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.

COOPER ALLOY 14S

Alloy Digest ◽  
1964 ◽  
Vol 13 (7) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Corrosion Resistant ◽  
Temperature Performance ◽  
Corrosion Resistant Alloy

Abstract Cooper Alloy 14S is an abrasion, heat and corrosion resistant alloy steel containing 12% chromium. It can be hardened by heat treatment. It is recommended for pumps and valves in the cast form. 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, and joining. Filing Code: SS-158. Producer or source: Cooper Alloy Corporation.

ALLEGHENY D-979

Alloy Digest ◽  
1960 ◽  
Vol 9 (10) ◽  
Keyword(s):  
Heat Treatment ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Tensile Properties ◽  
Gas Turbine ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract Allegheny D-979 is an austenitic, high-temperature superalloy for aircraft gas turbine applications. It responds to a precipitation hardening 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 as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-61. Producer or source: Allegheny Ludlum Corporation.

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.

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.

FIRTH VICKERS F.I. (A1)

Alloy Digest ◽  
1970 ◽  
Vol 19 (4) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Stainless Steels ◽  
Heat Treating ◽  
Oil Refining ◽  
Corrosion Resistant ◽  
Temperature Performance ◽  
Plant Equipment ◽  
Corrosion Resistant Alloy

Abstract FIRTH VICKERS FI (A1) is a chromium type heat and corrosion resistant alloy steel recommended for oil refining and chemical plant equipment. 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, joining, and surface treatment. Filing Code: SS-236. Producer or source: Firth-Vickers Stainless Steels Ltd.

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..

CARPENTER 825 PLUS

Alloy Digest ◽  
2006 ◽  
Vol 55 (3) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Heat Treating ◽  
Gas Well ◽  
Corrosion Resistant ◽  
Temperature Performance ◽  
Technology Corporation ◽  
Corrosion Resistant Alloy ◽  
Carpenter Technology Corporation

Abstract Carpenter 825 Plus is a corrosion-resistant alloy often used in downhole or surface gas well components. The alloy is age hardenable. 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, and joining. Filing Code: Ni-632. Producer or source: Carpenter Technology Corporation.

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.

FIRTH VICKERS F.V. 520(S)

Alloy Digest ◽  
1968 ◽  
Vol 17 (4) ◽  
Keyword(s):  
Heat Treatment ◽  
High Temperature ◽  
Stainless Steels ◽  
Martensitic Steel ◽  
Heat Treating ◽  
Corrosion Resistant ◽  
Supersonic Aircraft ◽  
Temperature Performance ◽  
Temperature Heat ◽  
Temperature Heat Treatment

Abstract Fifth-Vickers F.V. 520(S) is a corrosion resistant martensitic steel which is readily weldable and capable of being hardened by low temperature heat treatment. It is recommended for turbine components and supersonic aircraft parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: SS-208. Producer or source: Firth-Vickers Stainless Steels Ltd.

CHROMIUM COPPER-999

Alloy Digest ◽  
1953 ◽  
Vol 2 (8) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Low Temperature ◽  
Physical Properties ◽  
Heat Treating ◽  
High Temperature Solution ◽  
Temperature Solution ◽  
Precipitation Heat

Abstract Chromium Copper-999 is a copper-chromium-silicon alloy which is softened by a high-temperature solution anneal and quench, and will acquire improved properties with a low-temperature precipitation 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 corrosion resistance as well as heat treating, machining, and joining. Filing Code: Cu-10. Producer or source: American Brass Company.

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