ALUMINUM 5456

Alloy Digest ◽  
1958 ◽  
Vol 7 (9) ◽  

Abstract Aluminum 5456 is an aluminum-magnesium alloy suitable for structural welding applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: Al-70. Producer or source: Aluminum Company of America.

Alloy Digest ◽  
1960 ◽  
Vol 9 (1) ◽  

Abstract MAGNESIUM ALLOY-TA54A is a general purpose hammer-forging alloy having intermediate strength. 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 corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-44. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1992 ◽  
Vol 41 (3) ◽  

Abstract AA 5052 is a non heat treatable aluminum/magnesium alloy of moderate strength and good weldability. 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-322. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1978 ◽  
Vol 27 (11) ◽  

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.


Alloy Digest ◽  
1991 ◽  
Vol 40 (6) ◽  

Abstract AA 5657 is a binary aluminum/magnesium alloy of moderate strength. It is not hardenable by heat treatment. It is strain hardenable. 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-317. Producer or source: Various aluminum companies.


Alloy Digest ◽  
1966 ◽  
Vol 15 (3) ◽  

Abstract Aluminum 212 is a copper, silicon, aluminum-base sand casting alloy having good machinability and good castability. It is recommended for general machinery and utility castings. 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 corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-153. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1962 ◽  
Vol 11 (2) ◽  

Abstract Aluminum 384 is a silicon-copper type of aluminum die casting alloy having excellent castability and improved machinability. 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 and corrosion resistance as well as casting, heat treating, and machining. Filing Code: Al-111. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1971 ◽  
Vol 20 (5) ◽  

Abstract ALUMINUM 242.0 is an age-hardenable casting alloy that has excellent strength at elevated temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as creep and 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: Al-202. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1965 ◽  
Vol 14 (11) ◽  

Abstract Alcan 143 is a copper-silicon type aluminum die casting alloy having excellent fluidity, castability and improved machinability. It is recommended for pressure-tight castings. 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 and corrosion resistance as well as casting, heat treating, and machining. Filing Code: Al-149. Producer or source: Aluminum Company of Canada Ltd.


Alloy Digest ◽  
1955 ◽  
Vol 4 (4) ◽  

Abstract ALUMINUM 4032, formerly known as Aluminium 32S, is a forging alloy having comparatively low coefficient of expansion and good forgeability. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as creep and fatigue. It also includes information on low and high temperature performance as well as heat treating, machining, and joining. Filing Code: Al-25. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1966 ◽  
Vol 15 (10) ◽  

Abstract Aluminum 7002 is a heat treatable, weldable, high strength aluminum alloy recommended for space equipment and cryogenic 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 low temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-159. Producer or source: Aluminum Company of America.


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