CREEP-FATIGUE CRACK GROWTH AND FRACTOGRAPHY OF METALLIC MATERIALS IN AIR AND VACUUM AT ELEVATED TEMPERATURES

Author(s):  
Ryoichi Koterazawa
1993 ◽  
Vol 42 (474) ◽  
pp. 297-303 ◽  
Author(s):  
Ryoichi KOTERAZAWA ◽  
Nobuhiro YAMAZAKI ◽  
Masahiro MORISHITA ◽  
Satoru HORIOKA ◽  
Takayoshi NOSHO

Materials ◽  
2022 ◽  
Vol 15 (2) ◽  
pp. 651
Author(s):  
Jianxing Mao ◽  
Zhixing Xiao ◽  
Dianyin Hu ◽  
Xiaojun Guo ◽  
Rongqiao Wang

The creep-fatigue crack growth problem remains challenging since materials exhibit different linear and nonlinear behaviors depending on the environmental and loading conditions. In this paper, we systematically carried out a series of creep-fatigue crack growth experiments to evaluate the influence from temperature, stress ratio, and dwell time for the nickel-based superalloy GH4720Li. A transition from coupled fatigue-dominated fracture to creep-dominated fracture was observed with the increase of dwell time at 600 °C, while only the creep-dominated fracture existed at 700 °C, regardless of the dwell time. A concise binomial crack growth model was constructed on the basis of existing phenomenal models, where the linear terms are included to express the behavior under pure creep loading, and the nonlinear terms were introduced to represent the behavior near the fracture toughness and during the creep-fatigue interaction. Through the model implementation and validation of the proposed model, the correlation coefficient is higher than 0.9 on ten out of twelve sets of experimental data, revealing the accuracy of the proposed model. This work contributes to an enrichment of creep-fatigue crack growth data in the typical nickel-based superalloy at elevated temperatures and could be referable in the modeling for damage tolerance assessment of turbine disks.


2012 ◽  
Vol 41 (9) ◽  
pp. 2463-2469 ◽  
Author(s):  
Kittichai Fakpan ◽  
Yuichi Otsuka ◽  
Yoshiharu Mutoh ◽  
Shunsuke Inoue ◽  
Kohsoku Nagata ◽  
...  

2019 ◽  
Vol 36 (6) ◽  
pp. 562-574 ◽  
Author(s):  
N. Shaber ◽  
R. Stephens ◽  
J. Ramirez ◽  
G. P. Potirniche ◽  
M. Taylor ◽  
...  

2013 ◽  
Vol 577-578 ◽  
pp. 625-628
Author(s):  
Hao Liu ◽  
Rui Bao ◽  
Wei Ming Lei ◽  
Bin Jun Fei

For the components working in high temperature and enduring fatigue loading, the fatigue fracture properties will be reduced remarkably when the working temperature is higher than the critical temperature of creep-fatigue interactionTcof the material. In consequence, the damage mechanism from creep-fatigue interaction becomes more complex. A method is presented in this paper to determine theTcof a nickel-based powder metallurgy superalloy. Pure fatigue crack growth and creep-fatigue crack growth tests were conducted in several different elevated temperatures. The fracture mechanism was investigated via observing the fractographic characteristics using scanning electron microscope (SEM). The test results show that theTcof this superalloy is a little bit lower than a half of the melting temperatureTm.


2010 ◽  
Vol 4 (9) ◽  
pp. 1410-1426 ◽  
Author(s):  
Tae Wuk WOO ◽  
Masao SAKANE ◽  
Kwang Soo KIM ◽  
Kaoru KOBAYASHI ◽  
Hyun Chul PARK

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