GMR-235 Alloy

Alloy Digest ◽  
1968 ◽  
Vol 17 (2) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
General Motors ◽  
Jet Engine ◽  
Temperature Performance ◽  
Investment Cast ◽  
Nickel Base ◽  
Engine Components

Abstract GMR-235 Alloy is a nickel-base, precipitation-hardening alloy available in investment cast form for high temperature service. It is recommended for gas turbine and jet engine components operating in excess of 1400 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-131. Producer or source: Licensees of the General Motors Corporation.

CM-R 411

Alloy Digest ◽  
1967 ◽  
Vol 16 (9) ◽  
Keyword(s):  
Shear Strength ◽  
High Temperature ◽  
Gas Turbine ◽  
Precipitation Hardening ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Jet Engine ◽  
Temperature Performance ◽  
Nickel Base

Abstract CM-R41 is a vacuum-melted, precipitation hardening nickel-base alloy possessing outstanding properties in the temperature range of 1200 F to 1800 F. It is recommended for jet engine and gas turbine components operating at high temperatures. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-127. Producer or source: Cannon-Muskegon Corporation.

CARPENTER M-252

Alloy Digest ◽  
1973 ◽  
Vol 22 (9) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Gas Turbine ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Jet Engine ◽  
Temperature Performance ◽  
Nickel Base

Abstract CARPENTER M-252 is an age-hardenable nickel-base alloy designed for highly stressed parts operating at temperatures up to 1600 F. Its prime application is for jet-engine and gas-turbine buckets. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-195. Producer or source: Carpenter.

HAYNES ALLOY No. 713C

Alloy Digest ◽  
1961 ◽  
Vol 10 (3) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Precipitation Hardening ◽  
Cast Alloy ◽  
High Strength ◽  
Temperature Performance ◽  
Investment Cast ◽  
Nickel Base ◽  
Haynes Alloy

Abstract Haynes No. 713C is a nickel-base, vacuum melted, vacuum-cast alloy with excellent high-strength characteristics through 1800 F. It combines extraordinarily high strength with good ductility. It is a precipitation-hardening investment-cast alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as machining. Filing Code: Ni-64. Producer or source: Haynes Stellite Company.

IN-100

Alloy Digest ◽  
1970 ◽  
Vol 19 (3) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Base Alloy ◽  
Turbine Blades ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Temperature Performance ◽  
Investment Cast ◽  
Nickel Base

Abstract IN-100 is a vacuum melted and investment cast nickel-base alloy recommended for turbine blades operating at 1850-1900 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Ni-151. Producer or source: Howmet Corporation.

HASTELLOY ALLOY R-235

Alloy Digest ◽  
1965 ◽  
Vol 14 (1) ◽  
Keyword(s):  
Compressive Strength ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Union Carbide Corporation ◽  
Good Oxidation Resistance ◽  
Temperature Performance ◽  
Nickel Base

Abstract HASTELLOY ALLOY R-235 is a vacuum-melted nickel-base precipitation-hardening alloy with outstanding properties through 1750 F. It has good oxidation resistance, and a remarkable resistance to overaging in service. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-97. Producer or source: Union Carbide Corporation, Stellite Division.

ALLEGHENY LUDLUM 419

Alloy Digest ◽  
1967 ◽  
Vol 16 (7) ◽  
Keyword(s):  
Fracture Toughness ◽  
Compressive Strength ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Heat Treating ◽  
Tungsten Alloy ◽  
Jet Engine ◽  
Temperature Performance ◽  
Engine Components

Abstract Allegheny Ludlum 419 is a ferritic (martensitic) type chromium-tungsten alloy recommended for high temperature applications in the temperature range of 800-1200 F, such as turbine and jet engine components. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive strength as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-196. Producer or source: Allegheny Ludlum Corporation.

AISI No. 631

Alloy Digest ◽  
1965 ◽  
Vol 14 (5) ◽  
Keyword(s):  
Stainless Steel ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Nickel Aluminum ◽  
Jet Engine ◽  
Steel Mills ◽  
Temperature Performance

Abstract AISI No. 631 is chromium-nickel-aluminum precipitation hardening stainless steel recommended for aircraft, missile and jet engine parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-168. Producer or source: Alloy steel mills and foundries.

UDIMET N-115

Alloy Digest ◽  
1964 ◽  
Vol 13 (11) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Precipitation Hardening ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Large Forging ◽  
Temperature Performance ◽  
Nickel Base ◽  
Turbine Blading

Abstract Udimet N-115 is a vacuum-induction melted nickel-base alloy that responds to precipitation hardening. It is a superalloy for extended service to 1850 F. It has been thus far limited to barstock for turbine blading applications and may be suitable for existing or future large forging applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-95. Producer or source: Special Metals Inc..

UNITEMP 1753

Alloy Digest ◽  
1963 ◽  
Vol 12 (10) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Precipitation Hardening ◽  
High Strength ◽  
Heat Treating ◽  
Temperature Performance ◽  
Nickel Base

Abstract UNITEMP 1753 is a nickel-base precipitation hardening superalloy. It was developed for applications requiring wrought product with high strength and excellent oxidation resistance at temperatures up to about 1800 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-87. Producer or source: Universal Cyclops Steel Corporation.

UNITEMP 41

Alloy Digest ◽  
1981 ◽  
Vol 30 (4) ◽  
Keyword(s):  
Fracture Toughness ◽  
High Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Vacuum Melting ◽  
Jet Engine ◽  
Temperature Performance ◽  
High Temperature Alloys ◽  
Nickel Base ◽  
Engine Components

Abstract UNITEMP 41 is a nickel-base, precipitation-hardenable alloy that retains high strength and finds most use in the temperature range 1200 to 1800 F. It is produced by one or more vacuum melting practices. This alloy is one of the strongest high-temperature alloys that can be formed and welded in sheet form; consequently, it is used widely for jet engine components. Other uses include turbine buckets, turbine wheels, rings and high-temperature fasteners and springs. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-267. Producer or source: Cyclops Corporation.

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