Effects of heat treatment on prior particle boundary precipitation in a powder metallurgy nickel base superalloy

1995 ◽  
Vol 2 (3) ◽  
pp. 269-279 ◽  
Author(s):  
Yang Wanhong ◽  
Mao Jian ◽  
Wang Wuxiang ◽  
Zou Jinwen ◽  
Zhou Ruifa
Keyword(s):  
Heat Treatment ◽  
Powder Metallurgy ◽  
Nickel Base Superalloy ◽  
Prior Particle Boundary ◽  
Boundary Precipitation ◽  
Nickel Base ◽  
Particle Boundary ◽  
Base Superalloy

Microstructure Evolution during Supersolvus Heat Treatment of a Powder Metallurgy Nickel-Base Superalloy

2012 ◽  
Vol 43 (5) ◽  
pp. 1649-1661 ◽  
Author(s):  
S. L. Semiatin ◽  
K. E. McClary ◽  
A. D. Rollett ◽  
C. G. Roberts ◽  
E. J. Payton ◽  
...  
Keyword(s):  
Heat Treatment ◽  
Powder Metallurgy ◽  
Microstructure Evolution ◽  
Nickel Base Superalloy ◽  
Nickel Base ◽  
Base Superalloy

Effect of Pre-Weld Heat Treatment Temperatures on TIG Welded Microstructures on Nickel Base Superalloy, GTD-111

2015 ◽  
Vol 658 ◽  
pp. 14-18
Author(s):  
Tanaporn Rojhirunsakool ◽  
Duangkwan Thongpian ◽  
Nutthita Chuankrerkkul ◽  
Panyawat Wangyao
Keyword(s):  
Heat Treatment ◽  
High Temperature ◽  
Heat Treatment Temperature ◽  
Treatment Temperature ◽  
Tig Welding ◽  
Nickel Base Superalloy ◽  
Nickel Base ◽  
Base Superalloy ◽  
Weld Heat

Nickel-base superalloys have been used as high temperature materials in land-base gas turbine application. When subjected to long term, high temperature service, large crack propagation was observed. Typical refurbishment method of these turbines is carried out by using TIG welding followed by post-weld standard heat treatment. However, new crack initiation is found in the heat-affected zone after TIG welding. Pre-weld heat treatment has been discovered to improves final γ + γ’ microstructure. This study focuses on the effect of pre-weld heat treatment temperature on final γ + γ’ microstructure. Seven different conditions of pre-weld heat treatment temperature were investigated. Scanning electron microscopy studies were carried out after pre-weld and post-weld heat treatments to compare the γ + γ’ microstructure and capture microcracks. The best pre-weld heat treatment temperature produces uniform distribution of finely dispersed γ’ precipitates in the γ matrix without post-weld crack.

scholarly journals Effect of Heat Treatment Process on Microstructure and Fatigue Behavior of a Nickel-Base Superalloy

Materials ◽  
2015 ◽  
Vol 8 (9) ◽  
pp. 6179-6194 ◽  
Author(s):  
Peng Zhang ◽  
Qiang Zhu ◽  
Gang Chen ◽  
Heyong Qin ◽  
Chuanjie Wang
Keyword(s):  
Heat Treatment ◽  
Treatment Process ◽  
Fatigue Behavior ◽  
Nickel Base Superalloy ◽  
Heat Treatment Process ◽  
Nickel Base ◽  
Base Superalloy

Optimized hot workability of a powder metallurgy nickel-base superalloy

2019 ◽  
Vol 147 ◽  
pp. 340-352 ◽  
Author(s):  
Liming Tan ◽  
Yunping Li ◽  
Guoai He ◽  
Feng Liu ◽  
Yan Nie ◽  
...  
Keyword(s):  
Powder Metallurgy ◽  
Nickel Base Superalloy ◽  
Hot Workability ◽  
Nickel Base ◽  
Base Superalloy

Effect of heat treatment on superplastic response of powder-consolidated nickel-base superalloy IN 100

Metal Science ◽  
1982 ◽  
Vol 16 (7) ◽  
pp. 356-362 ◽  
Author(s):  
R. G. Menzies ◽  
G. J. Davies ◽  
J. W. Edington
Keyword(s):  
Heat Treatment ◽  
Nickel Base Superalloy ◽  
Nickel Base ◽  
Base Superalloy

Long-Term Gamma Prime Phase Stability after Various Heat Treatment Conditions with Temperature Dropping during Solution Treatment in Cast Nickel Base Superalloy, Grade Inconel-738

2017 ◽  
Vol 891 ◽  
pp. 420-425
Author(s):  
Sureerat Polsilapa ◽  
Aimamorn Promboopha ◽  
Panyawat Wangyao
Keyword(s):  
Heat Treatment ◽  
Turbine Blades ◽  
Solution Treatment ◽  
Nickel Base Superalloy ◽  
Gamma Prime ◽  
Nickel Based Superalloy ◽  
Treatment Conditions ◽  
Nickel Base ◽  
Base Superalloy

Cast nickel based superalloy, Grade Inconel 738, is a material for turbine blades. Its rejuvenation heat treatment usually consist of solution treatment condition with temperature range of 1125-1205 oC for 2-6 hours. Then it is following with double aging process including primary aging at 1055oC for 1 hour and secondary aging at 845oC for 24 hours. However, the various selected temperature dropping program were performed during solution treatment to simulate the possible error of heating furnace. The maximum number of temperature dropping during solution treatment is varied from 1-3 times From all obtained results, the various temperature dropping during solution treatment conditions showed extremely the significant effect on the final rejuvenated microstructures and long-term gamma prime stability after heating at temperature of 900oC for 200 hours.

Simulation of solidification and heat treatment of nickel-base superalloy SC16

2003 ◽  
Vol 94 (2) ◽  
pp. 139-143 ◽  
Author(s):  
B. Meurer ◽  
Ph. J. Spencer ◽  
D. Neuschütz
Keyword(s):  
Heat Treatment ◽  
Nickel Base Superalloy ◽  
Nickel Base ◽  
Base Superalloy

Effects of heat treatment on phase chemistry and microstructure of single crystal nickel base superalloy

1998 ◽  
Vol 4 (2) ◽  
pp. 146-152 ◽  
Author(s):  
A. A. Hopgood ◽  
A. Nicholls ◽  
G. D. W. Smith ◽  
J. W. Martin
Keyword(s):  
Heat Treatment ◽  
Single Crystal ◽  
Nickel Base Superalloy ◽  
Nickel Base ◽  
Phase Chemistry ◽  
Base Superalloy
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