Fatigue crack growth threshold concept and test results for Al- and Ti-alloys

被引:6
作者
Marci, G [1 ]
机构
[1] DLR, German Aerosp Res Ctr, Mat Res Inst, D-51170 Cologne, Germany
来源
FATIGUE CRACK GROWTH THRESHOLDS, ENDURANCE LIMITS, AND DESIGN | 2000年 / 1372卷
关键词
fatigue crack propagation; threshold; non-propagation condition; material property;
D O I
10.1520/STP13427S
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The fact that fatigue crack propagation (FCP) rates approach zero asymptotically as the fracture mechanics loading parameter Delta K decreases toward certain limiting values is the reason for the scientific interest in these so-called 'threshold' values. In respect to the practical use of these 'limiting values', the author divides them into two groups, namely in 'non-propagation conditions' Delta K-th and in a material property 'FCP-threshold' Delta K-T. It is shown that Delta K-T must be an integral part in the functional correlation between FCP-rates and the cyclic loading conditions expressed in; Delta K-eff. The experimental determination of Delta K-th on. six Al-alloys and four Ti-compressor disk alloys show that Delta K-T exists for all the alloys investigated. The effect of temperature on Delta K-T was investigated on one Ti 6Al4V- and one Ti 8Al 1V 1Mo disk material at room temperature (RT) and 260 degrees C and at RT, 260 degrees C and 360 degrees C,respectively. No temperature effect on Delta K-T was found for the temperature range investigated.
引用
收藏
页码:81 / 95
页数:15
相关论文
共 50 条
[41]   MODIFICATION OF THE LSM CRITERIA TO APPROXIMATE TEST DATA FOR FATIGUE CRACK GROWTH RATE [J].
Klysz, Sylwester ;
Lisiecki, Janusz ;
Leski, Andrzej ;
Bakowski, Tomasz .
JOURNAL OF THEORETICAL AND APPLIED MECHANICS, 2012, 50 (04) :923-931
[42]   3D shear-mode fatigue crack growth in maraging steel and Ti-6Al-4V [J].
Doquet, V. ;
Bui, Q. H. ;
Bertolino, G. ;
Merhy, E. ;
Alves, L. .
INTERNATIONAL JOURNAL OF FRACTURE, 2010, 165 (01) :61-76
[43]   Fatigue crack growth characteristics of inertia friction welded Ti17 alloy [J].
Ji, Y. ;
Wu, S. ;
Yu, G. .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2014, 37 (01) :39-49
[44]   High cycle fatigue and fatigue crack propagation behaviors of β-annealed Ti-6Al-4V alloy [J].
Jeong D. ;
Kwon Y. ;
Goto M. ;
Kim S. .
International Journal of Mechanical and Materials Engineering, 2017, 12 (1)
[45]   Fatigue crack propagation in β Ti-15Mo-5Zr-3Al alloy [J].
Tokaji, K ;
Shiota, H ;
Bian, JC .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1998, 243 (1-2) :155-162
[46]   Effect of grain structure on fatigue crack propagation behavior of Al-Cu-Li alloys [J].
Lu, Dingding ;
Lin, Ben ;
Liu, Tianle ;
Deng, Sanxi ;
Guo, Youjie ;
Li, Jinfeng ;
Liu, Danyang .
JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY, 2023, 148 :75-89
[47]   Fatigue crack growth rates for offshore wind monopile weldments in air and seawater: SLIC inter-laboratory test results [J].
Mehmanparast, Ali ;
Brennan, Feargal ;
Tavares, Isaac .
MATERIALS & DESIGN, 2017, 114 :494-504
[48]   The effect of various atmospheres on the threshold fatigue crack growth behavior of AISI 304 stainless steel [J].
Kelestemur, MH ;
Chaki, TK .
INTERNATIONAL JOURNAL OF FATIGUE, 2001, 23 (02) :169-174
[49]   Testing and evaluation for fatigue crack propagation of Ti-6Al-4V/ELI and 7050-T7452 alloys at high temperatures [J].
Zhu, Yuntao ;
Xiong, Junjiang ;
Lv, Zhiyang ;
Zhao, Yanguang .
CHINESE JOURNAL OF AERONAUTICS, 2018, 31 (06) :1388-1398
[50]   Near threshold fatigue crack growth in aluminium alloys at low and ultrasonic frequency: Influences of specimen thickness, strain rate, slip behaviour and air humidity [J].
Holper, B ;
Mayer, H ;
Vasudevan, AK ;
Stanzl-Tschegg, SE .
INTERNATIONAL JOURNAL OF FATIGUE, 2003, 25 (05) :397-411