ALUMINUM 6463

Alloy Digest ◽  
1981 ◽  
Vol 30 (5) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Physical Properties ◽  
Tensile Properties ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Silicon Alloy ◽  
Hardening Heat Treatment

Abstract ALUMINUM 6463 is an aluminum-magnesium-silicon alloy used widely for extrusions. It can be hardened and strengthened by a precipitation-hardening heat treatment. Its many applications comprise extrusions for trim and archtectural use in the automotive, appliance and building industries. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-189. Producer or source: Various aluminum companies. Originally published August 1969, revised May 1981.

AA 6351

Alloy Digest ◽  
1991 ◽  
Vol 40 (9) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Aluminum Alloys ◽  
Physical Properties ◽  
Tensile Properties ◽  
Precipitation Hardening ◽  
Heat Treating

Abstract AA 6351 wrought alloy contains silicon and magnesium in such amounts that Mg2Si is present as the precipitation hardening constituent with proper heat treatment. The 6000 series alloys are less strong than most of the 2000 and 7000 series aluminum alloys. The formability and corrosion resistance of AA 6351 are good. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-319. Producer or source: Various aluminum companies.

BRUSH ALLOY 10

Alloy Digest ◽  
1968 ◽  
Vol 17 (5) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Physical Properties ◽  
Surface Treatment ◽  
Tensile Properties ◽  
Copper Alloy ◽  
Heat Treating ◽  
Age Hardening ◽  
Resistance Welding Electrodes ◽  
Hardening Heat Treatment

Abstract BRUSH Alloy 10 is a low beryllium, cobalt-bearing copper alloy offering an excellent combination of strength, toughness and conductivity due to an age-hardening heat treatment. It is recommended for springs, clutch rings, resistance welding electrodes and tips, etc. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, joining, and surface treatment. Filing Code: Cu-187. Producer or source: Brush Beryllium Company.

REPUBLIC 65

Alloy Digest ◽  
1960 ◽  
Vol 9 (5) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Tensile Properties ◽  
Yield Point ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Low Alloy Steel ◽  
Rolled Condition ◽  
Hardening Heat Treatment ◽  
Minimum Yield

Abstract REPUBLIC-65 is a precipitation hardenable low alloy steel which will meet 65000 psi minimum yield point in the as-rolled condition followed by a precipitation hardening heat treatment. This datasheet provides information on composition, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-98. Producer or source: Republic Steel Corporation.

ALUMINUM 710.0

Alloy Digest ◽  
1983 ◽  
Vol 32 (9) ◽  
Keyword(s):  
Mechanical Properties ◽  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Aluminum Alloy ◽  
Physical Properties ◽  
Tensile Properties ◽  
High Resistance ◽  
Natural Aging ◽  
Heat Treating

Abstract ALUMINUM 710.0 is a natural-aging aluminum alloy produced by sand casting. It develops high mechanical properties without a quenching heat treatment. This alloy has high resistance to shock and excellent resistance to corrosion. Aluminum 710.0 is recommended for highly stressed castings. This datasheet provides information on composition, physical properties, hardness, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-247. Producer or source: Various aluminum companies.

REPUBLIC 70

Alloy Digest ◽  
1960 ◽  
Vol 9 (9) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Tensile Properties ◽  
Yield Point ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Low Alloy Steel ◽  
Rolled Condition ◽  
Hardening Heat Treatment ◽  
Minimum Yield

Abstract REPUBLIC-70 is a precipitation hardenable low alloy steel which will meet 70,000 psi minimum yield point in the as-rolled condition followed by a precipitation hardening heat treatment. This datasheet provides information on composition, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-104. Producer or source: Republic Steel 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.

AA 6066

Alloy Digest ◽  
1990 ◽  
Vol 39 (9) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
Physical Properties ◽  
Tensile Properties ◽  
Precipitation Hardening ◽  
Heat Treating ◽  
Heat Treated

Abstract AA 6066, like other 6XXX aluminum series alloys, contains magnesium and silicon in approximate proportions to form Mg2Si, the constituent responsible for the precipitation hardening capability of the alloy. AA6066 develops intermediate strength levels when heat treated and it possesses good formability and corrosion resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-307. Producer or source: Various aluminum companies.

ALUMINUM 5005

Alloy Digest ◽  
1978 ◽  
Vol 27 (11) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Magnesium Alloy ◽  
Physical Properties ◽  
Tensile Properties ◽  
Cold Working ◽  
Heat Treating ◽  
Aluminum Magnesium Alloy

Abstract ALUMINUM 5005 is nominally an aluminum-magnesium alloy that cannot be hardened or strengthened by heat treatment; however, it can be hardened by cold working. It has excellent resistance to corrosion, excellent weldability and good brazeability. Its numerous applications include appliances, utensils and architectural components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-38. Producer or source: Various aluminum companies. Originally published April 1956, revised April 1973, revised November 1978.

ALUMINUM 7079

Alloy Digest ◽  
1959 ◽  
Vol 8 (10) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Physical Properties ◽  
Tensile Properties ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Aluminum Company ◽  
Strength Alloy ◽  
Hardening Heat Treatment

Abstract ALUMINUM 7079 is a high strength alloy especially applicable to highly stressed aircraft parts in thick sections. It responds to age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-84. Producer or source: Aluminum Company of America.

ALUMINUM 2024

Alloy Digest ◽  
1973 ◽  
Vol 22 (8) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Physical Properties ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract ALUMINUM 2024 is a high-strength wrought alloy that responds readily to an age-hardening heat treatment. It is recommended for applications requiring highly favorable strength-weight ratios. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, and machining. Filing Code: Al-23. Producer or source: Various aluminum companies. Originally published February 1955, revised August 1973.

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