CONFLEX 720

Alloy Digest ◽  
1964 ◽  
Vol 13 (7) ◽  

Abstract CONFLEX 720 is a copper-manganese-nickel alloy that responds to an age-hardening heat treatment for high strength and corrosion resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: Cu-143. Producer or source: Metals & Controls Inc..

Alloy Digest ◽  
1956 ◽  
Vol 5 (9) ◽  

Abstract BERYLCO CR-1 is a high strength, corrosion resistant beryllium-nickel alloy which responds readily to an age-hardening heat treatment. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as casting, heat treating, machining, joining, and surface treatment. Filing Code: Ni-27. Producer or source: Beryllium Corporation.


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 ◽  
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 ◽  
1973 ◽  
Vol 22 (8) ◽  

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.


Alloy Digest ◽  
1969 ◽  
Vol 18 (10) ◽  

Abstract ACCURATE METAL is a copper-nickel alloy having high strength, ductility and corrosion resistance. It was especially designed for exacting electronic and electrical applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, joining, and surface treatment. Filing Code: Cu-207. Producer or source: Connecticut Metals Corporation.


Alloy Digest ◽  
1969 ◽  
Vol 18 (11) ◽  

Abstract Aluminum A356 is a sand and permanent mold casting alloy that responds to an age-hardening heat treatment. It is recommended for aircraft and missile components where high strength and corrosion resistance are required. 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 heat treating, machining, and joining. Filing Code: Al-192. Producer or source: Aluminum Company of America.


Alloy Digest ◽  
1954 ◽  
Vol 3 (1) ◽  

Abstract C.D.C. MANGANESE ALLOY No. 720 is a copper-manganese-nickel alloy that responds to hardening by heat treatment. It has high tensile and fatigue strength, wide hardness range, and excellent corrosion resisting characteristics. 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: Cu-14. Producer or source: Chicago Development Corporation.


Alloy Digest ◽  
1965 ◽  
Vol 14 (2) ◽  

Abstract CHASE PHOSNIC BRONZE is a high copper alloy combining high strength and high conductivity, both electrical and thermal, in an unusual degree. It has high workability and excellent corrosion resistance. The additions of nickel and phosphorus to the copper render the alloy capable of being hardened and strengthened by age-hardening heat treatment. The alloy has also high endurance strength in the harder drawn tempers of wire, and excellent resistance to creep or flow under the influence of prolonged stress. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cu-12. Producer or source: Chase Brass & Copper Company Inc.. Originally published November 1953, revised February 1965.


Alloy Digest ◽  
1964 ◽  
Vol 13 (4) ◽  

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..


Alloy Digest ◽  
1956 ◽  
Vol 5 (3) ◽  

Abstract DURANICKEL R is an age-hardenable nickel alloy having high strength and high corrosion resistance. It is magnetic at room temperature in all conditions. It is recommended for improved machinability over standard Duranickel. 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, joining, and surface treatment. Filing Code: Ni-24. Producer or source: The International Nickel Company Inc..


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