The Effect of Environment on the Stress-Rupture Properties of Metals at Elevated Temperatures

2009 ◽  
pp. 34-34-8
Author(s):  
O. Cutler Shepard ◽  
Willis Schalliol
Keyword(s):  
Elevated Temperatures ◽  
Stress Rupture ◽  
Stress Rupture Properties ◽  
Rupture Properties

New Iron-Based ODS-Superalloys for High Demanding Applications

1991 ◽  
Author(s):  
G. Korb ◽  
M. Rühle ◽  
H.-P. Martinz
Keyword(s):  
High Temperatures ◽  
Elevated Temperatures ◽  
Stress Rupture ◽  
Gas Content ◽  
Processing Route ◽  
Process Technology ◽  
Hot Gas ◽  
Stress Rupture Properties ◽  
Gas Corrosion ◽  
Rupture Properties

Some shortcomings of the commercial alloy MA 956 like insufficient hot gas corrosion resistance at extremely high temperatures or porous welding seams as a result of residual inert gas content, have been overcome by slightly changing the chemical composition, and a generally improved process technology. The mainly developed “work horse”-alloy PM 2000 - exhibits additionally significantly better stress-rupture properties at high temperatures. Workability even down to small dimensions is good, when an especially adapted processing route is applied. In this paper data of tensile strength and stress rupture properties are given for elevated temperatures. Hot gas corrosion behaviour is demonstrated for isothermally and cyclicly treated materials, including thermal shock tests. Some results of a burner rig test are presented additionally. Resistance against different molten slags, salts and glasses has been investigated and is discussed.

UNITEMP 188

Alloy Digest ◽  
1990 ◽  
Vol 39 (10) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Elevated Temperatures ◽  
Stress Rupture ◽  
High Strength ◽  
Heat Treating ◽  
Creep And Stress Rupture ◽  
Stress Rupture Properties ◽  
Specialty Steel ◽  
Rupture Properties ◽  
Oxidation And Corrosion

Abstract UNITEMP 188 provides outstanding oxidation and corrosion resistance, high strength at elevated temperatures, excellent creep and stress-rupture properties and thermal fatigue resistance. This datasheet provides information on composition, physical properties, and elasticity as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-80. Producer or source: Cytemp Specialty Steel Division, Cyclops. Originally published July 1983, revised October 1990.

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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