The Precipitation Behavior of γ′ Phase in Single Crystal Ni-Based DD6 Superalloy for Turbine Blade

2017 ◽  
Vol 898 ◽  
pp. 534-544
Author(s):  
Y.P. Xue ◽  
Jia Rong Li ◽  
Jin Qian Zhao ◽  
J.C. Xiong

The precipitation behavior of γ′ precipitates in typical section dimensions of DD6 single crystal superalloy turbine blade was investigated experimentally during directional solidification process. The phase transformation temperatures in the single crystal Ni-based DD6 superalloy from DSC analysis and JmatPro simulation were basically in consistent with the isothermal solidification experiments. The solidification route of DD6 single crystal superalloy could be described as follows: L1 → γ + L2; L2 → (γ + γ′)eutectic + MC; γ → γ′/γ. With increasing continuous cooling rates, the primary γ′ precipitates tended to be refined, and the size distributions of the primary γ′ precipitates at every temperature measuring position followed the normal distribution. In comparison to the interdendritic regions, nearly a 60% reduction in the average sizes of the primary γ′ precipitates was measured in the dendritic core regions. The result of the primary γ′ size difference was strongly affected by the multi-component segregations between the interdendritic and dendritic regions, where the γ′ forming elements of Al and Ta segregated towards the interdendritic regions. Furthermore, the secondary γ′ precipitation was found to occur within a relatively wide corridor of γ matrix for low cooling rates (12.6, 23.3 and 29.7 °C/min) during the directional solidification process. The occurrence of the secondary γ′ precipitation resulted from the complex interaction of multiple thermodynamic and kinetic factors in the γ′ nucleation and the diffusion rate of γ′ forming elements.

JOM ◽  
2010 ◽  
Vol 62 (5) ◽  
pp. 30-34 ◽  
Author(s):  
Dong Pan ◽  
Qingyan Xu ◽  
Baicheng Liu ◽  
Jiarong Li ◽  
Hailong Yuan ◽  
...  

2013 ◽  
Vol 712-715 ◽  
pp. 991-996
Author(s):  
Shi Feng Li ◽  
Ding Hua Zhang ◽  
Kun Bu ◽  
Qiu Sheng Luo

The cracks were found on the surface of DD6 single crystal turbine blade. The blade fracture mode and causing reason were studied by analyzing the fracture surface and the microstructure in the vicinity of the cracks using Optical Microscope (OM) and Scanning Electron Microscope (SEM). The results indicated that the cracks fracture was resulted from the surface recrystallization of the blade. Owing to the presence of cast stress in the blade during the directional solidification process, a later solution treatment resulted in the formation of recrystallization grains. Meanwhile, some white particles with high concentration of W were precipitated at the grain boundary. Under the testing condition, the cracks initiated at the recrystallization boundary and expanded along the white precipitated phases until fatigue fracture.


1997 ◽  
Vol 12 (12) ◽  
pp. 3199-3202 ◽  
Author(s):  
R. Cloots ◽  
Fr. Auguste ◽  
A. Rulmont ◽  
N. Vandewalle ◽  
M. Ausloos

A Dy2O3 single crystal has been used as a seed for the growth of isothermally melt-textured Dy-123 material. The nucleation-controlled step has been observed to be related to the heterogeneous nucleation of 211 particles at the surface of the dysprosium oxide single crystal. The subsequent growth mode seems to be controlled by a high concentration gradient of dysprosium in the liquid phase. This leads to a directional solidification process of the 123 phase. The size of the 211 particles seems to decrease as the distance from the dysprosium oxide single crystal increases.


Metals ◽  
2018 ◽  
Vol 8 (8) ◽  
pp. 632 ◽  
Author(s):  
Qingyan Xu ◽  
Cong Yang ◽  
Hang Zhang ◽  
Xuewei Yan ◽  
Ning Tang ◽  
...  

Ni-based superalloy turbine blades have become indispensable structural parts in modern gas engines. An understanding of the solidification behavior and microstructure formation in directional solidified turbine blades is necessary for improving their high-temperature performance. The multiscale simulation model was developed to simulate the directional solidification process of superalloy turbine blades. The 3D cellular automaton-finite difference (CA-FD) method was used to calculate heat transfer and grain growth on the macroscopic scale, while the phase-field method was developed to simulate dendrite growth on the microscopic scale. Firstly, the evolution of temperature field of an aero-engine blade and a large industrial gas turbine blade was studied under high-rate solidification (HRS) and liquid-metal cooling (LMC) solidification processes. The varying withdrawal velocity was applied to change the curved mushy zone to a flat shape. Secondly, the grain growth in the aero-engine blade was simulated, and the grain structures in the starter block part and the spiral selector part in the HRS process were compared with those in the LMC process. The simulated grain structures were generally in agreement with experimental results. Finally, the dendrite growth in the typical HRS and LMC solidification process was investigated and the simulation results were compared with the experimental results in terms of dendrite morphology and primary dendritic spacing.


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