the creep damage ratio rises from 70% to 99% and the interaction damage ratio decreases from 25% to 1%. (2) when the crack depth ratio increases from 0.35 to 0.5, the creep damage ratio rises from 80% to 90% and the interaction damage ratio decreases from 15% to 10%; (3) when the load level increases from 4200 N to 5000 N, the creep damage ratio rises from 75% to 90% and the interaction damage ratio decreases from 25% to 10%. It is also shown the increase of load level and crack depth ratio lead to the increase of equivalent stress and therefore enhances the creep damage and accelerates the crack growth rate.
引用
收藏
页数:16
相关论文
共 65 条
[1]   Cyclic and time-dependent crack growth mechanisms in Alloy 617 at 800 °C [J].
Addison, Dylan A. ;
Tucker, Julie D. ;
Siegmund, Thomas ;
Tomar, Vikas ;
Kruzic, Jamie J. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2018, 737 :205-212
[2]   Creep-fatigue crack growth behavior in 1Cr-1Mo-0.25V steels .1. Estimation of crack tip parameters [J].
Adefris, N ;
Saxena, A ;
McDowell, DL .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 1996, 19 (04) :387-399
[3]   High temperature deformation and damage behavior of RAFM steels under low cycle fatigue loading: Experiments and modeling [J].
Aktaa, J. ;
Schmitt, R. .
FUSION ENGINEERING AND DESIGN, 2006, 81 (19) :2221-2231
[4]  
[Anonymous], 2019, E276019 ASTM, DOI [10.1520/E2760-19, DOI 10.1520/E2760-19]
[5]  
[Anonymous], 2020, Standard Test Method for Measuring the Comparative Burning Characteristics of Solid Plastics in a Vertical Position, DOI DOI 10.1520/E0021-20.2
[6]   A cohesive zone model for fatigue and creep-fatigue crack growth in single crystal superalloys [J].
Bouvard, J. L. ;
Chaboche, J. L. ;
Feyel, F. ;
Gallerneau, F. .
INTERNATIONAL JOURNAL OF FATIGUE, 2009, 31 (05) :868-879
[7]   A new method to predict fatigue crack growth rate of materials based on average cyclic plasticity strain damage accumulation [J].
Chen Long ;
Cai Lixun ;
Yao Di .
CHINESE JOURNAL OF AERONAUTICS, 2013, 26 (01) :130-135
[8]   Creep-fatigue interaction and thermo-mechanical fatigue behaviors of thermoplastics and their composites [J].
Eftekhari, Mohammadreza ;
Fatemi, Ali .
INTERNATIONAL JOURNAL OF FATIGUE, 2016, 91 :136-148
[9]   An investigation on crack growth rate of fatigue and induction heating thermo-mechanical fatigue (TMF) in Hastelloy X superalloy via LEFM, EPFM and integration models [J].
Esmaeilzadeh, M. ;
Qods, F. ;
Arabi, H. ;
Sadeghi, B. M. .
INTERNATIONAL JOURNAL OF FATIGUE, 2017, 97 :135-149
[10]  
Grover PS, 1999, FATIGUE FRACT ENG M, V22, P111, DOI 10.1046/j.1460-2695.1999.00144.x