ALTEMP X-750

Alloy Digest ◽  
2007 ◽  
Vol 56 (5) ◽  
Keyword(s):  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Structural Components ◽  
Creep Properties ◽  
Chemical Corrosion ◽  
Temperature Performance ◽  
Suitable Heat Treatment ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract Altemp X-750 is a precipitation-hardenable nickel-base alloy that is highly resistant to chemical corrosion and oxidation and has excellent stress-rupture and creep properties at temperatures up to 815 deg C (1500 deg F) after suitable heat treatment. The alloy has oxidation resistance up to 980 deg C (1800 deg F). It is typically used in aircraft turbine and structural components. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ni-649. Producer or source: Allegheny Ludlum.

PYROMET X-750

Alloy Digest ◽  
1971 ◽  
Vol 20 (3) ◽  
Keyword(s):  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Creep Properties ◽  
Chemical Corrosion ◽  
Suitable Heat Treatment ◽  
Technology Corporation ◽  
Carpenter Technology Corporation ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract PYROMET X-750 is a precipitation-hardenable nickel-base alloy that is highly resistant to chemical corrosion and oxidation and has excellent stress-rupture and creep properties at temperatures up to 1500 F after suitable heat treatment. 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 forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-163. Producer or source: Carpenter Technology Corporation.

INCONEL X

Alloy Digest ◽  
1953 ◽  
Vol 2 (3) ◽  
Keyword(s):  
High Temperature ◽  
Base Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Chemical Corrosion ◽  
International Nickel Company ◽  
Temperature Performance ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract INCONEL X is a high-strength, high-temperature nickel-base alloy responding to age hardening for maximum properties. It is highly resistant to chemical corrosion and oxidation. Its creep rate is low under high stresses at 1200-1500 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 high temperature performance as well as heat treating, machining, joining, and surface treatment. Filing Code: Ni-3. Producer or source: International Nickel Company Inc..

PYROMET 751

Alloy Digest ◽  
1986 ◽  
Vol 35 (7) ◽  
Keyword(s):  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Chemical Corrosion ◽  
Stress Rupture Properties ◽  
Technology Corporation ◽  
Carpenter Technology Corporation ◽  
Nickel Base ◽  
Rupture Properties ◽  
Corrosion And Oxidation

Abstract PYROMET 751 is an age-hardenable nickel-base alloy with good stress-rupture properties to 1600 F. Its creep rate is low under high stresses at 1200-1500 F. It is highly resistant to chemical corrosion and oxidation. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-335. Producer or source: Carpenter Technology Corporation.

PYROMET X-751

Alloy Digest ◽  
1973 ◽  
Vol 22 (5) ◽  
Keyword(s):  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Chemical Corrosion ◽  
Stress Rupture Properties ◽  
Technology Corporation ◽  
Carpenter Technology Corporation ◽  
Nickel Base ◽  
Rupture Properties ◽  
Corrosion And Oxidation

Abstract PYROMET X-751 is an age hardenable nickel-base alloy with good stress-rupture properties at 1600 F. It is highly resistant to chemical corrosion and oxidation. 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-190. Producer or source: Carpenter Technology Corporation.

UDIMET 41

Alloy Digest ◽  
1964 ◽  
Vol 13 (6) ◽  
Keyword(s):  
High Temperature ◽  
Elevated Temperature ◽  
Physical Properties ◽  
Precipitation Hardening ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Temperature Performance ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract UDIMET 41 is a vacuum induction melted precipitation hardening nickel-base alloy having outstanding room and elevated temperature properties. It possesses excellent corrosion and oxidation resistance. It is designed for highly stressed components operating in the 1400-1700 deg F temperature range. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-92. Producer or source: Special Metals Inc..

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.

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.

NICRIMPHY 600

Alloy Digest ◽  
2006 ◽  
Vol 55 (3) ◽  
Keyword(s):  
Mechanical Properties ◽  
Corrosion Resistance ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Temperature Performance ◽  
Precision Alloys ◽  
Wide Range ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract Nicrimphy 600 is a nickel-base alloy designed to offer good corrosion and oxidation resistance. It also has good mechanical properties over a wide range of temperatures. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-633. Producer or source: Metalimphy Precision Alloys Inc.

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.

INCONEL 700

Alloy Digest ◽  
1960 ◽  
Vol 9 (11) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Base Alloy ◽  
High Stress ◽  
Stress Rupture ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
International Nickel Company ◽  
Temperature Performance ◽  
Nickel Base

Abstract INCONEL 700 is an age-hardenable heat and corrosion resisting nickel-base alloy. It has high stress-rupture characteristics. 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 forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-33. Producer or source: International Nickel Company Inc.. Originally published April 1957, revised November 1960.

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