UDIMET M-252

Alloy Digest ◽  
1967 ◽  
Vol 16 (5) ◽  
Keyword(s):  
High Temperature ◽  
Elevated Temperatures ◽  
Rupture Strength ◽  
Stress Rupture ◽  
Heat Treating ◽  
Age Hardening ◽  
Heavy Duty ◽  
Induction Method ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract UDIMET M-252 is a vacuum induction method alloy recommended for heavy-duty high temperature applications in the range 1300-1600 F. It has good stress-rupture strength, fatigue strength and mechanical strength at elevated temperatures. The alloy responds to an age-hardening heat treatment. 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, and joining. Filing Code: Ni-124. Producer or source: Special Metals Inc..

MST 2.5Al-16V

Alloy Digest ◽  
1960 ◽  
Vol 9 (2) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Elevated Temperatures ◽  
Base Alloy ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract MST 2.5A1-16V is a titanium-base alloy having a favorable combination of strength, formability and resistance to creep at elevated temperatures. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength 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: Ti-24. Producer or source: Mallory-Sharon Metals Company.

ALUMINUM 6151

Alloy Digest ◽  
1958 ◽  
Vol 7 (7) ◽  
Keyword(s):  
Heat Treatment ◽  
Shear Strength ◽  
High Temperature ◽  
Physical Properties ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Aluminum Company ◽  
Aluminum Forging ◽  
Hardening Heat Treatment

Abstract ALUMINUM 6151, formerly A51S Alloy, is an aluminum forging alloy combining good forgeability, strength, and resistance to corrosion. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-67. Producer or source: Aluminum Company of America.

TECHALLOY WASPALOY

Alloy Digest ◽  
1977 ◽  
Vol 26 (4) ◽  
Keyword(s):  
Elevated Temperatures ◽  
Rupture Strength ◽  
Stress Rupture ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Solid Solution Strengthening ◽  
Solution Strengthening ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract TECHALLOY WASPALOY, a nickel-base austenitic precipitation-hardenable alloy, derives its high strength at elevated temperatures from additions of the solid-solution strengthening elements molybdenum, cobalt and chromium and from aluminum and titanium which produce age hardening. Boron and zirconium additions also have been made to obtain optimum stress-rupture strength. It has excellent strength and good resistance to corrosion and oxidation at least to 1600 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 corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-243. Producer or source: Techalloy Company Inc..

Ti-5Al-4FeCr

Alloy Digest ◽  
1969 ◽  
Vol 18 (6) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Titanium Alloy ◽  
High Temperature ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Alpha Beta ◽  
Hardening Heat Treatment

Abstract Ti-5A1-4FeCr is an alpha-beta type titanium alloy recommended for airframe components. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-58. Producer or source: Titanium alloy mills.

ALLVAC 718

Alloy Digest ◽  
1964 ◽  
Vol 13 (4) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Iron Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Nickel Chromium ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract Allvac 718 is a nickel-chromium-iron alloy that responds to an age-hardening heat treatment. It is recommended for parts requiring high strength and oxidation resistance up to about 1300 F and particularly for such parts that require welding. 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, machining, joining, and surface treatment. Filing Code: Ni-90. Producer or source: Allvac 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.

CLIMELT MOLYBDENUM-0.5%Ti-0.08%Zr

Alloy Digest ◽  
1961 ◽  
Vol 10 (10) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Rupture Strength ◽  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Recrystallization Temperature ◽  
Ti Alloy ◽  
Temperature Performance

Abstract Climelt Molybdenum-0.5 Ti-0.08 Zr is a molybdenum-base alloy that offers substantial benefits for high temperature applications. It has higher recrystallization temperature, and better stress-rupture strength than unalloyed molybdenum and the Mo-0.5% Ti alloy. This datasheet provides information on composition, physical properties, hardness, and elasticity 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: Mo-3. Producer or source: Climax Molybdenum Company.

ALLEGHENY S-816

Alloy Digest ◽  
1962 ◽  
Vol 11 (4) ◽  
Keyword(s):  
Mechanical Properties ◽  
Elevated Temperatures ◽  
Heat Treating ◽  
High Heat ◽  
Age Hardening ◽  
Corrosion Resistant ◽  
Temperature Performance ◽  
Corrosion Resistant Alloy ◽  
Oxidation And Corrosion ◽  
Hardening Heat Treatment

Abstract ALLEGHENY LUDLUM ALLOY S-816 is a high heat and corrosion resistant alloy, responding to age-hardening heat treatment. It has high mechanical properties at elevated temperatures, and is oxidation and corrosion resistant. 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, and joining. Filing Code: Co-3. Producer or source: Allegheny Ludlum Corporation. Originally published August 1953, revised April 1962.

ECLIPSALOY 517

Alloy Digest ◽  
1956 ◽  
Vol 5 (11) ◽  
Keyword(s):  
Heat Treatment ◽  
Compressive Strength ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Heat Treating ◽  
Age Hardening ◽  
Casting Alloy ◽  
Good Corrosion Resistance ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract ECLIPSALOY 517 is a cerium-magnesium sand casting alloy having excellent creep resistance up to 500 deg. F. It is suitable for applications where pressure tightness is required and good corrosion resistance is important. It responds to an age-hardening heat treatment. 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 casting, heat treating, machining, and joining. Filing Code: Mg-29. Producer or source: Bendix Aviation Corporation.

ALUMINUM 122

Alloy Digest ◽  
1957 ◽  
Vol 6 (2) ◽  
Keyword(s):  
High Temperature ◽  
High Hardness ◽  
Heat Treating ◽  
Age Hardening ◽  
High Temperature Strength ◽  
Temperature Performance ◽  
Aluminum Company ◽  
Mold Casting ◽  
Resistance To Wear ◽  
Hardening Heat Treatment

Abstract ALUMINUM 122 is an aluminum sand and permanent mold casting alloy recommended for applications where good high temperature strength, high hardness, resistance to wear and good machinability are required. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Al-48. Producer or source: Aluminum Company of America.

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