ALUMINUM 3004

Alloy Digest ◽  
1974 ◽  
Vol 23 (4) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Magnesium Alloy ◽  
Cold Working ◽  
Heat Treating ◽  
Temperature Performance ◽  
Good Workability ◽  
Manganese Magnesium

Abstract ALUMINUM 3004 is nominally an aluminum-manganese-magnesium alloy which cannot be hardened by heat treatment; however, it can be strain hardened by cold working. It has higher strength than Aluminum 3003 and good workability, weldability and resistance to corrosion. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-51. Producer or source: Various aluminum companies. Originally published June 1957, revised April 1974.

ALUMINUM 5052

Alloy Digest ◽  
1973 ◽  
Vol 22 (6) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Cold Working ◽  
Salt Water ◽  
Heat Treating ◽  
Chromium Alloy ◽  
High Corrosion Resistance ◽  
Temperature Performance ◽  
Good Workability

Abstract ALUMINUM 5052 is nominally an aluminum-magnesium-chromium alloy which cannot be hardened by heat treatment; however, it can be strain hardened by cold working. It combines good workability with good fatigue strength and high corrosion resistance to the atomsphere and to salt water. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-39. Producer or source: Various aluminum companies. Originally published May 1956, revised June 1971, revised June 1973.

COPPER ALLOY No. 210

Alloy Digest ◽  
1972 ◽  
Vol 21 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Copper Alloy ◽  
Cold Working ◽  
Heat Treating ◽  
Temperature Performance

Abstract COPPER ALLOY No. 210 is a 5% zinc brass having excellent cold working properties. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as 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-255. Producer or source: Brass mills.

MAGNESIUM MSR-B

Alloy Digest ◽  
1967 ◽  
Vol 16 (6) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Magnesium Alloy ◽  
Yield Strength ◽  
Physical Properties ◽  
Heat Treating ◽  
Temperature Performance ◽  
Cast Magnesium Alloy ◽  
Cast Magnesium

Abstract Magnesium MSR-B is a heat-treatable magnesium alloy with highest yield strength of any cast magnesium alloy up to 480 F. It is pressure tight and weldable by argon-arc. It is recommended for aircraft nose wheels, missile components, transmission cases, etc. 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 low and high temperature performance, and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-63. Producer or source: Magnesium Elektron Ltd.

ALUMINUM 5254

Alloy Digest ◽  
1979 ◽  
Vol 28 (9) ◽  
Keyword(s):  
Hydrogen Peroxide ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Physical Properties ◽  
Stress Corrosion Cracking ◽  
Cold Working ◽  
Heat Treating ◽  
General Corrosion ◽  
Temperature Performance

Abstract ALUMINUM 5254 is an aluminum-magnesium-chromium wrought alloy of the non-heat-treatable type; however, it can be hardened and strengthened by cold working. It is relatively strong and has excellent resistance to general corrosion and stress-corrosion cracking. Its applications include hydrogen peroxide serivce and chemical storage vessels. 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, machining, and joining. Filing Code: Al-157. Producer or source: Various aluminum companies. Originally published August 1966, revised September 1979.

ALUMINUM 328.0

Alloy Digest ◽  
1984 ◽  
Vol 33 (10) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Magnesium Alloy ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Good Strength ◽  
Temperature Performance ◽  
Aluminum Silicon

Abstract ALUMINUM 328.0 is an aluminum-silicon-copper-magnesium alloy that responds to heat treatment. It retains good strength up to 400 F. The machinability of this alloy is fair. Its uses include cylinder blocks, crankcases, gear housings and similar components. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, and machining. Filing Code: Al-253. Producer or source: Various aluminum companies.

ALUMINUM 7075

Alloy Digest ◽  
1973 ◽  
Vol 22 (2) ◽  
Keyword(s):  
Mechanical Properties ◽  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
Aluminum Alloy ◽  
High Temperature ◽  
Physical Properties ◽  
Heat Treating ◽  
Temperature Performance ◽  
Aluminum 7075

Abstract ALUMINUM 7075 is a wrought precipitation-hardenable aluminum alloy having excellent mechanical properties, workability and response to heat treatment and refrigeration. (This alloy is covered under its previous designation, ALUMINUM 75S, in Alloy Digest Al-5, February 1953). 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, machining, and joining. Filing Code: Al-179. Producer or source: Various aluminum companies.

UNS A05140

Alloy Digest ◽  
1987 ◽  
Vol 36 (4) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Physical Properties ◽  
Food Processing ◽  
Heat Treating ◽  
Casting Alloy ◽  
Temperature Performance ◽  
Marine Applications

Abstract UNS No. A05140 is a casting alloy that cannot be hardened nor strengthened by heat treatment. It has relatively low strength and hardness. It is characterized by excellent weldability and excellent resistance to corrosion. UNS No. A05140 is recommended for food-processing equipment and marine applications. 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 casting, heat treating, machining, and joining. Filing Code: Al-280. Producer or source: Various aluminum companies.

ALUMINUM 5252

Alloy Digest ◽  
1980 ◽  
Vol 29 (1) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Magnesium Alloy ◽  
Automotive Industry ◽  
High Purity ◽  
Heat Treating ◽  
Temperature Performance ◽  
High Purity Aluminum ◽  
Aluminum Magnesium Alloy

Abstract ALUMINUM 5252 is a high-purity aluminum-magnesium alloy of moderate strength, good fabricating characteristics and excellent resistance to corrosion. It is highly resistant to denting and is used widely as trim in the automotive industry and for a wide variety of other industrial products. This datasheet provides information on composition, physical properties, hardness, elasticity, 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: Al-161. Producer or source: Various aluminum companies. Originally published December 1966, revised January 1980.

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.

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.

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