ALLCAST 41A

Alloy Digest ◽  
1968 ◽  
Vol 17 (5) ◽  

Abstract ALLCAST 41A is an aluminum-silicon-copper casting alloy. It responds to an age-hardening heat treatment and is recommended for light weight, high strength, pressure-tight 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 high temperature performance as well as heat treating, machining, and joining. Filing Code: Al-175. Producer or source: Apex Smelting Company.

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 ◽  
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.


Alloy Digest ◽  
1958 ◽  
Vol 7 (7) ◽  

Abstract ALUMINUM 6151, formerly A51S Alloy, is an aluminum forging alloy combining good forgeability, strength, and resistance to corrosion. It responds to an age-hardening heat treatment. 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 as well as forming, heat treating, machining, and joining. Filing Code: Al-67. Producer or source: Aluminum Company of America.


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 (11) ◽  

Abstract ECLIPSALOY 517 is a cerium-magnesium sand casting alloy having excellent creep resistance up to 500 deg. F. It is suitable for applications where pressure tightness is required and good corrosion resistance is important. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-29. Producer or source: Bendix Aviation Corporation.


Alloy Digest ◽  
1960 ◽  
Vol 9 (2) ◽  

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.


Alloy Digest ◽  
1958 ◽  
Vol 7 (2) ◽  

Abstract ARMCO 17-10P is an austenitic stainless steel that responds favorably to an age-hardening heat treatment. It is recommended for use in applications requiring high strength with low magnetic permeability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-69. Producer or source: Armco Inc., Eastern Steel Division.


Alloy Digest ◽  
1960 ◽  
Vol 9 (6) ◽  

Abstract INCONEL W is a high strength, high temperature nickel-base alloy responding to an age-hardening heat treatment for maximum properties. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-58. Producer or source: Huntington Alloy Products Division, An INCO Company.


Alloy Digest ◽  
1966 ◽  
Vol 15 (7) ◽  

Abstract Brush Alloy M220C is a betyllium-nickel casting alloy that responds to an age-hardening heat treatment and is characterized by high strength thermal conductivity combined with excellent corrosion, oxidation and wear resistance. It is recommended for mold tooling in the glass industries. 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Ni-114. Producer or source: Brush Beryllium Company.


Alloy Digest ◽  
1961 ◽  
Vol 10 (5) ◽  

Abstract COOPER PH-55B is a high-strength high-ductility alloy recommended for corrosion resistance of parts subjected to a combination of stress and shock. It responds 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 high temperature performance and corrosion resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: SS-117. Producer or source: Cooper Alloy Corporation.


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