LOCKALLOY

Alloy Digest ◽  
1971 ◽  
Vol 20 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Aluminum Alloy ◽  
Heat Treating ◽  
Design Criteria ◽  
Low Density ◽  
High Modulus ◽  
Bearing Strength ◽  
Temperature Performance ◽  
Structural Applications

Abstract LOCKALLOY is a beryllium-aluminum alloy that was developed for aerospace structural applications where high modulus and low density are design criteria. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and 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: Be-1. Producer or source: Kawecki Berylco Industries Inc..

ALCAN 65S

Alloy Digest ◽  
1958 ◽  
Vol 7 (4) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
Aluminum Alloy ◽  
High Temperature ◽  
Heat Treating ◽  
Good Corrosion Resistance ◽  
Temperature Performance ◽  
Aluminum Company ◽  
Structural Applications ◽  
Wrought Aluminum

Abstract ALCAN 65S is a wrought aluminum alloy having good forming qualities. It is recommended for structural applications where good corrosion resistance is important. 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-65. Producer or source: Aluminum Company of Canada Ltd.

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..

SUPER-Z

Alloy Digest ◽  
1978 ◽  
Vol 27 (10) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Aluminum Alloy ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Creep Resistance ◽  
Heat Treating ◽  
Zinc Alloys ◽  
Temperature Performance

Abstract SUPER-Z is a superplastic zinc-aluminum alloy basically of the eutectoid composition of 78% zinc-22% aluminum with various minor additives to improve its properties, such as strength and creep resistance. Four grades of superplastic zinc alloys are available: SUPER-Z 100, SUPER-Z 200, SUPER-Z 300 and SUPER-Z 400. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties 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: Zn-34. Producer or source: The New Jersey Zinc Company.

NORAL B54S

Alloy Digest ◽  
1960 ◽  
Vol 9 (4) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Aluminum Alloy ◽  
Physical Properties ◽  
Tensile Properties ◽  
High Strength ◽  
Heat Treating ◽  
Bearing Strength ◽  
Excellent Corrosion Resistance

Abstract NORAL B54S is a non-heat treatable aluminum alloy characterized by high strength, excellent corrosion resistance especially in marine atmospheres, and excellent welding characteristics. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: Al-90. Producer or source: Northern Aluminium Company Ltd.

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.

WC-Ta-10W

Alloy Digest ◽  
1970 ◽  
Vol 19 (12) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Low Temperature ◽  
Physical Properties ◽  
Elevated Temperatures ◽  
Base Alloy ◽  
Heat Treating ◽  
Temperature Performance ◽  
Structural Applications

Abstract WC Ta-10W is a tantalum-base alloy having a combination of low-temperature ductility and fabricability in both the recrystalilzed and wrought conditions, as well as excellent weld ductility. Developed originally for structural applications at elevated temperatures, it is now available in a complete line of aerospace hardware. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ta-1. Producer or source: Teledyne Wah Chang Albany.

ALUMINUM 7039

Alloy Digest ◽  
1966 ◽  
Vol 15 (4) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Low Temperature ◽  
Physical Properties ◽  
High Strength ◽  
Heat Treating ◽  
Bearing Strength ◽  
Good Corrosion Resistance ◽  
Temperature Performance ◽  
Chemical Corporation

Abstract Aluminum 7039 is a wrought, heat treatable alloy having good weldability and good corrosion resistance combined with high strength. It is recommended for cryogenic applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-154. Producer or source: Kaiser Aluminum & Chemical Corporation.

NORAL 19S

Alloy Digest ◽  
1962 ◽  
Vol 11 (10) ◽  
Keyword(s):  
Fracture Toughness ◽  
Aluminum Alloy ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Elevated Temperatures ◽  
Heat Treating ◽  
Bearing Strength ◽  
Temperature Performance ◽  
Wrought Aluminum

Abstract NORAL 19S is an age-hardenable, wrought aluminum alloy that retains its strength well at elevated temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-119. Producer or source: Alcan Industries Ltd.

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.

BETHLEHEM RQ-100A

Alloy Digest ◽  
1972 ◽  
Vol 21 (3) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Strength ◽  
Heat Treating ◽  
Pressure Vessels ◽  
Bethlehem Steel Corporation ◽  
Temperature Performance ◽  
Heat Treated ◽  
Structural Applications

Abstract BETHLEHEM RQ-100A is a heat-treated alloy steel having 100,000 psi yield strength through 11/4-in. thickness, in combination with good toughness, abrasion resistance and weldability. It is engineered specifically for structural applications such as earth moving equipment,buildings, bridges, and pressure vessels where high strength is required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness and 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: SA-272. Producer or source: Bethlehem Steel Corporation. See also Alloy Digest SA-221, January 1968.

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