DOWMETAL O1

Alloy Digest ◽  
1954 ◽  
Vol 3 (2) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Fatigue Strength ◽  
Magnesium Alloy ◽  
Bearing Strength ◽  
Chemical Company ◽  
Temperature Performance ◽  
High Fatigue ◽  
Good Creep Resistance

Abstract DOWMETAL O1 is a heat treatable magnesium alloy for forgings and extrusions requiring high fatigue strength and good creep resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, machining, joining, and surface treatment. Filing Code: Mg-8. Producer or source: The Dow Chemical Company.

MAGNESIUM AZ80A

Alloy Digest ◽  
1964 ◽  
Vol 13 (1) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Fatigue Strength ◽  
Magnesium Alloy ◽  
Heat Treating ◽  
Bearing Strength ◽  
Temperature Performance ◽  
High Fatigue ◽  
Metal Products ◽  
Good Creep Resistance

Abstract Magnesium AZ80A is a heat treatable, magnesium alloy recommended for forgings and extrusions requiring high fatigue strength and good creep resistance. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, joining, and surface treatment. Filing Code: Mg-55. Producer or source: The Dow Metal Products Company.

MAGNESIUM ZK60A

Alloy Digest ◽  
1967 ◽  
Vol 16 (4) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
High Strength ◽  
Heat Treating ◽  
Bend Strength ◽  
Chemical Company ◽  
Temperature Performance

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.

MAGNESIUM AZ61A

Alloy Digest ◽  
1959 ◽  
Vol 8 (8) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Tensile Properties ◽  
Heat Treating ◽  
Bearing Strength ◽  
Chemical Company ◽  
Temperature Performance ◽  
Extrusion Alloy

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.

CRUCIBLE P/M 625

Alloy Digest ◽  
1993 ◽  
Vol 42 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Fatigue Strength ◽  
Stress Corrosion ◽  
Stress Corrosion Cracking ◽  
Chloride Ions ◽  
Corrosion Cracking ◽  
Cryogenic Temperatures ◽  
Temperature Performance

Abstract P/M 625 is a nonmagnetic alloy with outstanding strength and toughness from cryogenic temperatures to 2000 F. It has excellent fatigue strength and stress-corrosion-cracking resistance to chloride ions. This datasheet provides information on composition, microstructureand elasticity as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance. Filing Code: Ni-441. Producer or source: Crucible Compaction Metals.

REM-CRU A-70

Alloy Digest ◽  
1958 ◽  
Vol 7 (5) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Tensile Properties ◽  
Heat Treating ◽  
Bearing Strength ◽  
Temperature Performance

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..

MAGNESIUM HM31A

Alloy Digest ◽  
1966 ◽  
Vol 15 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Elevated Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Space Vehicles ◽  
Bearing Strength ◽  
Chemical Company ◽  
Temperature Performance

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.

MAGNESIUM ZH62A

Alloy Digest ◽  
1959 ◽  
Vol 8 (2) ◽  
Keyword(s):  
Fracture Toughness ◽  
Compressive Strength ◽  
Corrosion Resistance ◽  
High Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Fatigue Properties ◽  
Casting Alloy ◽  
Chemical Company ◽  
Temperature Performance

Abstract Magnesium ZH62A is a high strength casting alloy having acceptable castability and weldability. It has good fatigue properties and ductility. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-40. Producer or source: Dow Chemical Company, Magnesium Products Department.

CRUCIBLE A-70

Alloy Digest ◽  
1971 ◽  
Vol 20 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Pure Titanium ◽  
Heat Treating ◽  
Commercially Pure Titanium ◽  
Bearing Strength ◽  
Temperature Performance ◽  
Commercially Pure ◽  
Specialty Metals

Abstract CRUCIBLE A-70 is a grade of commercially pure titanium that is used where higher strength is required than is achieved with grade A-55. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness, creep, and fatigue. 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-63. Producer or source: Crucible Specialty Metals Division, Colt Industries.

SANDVIK 11R51

Alloy Digest ◽  
1966 ◽  
Vol 15 (2) ◽  
Keyword(s):  
Fracture Toughness ◽  
Stainless Steel ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Temperature Performance ◽  
High Fatigue ◽  
High Torque ◽  
Torque Values

Abstract SANDVIK 11R51 is a stainless steel having high fatigue and tensile strengths. It is recommended for springs requiring corrosion resistance and high torque values. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on low and high temperature performance as well as forming. Filing Code: SS-177. Producer or source: Sandvik.

CRUCIBLE A-55

Alloy Digest ◽  
1971 ◽  
Vol 20 (7) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Heat Treating ◽  
General Purpose ◽  
Bearing Strength ◽  
Temperature Performance ◽  
Specialty Metals

Abstract CRUCIBLE A-55 is the general purpose grade of titanium for applications requiring moderate to severe forming. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength 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, joining, and surface treatment. Filing Code: Ti-62. Producer or source: Crucible Specialty Metals Division, Colt Industries.

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