The effect of aging on the serrated yielding and intermediate temperature embrittlement of nickel-base C-276 alloy

2018 ◽  
Vol 714 ◽  
pp. 59-67 ◽  
Author(s):  
Enxiang Pu ◽  
Wenjie Zheng ◽  
Zhigang Song ◽  
Ke Zhang ◽  
Shuang Liu ◽  
...  
2008 ◽  
Vol 59 (9) ◽  
pp. 991-994 ◽  
Author(s):  
S.A. Nalawade ◽  
M. Sundararaman ◽  
R. Kishore ◽  
J.G. Shah

2013 ◽  
Vol 32 (1) ◽  
pp. 7-13
Author(s):  
Sugui Tian ◽  
Xianlin Meng ◽  
Zeng Zeng ◽  
Chao Zhang ◽  
Chen Liu

AbstractBy means of creep curves measurement and microstructure observation, an investigation has been made into the influence of the element Re on creep behaviors of single crystal nickel-base superalloy at intermediate temperature. Results show that, after fully heat treated, microstructure of the alloy consists of the cubic γ′ phase embedded coherent in the γ matrix. Comparing with Re-free superalloy, 4.5% Re alloy displays a better creep resistance and longer creep rupture life in the ranges of the applied stresses and temperatures. After crept for 425 h up to fracture at 760 °C/800 MPa, the γ′ phase in the alloy keeps still the regular cubical configuration, which is attributed to the effect of the element Re decreasing the diffusing rate of other elements during creep. The deformation features of the alloy during creep are that the dislocations move in the γ matrix channels and shear into the γ′ phase, the 〈110〉 super-dislocation shearing into the γ′ phase may be decomposed to form the configuration of (1/3)〈112〉 super-Shockleys partials plus the stacking fault, which may hinder dislocations movement and restrain the cross-slipping of dislocations. This is thought to be the main reason of the alloy having a better creep resistance. In the latter stage of creep, the crack is firstly initiated in the interface of γ′/γ phases and propagated along the interface vertical to the stress axis up to the occurrence of the creep fracture, which is thought to be the fracture mechanism of the alloy during creep.


Author(s):  
P. S. Kotval ◽  
R. W. Calder

Cast nickel-base superalloys, used in turbine hardware, are typically composed of ~ 60 vol.% γ' phase coherently precipitated in an f.c.c. matrix, eutectic phases, and one or more carbide phases. These alloys are not heat-treatable in the sense of being able to re-solution and reprecipitate the γ' phase. Hence, the properties are governed by the as-cast microstructure which has become increasingly more complex as higher elevated-temperature strength has been required. This improvement in strength has an associated penalty in that the ambient and intermediate temperature ductility of cast superalloys is poor.Recently, it has been shown that additions of hafnium in nickel-base superalloys result in substantial improvements in ductility. The results presented here are from a study undertaken to define the role of hafnium in modifying microstructure in nickel-base alloys and the effect of this modification on properties.


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