NORAL 38S

Alloy Digest ◽  
1958 ◽  
Vol 7 (8) ◽  

Abstract Noral 38S is a high-silicon aluminum having comparatively low coefficient of expansion and good forgeability. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-68. Producer or source: Northern Aluminium Company Ltd.

Alloy Digest ◽  
1971 ◽  
Vol 20 (6) ◽  

Abstract MUELLER ALLOY No. 6741 (formerly 600 Alloy) is a high-strength bearing alloy intended for use in applications requiring a combination of outstanding wear characteristics and high bearing strength. 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, and joining. Filing Code: Cu-235. Producer or source: Mueller Brass Company.


Alloy Digest ◽  
1960 ◽  
Vol 9 (8) ◽  

Abstract MAGNESIUM AZ91C is a general sand casting alloy having good strength, pressure tightness and ductility. It was designed to give optimum properties in both the T4 and T6 tempers. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and and bearing strength It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-47. Producer or source: The Dow Metal Products Company.


Alloy Digest ◽  
1959 ◽  
Vol 8 (8) ◽  

Abstract MAGNESIUM AZ61A is a magnesium extrusion alloy having a strength level between that of AZ31B and ZK60A. 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-43. Producer or source: The Dow Chemical Company.


Alloy Digest ◽  
1999 ◽  
Vol 48 (7) ◽  

Abstract URANUS S1 is the development of 15 years research into alloys containing high silicon contents (4% here) to resist the transpassive intergranular corrosion from such chemicals as concentrated nitric acid. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-751. Producer or source: Cruesot-Marrel.


Alloy Digest ◽  
1970 ◽  
Vol 19 (5) ◽  

Abstract NICKEL 233 is used primarily for plates (anodes) in vacuum tubes. It is also suitable for structural parts of tubes other than cathodes and it exhibits good magnetostriction properties. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and and bearing strength It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-154. Producer or source: Huntington Alloy Products Division.


Alloy Digest ◽  
1966 ◽  
Vol 15 (11) ◽  

Abstract MONEL Alloy K-500 combines the excellent corrosion resistance characteristics of the MONEL nickel-copper alloys with the added advantages of greaterr strength and hardness. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties and bearing strength as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-119. Producer or source: Huntington Alloy Products Division.


Alloy Digest ◽  
1958 ◽  
Vol 7 (5) ◽  

Abstract REM-CRU A-70 is the grade of unalloyed titanium used where higher strength is required. It is specified for many moderately stressed aircraft parts. (Formerly known as RC-70.) This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-16. Producer or source: Rem-Cru Titanium Inc..


Alloy Digest ◽  
1957 ◽  
Vol 6 (3) ◽  

Abstract MAGNESIUM AZ63A is a structural light weight alloy particularly suitable for intricate parts. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, joining, and surface treatment. Filing Code: Mg-32. Producer or source: Magnesium foundries.


Alloy Digest ◽  
1966 ◽  
Vol 15 (5) ◽  

Abstract Magnesium HM331A is a magnesium-thorium alloy recommended for elevated temperature service (600-850 F) in aircraft, missiles, and space vehicles. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Mg-59. Producer or source: Dow Chemical Company.


Alloy Digest ◽  
1958 ◽  
Vol 7 (7) ◽  

Abstract Magnesium HK31 is a magnesium-base alloy possessing extraordinary resistance to creep and maintaining excellent strength through the temperature range of 300-700 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on low and high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Mg-39. Producer or source: Brooks & Perkins Inc..


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