scholarly journals Microstructure evolution and stress rupture properties of A286 superalloy in the 600 to 750 °C temperature range

2021 ◽  
Vol 8 (2) ◽  
pp. 026521
Author(s):  
Li Wei ◽  
Hongjin Zhao ◽  
Yongqing Sun ◽  
Yan Zhang ◽  
Bo Zhao ◽  
...  
Keyword(s):  
Microstructure Evolution ◽  
Stress Rupture ◽  
Temperature Range ◽  
Stress Rupture Properties ◽  
Rupture Properties

Microstructure evolution and stress-rupture properties of Nimonic 80A after various heat treatments

2013 ◽  
Vol 47 ◽  
pp. 218-226 ◽  
Author(s):  
Yulai Xu ◽  
Caixiong Yang ◽  
Qingxuan Ran ◽  
Pengfei Hu ◽  
Xueshan Xiao ◽  
...  
Keyword(s):  
Microstructure Evolution ◽  
Stress Rupture ◽  
Heat Treatments ◽  
Stress Rupture Properties ◽  
Nimonic 80A ◽  
Rupture Properties

CDA 710

Alloy Digest ◽  
1970 ◽  
Vol 19 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
High Resistance ◽  
Stress Rupture ◽  
Heat Treating ◽  
Temperature Performance ◽  
Seawater Corrosion ◽  
Stress Rupture Properties ◽  
Rupture Properties

Abstract CDA 710 is a cupro-nickel alloy having high resistance to seawater corrosion and good stress-rupture properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Cu-215. Producer or source: Anaconda American Brass Company.

FANSTEEL 42

Alloy Digest ◽  
1965 ◽  
Vol 14 (4) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Recrystallization Temperature ◽  
Stress Rupture Properties ◽  
Rupture Properties

Abstract FANSTEEL 42 Metal is a molybdenum-base alloy recommended for high temperature applications. It has high recrystallization temperature and good stress-rupture properties. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, joining, and surface treatment. Filing Code: Mo-6. Producer or source: Fansteel Metallurgical Corporation.

AISI No. 664

Alloy Digest ◽  
1981 ◽  
Vol 30 (7) ◽  
Keyword(s):  
High Temperature ◽  
Stress Rupture ◽  
Heat Treating ◽  
Good Combination ◽  
Creep And Stress Rupture ◽  
High Temperature Alloy ◽  
Vacuum Melting ◽  
Stress Rupture Properties ◽  
Nickel Base ◽  
Rupture Properties

Abstract AISI No. 664 is a nickel-base high-temperature alloy that can be precipitation hardened because of its contents of aluminum and titanium. Vacuum melting is used in its production to provide excellent quality and reproducability. It is used for applications requiring a good combination of creep and stress-rupture properties up to about 1500 F. Typical applications are gas-turbine components, airframes and fasteners. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-269. Producer or source: Nickel alloy producers.

Influence of element Re on lattice misfits and stress rupture properties of single crystal nickel-based superalloys

2010 ◽  
Vol 527 (16-17) ◽  
pp. 4458-4465 ◽  
Author(s):  
Tian Sugui ◽  
Wang Minggang ◽  
Yu Huichen ◽  
Yu Xingfu ◽  
Li Tang ◽  
...  
Keyword(s):  
Single Crystal ◽  
Stress Rupture ◽  
Stress Rupture Properties ◽  
Rupture Properties
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