DOWMETAL FS and FS-1

Alloy Digest ◽  
1953 ◽  
Vol 2 (9) ◽  

Abstract DOWMETAL FS and FS-1 are wrought magesium-base alloys that do not respond to age-hardening heat treatment for increased hardness and strength. They are general purpose extrusion alloys. DOWMETAL FS-1 is the controlled purity grade. Extrusions are supplied in both FS and FS-1. Sheet and plate are supplied in FS-1 only. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength. It also includes information on as well as forming, machining, and joining. Filing Code: Mg-7. Producer or source: The Dow Chemical Company.

Alloy Digest ◽  
1953 ◽  
Vol 2 (2) ◽  

Abstract DOWMETAL M is a manganese type magnesium base alloy which does not respond to hardening heat treatment, but is recommended where maximum formability and weldability are desired. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: Mg-3. Producer or source: The Dow Chemical Company.


Alloy Digest ◽  
1959 ◽  
Vol 8 (4) ◽  

Abstract NORAL 62S is an aluminum extrusion alloy that responds to an age hardening heat treatment. It has good strength and excellent fabricating characteristics. This datasheet provides information on composition, physical properties, hardness, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on as well as forming, heat treating, machining, and joining. Filing Code: Al-77. Producer or source: Northern Aluminium Company Ltd.


Alloy Digest ◽  
1953 ◽  
Vol 2 (10) ◽  

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.


Alloy Digest ◽  
1957 ◽  
Vol 6 (1) ◽  

Abstract WHITE LIGHT-MF is a wrought magnesium-base alloy that does not respond to age-hardening heat treatment for increased hardness and strength. It is a general purpose extrusion alloy for applications where medium strength and economy are prime factors. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Mg-30. Producer or source: Whitelight Magnesium Division.


Alloy Digest ◽  
1968 ◽  
Vol 17 (5) ◽  

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.


Alloy Digest ◽  
1970 ◽  
Vol 19 (3) ◽  

Abstract DOMAL AZ21X is a readily extrudable magnesium alloy used where moderate strength requirements will suffice. It does not respond to an age-hardening heat treatment. It is recommended for structural members, truck bodies and paneling. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Mg-68. Producer or source: Dominion Magnesium Ltd.


Alloy Digest ◽  
1961 ◽  
Vol 10 (2) ◽  

Abstract MAGNESIUM-AM100A has a good combination of strength and ductility. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on corrosion resistance as well as casting, heat treating, machining, and surface treatment. Filing Code: Mg-49. Producer or source: The Dow Metal Products Company.


Alloy Digest ◽  
1959 ◽  
Vol 8 (10) ◽  

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.


Alloy Digest ◽  
1987 ◽  
Vol 36 (12) ◽  

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.


Alloy Digest ◽  
1982 ◽  
Vol 31 (11) ◽  

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.


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