Effect of pre-rafting on creep properties of Ni-based single crystal superalloy

Author(s):  
Wenyan Gan ◽  
Zhixun Wen ◽  
Haiqing Pei ◽  
Yamin Zhang ◽  
Hangshan Gao
China Foundry ◽  
2021 ◽  
Vol 18 (3) ◽  
pp. 185-191
Author(s):  
Xu-dong Wang ◽  
Zhong Yang ◽  
Qiang Gao ◽  
Li-rong Liu

2004 ◽  
Vol 461-464 ◽  
pp. 647-654 ◽  
Author(s):  
Sébastien Dryepondt ◽  
Daniel Monceau ◽  
Fabrice Crabos ◽  
Cyril Vernault

Author(s):  
Sébastien Dryepondt ◽  
Eric Andrieu ◽  
Daniel Monceau ◽  
Fabrice Crabos ◽  
Cyril Vernault

2018 ◽  
Vol 720 ◽  
pp. 69-74 ◽  
Author(s):  
YuZhang Lu ◽  
Guang Xie ◽  
Dong Wang ◽  
ShaoHua Zhang ◽  
Wei Zheng ◽  
...  

2010 ◽  
Vol 638-642 ◽  
pp. 2279-2284
Author(s):  
Jia Rong Li ◽  
Feng Li Sun ◽  
Ji Chun Xiong ◽  
Shi Zhong Liu ◽  
Mei Han

This work assesses the effects of the surface recrystallization of the processing of water grit blasting, grit blasting and mechanically polishing on the microstructures and creep rupture properties of DD6 alloy, a low-cost second generation single crystal superalloy. The results demonstrate that the possibility and the depth of the surface recrystallization of DD6 show an increase as the annealing temperature increases from 1050°C to 1250°C. No surface recrystallization happens when the specimens of the alloy have been undergone at 1100°C for 4 hours after water grit blasting, but the surface recrystallization occurs at the annealing temperature above 1200°C for 4 hours after water grit blasting. The test indicates that the increasing pre-deformation decreases the surface recrystallization temperature. The creep rupture life of DD6 alloy without processing is 274.4 hours, 341.1 hours at the conditions of 980°C/250MPa, 1070°C/140MPa respectively. After annealing at 1100°C for 4 hours, the creep rupture life of the alloy with the processing of water grit blasting is equivalent to that of the alloy without processing. The surface recrystallization of the alloy happens with the processing of grit blasting after the annealing at 1100°C for 4 hours, and there is a reduction of the creep rupture life at the conditions as mentioned above. The creep properties of DD6 alloy meet the needs of blades and vanes of single crystal for advanced aeroengines when the surface recrystallization of the alloy occurs during manufacturing and processing.


2014 ◽  
Vol 788 ◽  
pp. 459-465 ◽  
Author(s):  
De Long Shu ◽  
Su Gui Tian ◽  
Jing Wu ◽  
Zhong Ge Guo

The deformation and damage behaviors of a 4.5% Re nickel-based single crystal superalloy during creep at medium temperature were conducted by means of creep properties measurement and microstructure observation in the present investigation. The results show that the creep life of the superalloy was measured to be 226h at 820MPa/820oC, displaying a better creep resistance. After the alloy crept up to fracture, the γ′ phase in the region near fracture was contorted and coarsened, which is attributed to the severe plastic deformation. In the latter stage of creep, the main/secondary slipping systems were alternately activated to twist the γ′ and γ phases, which promoted the initiation of the cracks along the interfaces of γ′ /γ phases. And the micro-cracks may be propagated both along the direction vertical to the stress axis and along the direction of slipping traces, which is thought to be the main deformation and fracture mechanisms of the alloy in the latter stage of the creep.


2006 ◽  
Vol 70 (8) ◽  
pp. 690-693 ◽  
Author(s):  
Kyoko Kawagishi ◽  
Akihiro Sato ◽  
Toshiharu Kobayashi ◽  
Hiroshi Harada

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