Coherency loss in γ' precipitates in nickel-base superalloy

Author(s):  
R. A. Ricks ◽  
Angus J. Porter

During a recent investigation concerning the growth of γ' precipitates in nickel-base superalloys it was observed that the sign of the lattice mismatch between the coherent particles and the matrix (γ) was important in determining the ease with which matrix dislocations could be incorporated into the interface to relieve coherency strains. Thus alloys with a negative misfit (ie. the γ' lattice parameter was smaller than the matrix) could lose coherency easily and γ/γ' interfaces would exhibit regularly spaced networks of dislocations, as shown in figure 1 for the case of Nimonic 115 (misfit = -0.15%). In contrast, γ' particles in alloys with a positive misfit could grow to a large size and not show any such dislocation arrangements in the interface, thus indicating that coherency had not been lost. Figure 2 depicts a large γ' precipitate in Nimonic 80A (misfit = +0.32%) showing few interfacial dislocations.

Author(s):  
J. M. Oblak ◽  
B. H. Kear

During an investigation of recrystallization in the γ′ precipitation hardened nickel-base superalloy Udimet 700 many examples were found of fringe contrast at coherent matrix-γ′ interfaces. The properties of the fringes are those characteristic of so-called “δ-fringes”, as discussed by Gevers et al. A similar phenomenon has been observed in Ni-6.71 wt. % Al, and related to the formation of δ fringes by a tetragonal distortion of the γ matrix at the γ-γ′ interface. The interface fringes in Udimet 700 show surprisingly pronounced contrast despite the small difference in lattice parameter between γ and γ′ (<0.1% vs 0.5% in binary Ni-Al).


2013 ◽  
Vol 575-576 ◽  
pp. 394-397
Author(s):  
Xiang Feng Liang ◽  
Yu Tao Zhao ◽  
Zhen Li Zuo ◽  
Zhi Hong Jia

In this paper, we use the High rate solidification to study process parameters and CMSX-6 super-alloy solidification structure. And then, it can provide more basis for the industrial directionally solidified casting of superalloys blades. The results show that: under certain process parameters, it can be obtained parallel columnar crystals directional solidification structure. The organization is composed of the matrix γ phase and the secondary precipitated γ ' phase; under an optical microscope, it can be observed the shrinkage porosity due to the volumes reduction arising solidification.


Author(s):  
M.G. Burke ◽  
R. Bajaj

Direct-aged alloy 625 (DA-A625) is a precipitation-hardened nickel-base superalloy with good mechanical properties and excellent corrosion resistance. Its superior stress corrosion cracking (SCC) performance makes it a candidate material for applications in light water reactors where resistance to irradiation-assisted SCC (IASCC) is important. This alloy derives its strength from the intragranular precipitation of fine DO22 – ordered γ” precipitates. These precipitates have a disc-like morphology and are crystallo-grahically related to the γ matrix such that the [001] axis of the precipitates are oriented parallel to <100> directions in the matrix. This alloy is generally solution-annealed then aged within the temperature range ~600 to 750°C. In direct-aging, the alloy is immediately aged at ~ 660°C for 80 h following hot-working. In addition to the γ° precipitates, intergranular M23C6, M7C3, M6C, or MC carbides can form in this material.


2010 ◽  
Vol 654-656 ◽  
pp. 512-515
Author(s):  
Su Gui Tian ◽  
Shu Zhang ◽  
Li Li Yu ◽  
Hui Chen Yu ◽  
Ben Jiang Qian

An investigation has been made into the microstructure and creep behaviors of [110] oriented single crystal nickel-base superalloy. Results show that, after a full heat treated, the cubic  phase is coherently embedded in the matrix and regularly arranged along the <100> orientation. During creep, the cubic phase in the alloy is transformed into the rafted structure lying 45 relative to the direction of the applied stress. Under the condition of the applied stress of 137 MPa at 1040°C, the alloy displays a higher strain rate and shorter creep lifetime. The deformation mode of the alloy during creep is dislocations activated within the matrix channels and the rafted phase. Dislocation slip activated easily on the Roof-type channel is thought to be the main reason of the alloy having higher strain rate and shorter creep lifetime.


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