Cyclic and time-dependent crack growth mechanisms in Alloy 617 at 800 °C

被引:13
作者
Addison, Dylan A. [1 ]
Tucker, Julie D. [1 ]
Siegmund, Thomas [2 ]
Tomar, Vikas [3 ]
Kruzic, Jamie J. [4 ]
机构
[1] Oregon State Univ, Sch Mech Ind & Mfg Engn, Corvallis, OR 97331 USA
[2] Purdue Univ, Sch Mech Engn, W Lafayette, IN 47907 USA
[3] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
[4] UNSW Sydney, Sch Mech & Mfg Engn, Sydney, NSW 2052, Australia
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2018年 / 737卷
关键词
Alloy; 617; Fatigue; Creep; Void growth; Crack propagation; SAGBO; BEHAVIOR;
D O I
10.1016/j.msea.2018.09.034
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Crack growth mechanisms for Alloy 617 at 800 degrees C were investigated in air with specific emphasis on the transition from cycle-dependent to time-dependent crack growth mechanisms in the creep-fatigue regime. Crack growth studies were conducted using compact tension samples, a load ratio of 0.5, and triangular 5 Hz, 0.33 Hz, and 0.05 Hz waveforms, a trapezoidal 0.05 Hz waveform with 17 s hold time, and sustained loading. Fatigue crack growth rates were relatively insensitive to changes in frequency and hold times in air up to Delta K approximate to 11.5 MPa root m for R = 0.5, i.e, K-max = 23 MPa root m. Above this threshold, the onset of time dependent crack growth was observed via a creep void nucleation and coalescence mechanism for triangular and trapezoidal waveforms with a loading frequency of 0.05 Hz, and during sustained loading. An estimate of the threshold for stress assisted grain boundary oxidation (SAGBO) crack growth was calculated to be 23 MPa root m, and oxidized grain boundaries observed near the crack tip were mostly uncracked, suggesting the SAGBO threshold was not reached before the onset of the void nucleation mechanism. A comparison of results across all available studies suggests that a threshold-based transition from cycle- to time-dependent crack growth at 800 degrees C likely exists. However, the stress intensity factor does not maintain similitude to accurately define a threshold across studies. Thus, gaining an understanding of the crack tip stress states that define the various time dependent mechanisms should be considered in future work.
引用
收藏
页码:205 / 212
页数:8
相关论文
共 24 条
[1]  
American Society for Testing Materials, 2016, Astm e2760-16: standard test method for creep-fatigue crack growth testing, DOI [10.1520/E2760-16, DOI 10.1520/E2760-16]
[2]  
[Anonymous], J PRESS VESSEL TECHN
[3]  
[Anonymous], 2013, ASTM E1457
[4]  
[Anonymous], J PRESS VESSEL TECHN
[5]  
[Anonymous], PUBL SPEC MET CORP
[6]  
[Anonymous], J ASTM INT
[7]  
[Anonymous], INLEXT0814054
[8]  
[Anonymous], 2013, INLCON1330214
[9]  
[Anonymous], 2011, TECHNICAL EC ASPECTS
[10]  
ASTM, 2015, E64715E1 ASTM INT