MAGNESIUM HM31A

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 ◽  
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 ◽  
1959 ◽  
Vol 8 (6) ◽  

Abstract MAGNESIUM HZ 32A is a magnesium-base alloy containing thorium, zirconium and zinc. It is recommended for elevated temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties 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-42. Producer or source: Dow Chemical Company, Magnesium Department.


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 ◽  
1967 ◽  
Vol 16 (4) ◽  

Abstract Magnesium ZK60A is a heat treatable extrusion and forging alloy recommended for applications where high strength with good toughness are required. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, bearing, and bend strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Mg-62. Producer or source: The Dow Chemical 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 ◽  
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 ◽  
1979 ◽  
Vol 28 (5) ◽  

Abstract ALUMINUM 2018 is an age-hardenable aluminum forging alloy characterized by relatively high tensile and yield strengths along with fairly good ductility. It has good elevated-temperature properties. Its applications include engine pistons and engine cylinder heads. 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, machining, and joining. Filing Code: Al-130. Producer or source: Various aluminum companies. Originally published October 1963, revised May 1979.


Alloy Digest ◽  
2006 ◽  
Vol 55 (7) ◽  

Abstract Alloy 2124 is a heat treatable plate alloy that was developed for elevated-temperature application. Copper is the main alloying addition. 2124-T851 plate is an improvement in fracture toughness compared to 2024-T851. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, 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: AL-399. Producer or source: Alcoa Mill Products.


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..


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