WASPALOY

Alloy Digest ◽  
1967 ◽  
Vol 16 (11) ◽  
Keyword(s):  
Rupture Strength ◽  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Union Carbide Corporation ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract WASPALOY is a vacuum induction melted nickel-base alloy having outstanding tensil and stress-rupture strength up to 1400 F combined with high oxidation resistance up to 1600 F. It is recommended for gas turbine engines, airframe assemblies and missile systems. 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, joining, and surface treatment. Filing Code: Ni-129. Producer or source: Union Carbide Corporation, Materials Systems Division.

HAYNES WASPALOY

Alloy Digest ◽  
2000 ◽  
Vol 49 (3) ◽  
Keyword(s):  
Rupture Strength ◽  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Temperature Performance ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract Haynes Waspaloy is a specially vacuum melted, nickel-base alloy having outstanding tensile and stress-rupture strength up to 760 deg C (1400 deg F) combined with high oxidation resistance up to 871 deg C (1600 deg F). It is recommended for gas turbine engines, airframe assemblies, and missile systems. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating and machining. Filing Code: Ni-560. Producer or source: Haynes International Inc.

UDIMET WASPALOY

Alloy Digest ◽  
1978 ◽  
Vol 27 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Rupture Strength ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Temperature Performance ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-257. Producer or source: Special Metals Corporation.

AISI No. 685

Alloy Digest ◽  
1981 ◽  
Vol 30 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Rupture Strength ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Temperature Performance ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract AISI No. 685 is a nickel-base, austenitic, precipitation-hardenable alloy. It has excellent tensile and stress-rupture strength to 1400 F and high resistance to corrosion and oxidation at temperatures at least to 1600 F. It is used widely in airframe assemblies, gas turbine engines and missile systems. This datasheet provides information on composition, physical properties, hardness, 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 forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-271. Producer or source: Nickel alloy mills.

CRUCIBLE CG27

Alloy Digest ◽  
1969 ◽  
Vol 18 (1) ◽  
Keyword(s):  
High Temperature ◽  
Tensile Properties ◽  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
High Temperature Stress ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Iron Nickel ◽  
Nickel Base

Abstract Crucible CG27 is a forgeable iron-nickel base alloy having an excellent combination of high temperature stress-rupture and tensile properties. It resists oxidation up to 1500 F and is recommended for gas turbine engines and turbine wheels. 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: SS-219. Producer or source: Crucible Materials Corporation.

ALLOY 713LC

Alloy Digest ◽  
1966 ◽  
Vol 15 (10) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Rupture Strength ◽  
Base Alloy ◽  
High Stress ◽  
Stress Rupture ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Temperature Performance ◽  
Nickel Base

Abstract ALLOY 713LC is a nickel-base alloy possessing high stress-rupture strength up to 1700 F combined with excellent resistance to thermal fatigue. It is recommended for turbine wheels. 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 casting, heat treating, machining, and joining. Filing Code: Ni-118. Producer or source: Austenal Microcast Division, Howmet Corporation.

NIMONIC 93

Alloy Digest ◽  
1970 ◽  
Vol 19 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Base Alloy ◽  
Heat Treating ◽  
Elevated Temperature Strength ◽  
Jet Engine ◽  
Good Corrosion Resistance ◽  
Temperature Performance ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract NIMONIC 93 is a nickel-base alloy having high elevated temperature strength, high oxidation resistance and good corrosion resistance. It is recommended for jet engine and gas turbine components. 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-153. Producer or source: Henry Wiggin & Company Ltd.

HASTELLOY ALLOY N

Alloy Digest ◽  
1960 ◽  
Vol 9 (2) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Temperature Performance ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract HASTELLOY ALLOY N is a high temperature nickel-base alloy having high oxidation resistance and freedom from aging embrittlement. This datasheet provides information on composition, physical properties, 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 forming, heat treating, machining, and joining. Filing Code: Ni-55. Producer or source: Haynes Stellite Company.

PYROMET ALLOY 80A

Alloy Digest ◽  
1989 ◽  
Vol 38 (10) ◽  
Keyword(s):  
High Temperature ◽  
Base Alloy ◽  
Heat Treating ◽  
Fatigue Properties ◽  
High Oxidation ◽  
High Fatigue ◽  
Technology Corporation ◽  
High Oxidation Resistance ◽  
Carpenter Technology Corporation ◽  
Nickel Base

Abstract PYROMET Alloy 80A, a high-temperature nickel-base alloy is characterized by its excellent creep resistance, high fatigue properties under very arduous conditions and high oxidation resistance. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-189. Producer or source: Carpenter Technology Corporation. Originally published April 1973, revised October 1989.

G-E ALLOY RENE 62

Alloy Digest ◽  
1965 ◽  
Vol 14 (9) ◽  
Keyword(s):  
Physical Properties ◽  
Precipitation Hardening ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
General Electric Company ◽  
Electric Company ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract G-E Alloy Rene 62 is a vacuum melted nickel-base alloy having good weldability and high oxidation resistance. It is recommended for highly stressed structures which operate up to 1500/'B0F. It is a precipitation hardening alloy. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ni-105. Producer or source: General Electric Company.

MAR-M Alloy 246

Alloy Digest ◽  
1968 ◽  
Vol 17 (6) ◽  
Keyword(s):  
Precipitation Hardening ◽  
Operating Temperature ◽  
Rupture Strength ◽  
Base Alloy ◽  
Heat Treating ◽  
Solid Solution Strengthening ◽  
Temperature Performance ◽  
Solution Strengthening ◽  
Nickel Base ◽  
Operating Temperature Range

Abstract MAR-M alloy 246 is a vacuum-cast nickel-base alloy combining precipitation hardening and solid solution strengthening. It has high rupture strength and adequate ductility in the recommended operating temperature range of 1200-1900 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Ni-134. Producer or source: Martin Metals Division.

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