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.

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.

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..

REFRACTALOY 26

Alloy Digest ◽  
1954 ◽  
Vol 3 (2) ◽  
Keyword(s):  
Precipitation Hardening ◽  
Elevated Temperatures ◽  
Heat Treating ◽  
High Heat ◽  
Heat Resistant Alloy ◽  
Nickel Chromium ◽  
Temperature Performance ◽  
Westinghouse Electric Corporation ◽  
Westinghouse Electric ◽  
Hardening Heat Treatment

Abstract REFRACTALOY 26 is a high heat resistant alloy of nickel, chromium, cobalt and iron, possessing high creep and endurance strengths along with high ductility at elevated temperatures. It responds to precipitation-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-8. Producer or source: Westinghouse Electric Corporation.

CHROMIUM COPPER-182

Alloy Digest ◽  
1967 ◽  
Vol 16 (3) ◽  
Keyword(s):  
Heat Treatment ◽  
High Temperature ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
High Temperature Solution ◽  
Corrosion Resistant ◽  
Temperature Performance ◽  
Temperature Solution ◽  
Corrosion Resistant Alloy ◽  
Hardening Heat Treatment

Abstract Chromium Copper-182 is a copper-chromium corrosion resistant alloy which is softened by a high-temperature solution anneal and quench, and will improved acquire properties with a low temperature precipitation-hardening heat treatment. 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, and joining. Filing Code: Cu-174. Producer or source: Anaconda American Brass Company.

ALCAN 28S

Alloy Digest ◽  
1956 ◽  
Vol 5 (2) ◽  
Keyword(s):  
Mechanical Properties ◽  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Aluminum Company ◽  
Screw Machine ◽  
Hardening Heat Treatment

Abstract ALCAN 28S is a free-cutting alloy having good mechanical properties. It responds to an age-hardening heat treatment and is designed primarily for screw machine products. 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 forming, heat treating, and machining. Filing Code: Al-36. Producer or source: Aluminum Company of Canada Ltd.

CONDULOY

Alloy Digest ◽  
1953 ◽  
Vol 2 (10) ◽  
Keyword(s):  
Mechanical Properties ◽  
Heat Treatment ◽  
Physical Properties ◽  
Tensile Properties ◽  
Copper Alloy ◽  
Heat Treating ◽  
Age Hardening ◽  
Beryllium Copper ◽  
Hardening Heat Treatment

Abstract CONDULOY is a low beryllium-copper alloy containing about 1.5% nickel. It responds to age-hardening heat treatment for improved mechanical properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on casting, heat treating, machining, and joining. Filing Code: Cu-11. Producer or source: Brush Beryllium Company.

UNS A02960

Alloy Digest ◽  
1987 ◽  
Vol 36 (12) ◽  
Keyword(s):  
Heat Treatment ◽  
Tensile Properties ◽  
Heat Treating ◽  
Age Hardening ◽  
Casting Alloy ◽  
Passenger Cars ◽  
Temperature Performance ◽  
Mold Casting ◽  
Railway Passenger ◽  
Hardening Heat Treatment

Abstract UNS No. A02060 is an aluminum-mold casting alloy that responds to an age-hardening heat treatment. It is recommended for applications that require a combination of high tensile properties and good machinability. Among its many uses are fuel pump bodies, aircraft fittings and seat frames for railway passenger cars. 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 as well as casting, heat treating, machining, and joining. Filing Code: Al-285. Producer or source: Various aluminum companies.

ALUMINUM C355.0

Alloy Digest ◽  
1983 ◽  
Vol 32 (2) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Heat Treating ◽  
Age Hardening ◽  
Casting Alloy ◽  
Permanent Mold ◽  
Good Resistance ◽  
Temperature Performance ◽  
Structural Parts ◽  
Hardening Heat Treatment

Abstract ALUMINUM C355.0 is a high-purity casting alloy that responds to an age-hardening heat treatment. It can be cast successfully by the sand and permanent-mold processes. Its castings characteristics are excellent and it is recommended for pressure-tight castings. It has good resistance to corrosion. Its applications include propeller gear boxes, crankcases and stressed structural parts in aircraft. 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: Al-243. Producer or source: Various aluminum companies.

ALUMINUM 296.0

Alloy Digest ◽  
1982 ◽  
Vol 31 (11) ◽  
Keyword(s):  
Heat Treatment ◽  
Shear Strength ◽  
Tensile Properties ◽  
Heat Treating ◽  
Age Hardening ◽  
Casting Alloy ◽  
Permanent Mold ◽  
Temperature Performance ◽  
Mold Casting ◽  
Hardening Heat Treatment

Abstract ALUMINUM 296.0 is an aluminum permanent-mold casting alloy that responds to an age-hardening heat treatment. It is recommended for applications that require a combination of high tensile properties and good machinability. Among its many uses are fuel pump bodies, aircraft fittings and seat frames for railway passengers cars. 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 as well as casting, heat treating, machining, and joining. Filing Code: Al-241. Producer or source: Various aluminum companies. See also Alloy Digest Al-261, October 1985.

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.

Sign in / Sign up

Export Citation Format

Share Document