ALUMINUM A201

Alloy Digest ◽  
1979 ◽  
Vol 28 (4) ◽  
Keyword(s):  
Impact Resistance ◽  
High Strength ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Military Aircraft ◽  
Temperature Performance ◽  
Ballistic Properties ◽  
Wrought Aluminum Alloys ◽  
Wrought Aluminum

Abstract ALUMINUM A201 offers high strength, high impact resistance, a good combination of room and elevated-temperature performance, and good ballistic properties. Its ballistic properties are comparable to those of the standard wrought aluminum alloys. Among its many application are components for military aircraft and missiles, and impellers for gas turbine engines. This datasheet provides information on composition, physical properties, elasticity, 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Al-234. Producer or source: Consolidated Aluminum Corporation.

PYROMET ALLOY CTX-1

Alloy Digest ◽  
1997 ◽  
Vol 46 (5) ◽  
Keyword(s):  
Coefficient Of Thermal Expansion ◽  
High Strength ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Thermal Fatigue Resistance ◽  
Temperature Performance ◽  
Hot Work Die ◽  
Pressure Hydrogen ◽  
Hot Hardness

Abstract Pyromet CTX-1 is a high-strength, precipitation-hardenable superalloy exhibiting a low coefficient of thermal expansion and high strength up to about 1200 deg F. The alloy possesses high hot hardness and good thermal fatigue resistance. Its applications include components for gas turbine engines, hot-work die applications and high-pressure hydrogen environments. 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 forming, heat treating, machining, and joining. Filing Code: FE-56. Producer or source: Carpenter. Originally published February 1976, revised May 1997.

ALUMINUM 5056

Alloy Digest ◽  
1979 ◽  
Vol 28 (2) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
High Strength ◽  
Heat Treating ◽  
Chromium Alloy ◽  
Temperature Performance ◽  
Wrought Aluminum ◽  
Strength And Ductility ◽  
Cold Workability ◽  
Manganese Chromium

Abstract ALUMINUM 5056 is a non-heat-treatable wrought aluminum-magnesium-manganese-chromium alloy possessing high strength and ductility along with good hot and cold workability. It is recommended for such applications as rivets and screen wire. It may be used with or without cladding. 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-126. Producer or source: Various aluminum companies. Originally published June 1963, revised February 1979.

HAYNES ALLOY 75

Alloy Digest ◽  
1999 ◽  
Vol 48 (7) ◽  
Keyword(s):  
Mechanical Properties ◽  
High Temperature ◽  
Heat Treating ◽  
Turbine Engines ◽  
Chromium Alloy ◽  
Gas Turbine Engines ◽  
Typical Application ◽  
Good Oxidation Resistance ◽  
Temperature Performance ◽  
Haynes Alloy

Abstract Haynes alloy 75 is an 80 nickel-20 chromium alloy with both good oxidation resistance and good mechanical properties at high temperatures. It is amenable to all forms of fabrication and welding. A typical application for sheet metal is fabrications in gas turbine engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: Ni-557. Producer or source: Haynes International Inc.

HAYNES WASPALOY

Alloy Digest ◽  
2000 ◽  
Vol 49 (3) ◽  
Keyword(s):  
Rupture Strength ◽  
Base Alloy ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Temperature Performance ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract Haynes Waspaloy is a specially vacuum melted, nickel-base alloy having outstanding tensile and stress-rupture strength up to 760 deg C (1400 deg F) combined with high oxidation resistance up to 871 deg C (1600 deg F). It is recommended for gas turbine engines, airframe assemblies, and missile systems. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating and machining. Filing Code: Ni-560. Producer or source: Haynes International Inc.

UDIMET WASPALOY

Alloy Digest ◽  
1978 ◽  
Vol 27 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Rupture Strength ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Temperature Performance ◽  
High Oxidation ◽  
High Oxidation Resistance ◽  
Nickel Base

Abstract UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. This datasheet provides information on composition, physical properties, hardness, elasticity, 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, joining, and surface treatment. Filing Code: Ni-257. Producer or source: Special Metals Corporation.

AISI No. 685

Alloy Digest ◽  
1981 ◽  
Vol 30 (9) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Rupture Strength ◽  
Stress Rupture ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Temperature Performance ◽  
Nickel Base ◽  
Corrosion And Oxidation

Abstract AISI No. 685 is a nickel-base, austenitic, precipitation-hardenable alloy. It has excellent tensile and stress-rupture strength to 1400 F and high resistance to corrosion and oxidation at temperatures at least to 1600 F. It is used widely in airframe assemblies, gas turbine engines and missile systems. This datasheet provides information on composition, physical properties, hardness, 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: Ni-271. Producer or source: Nickel alloy mills.

PYROMET CTX-3

Alloy Digest ◽  
1987 ◽  
Vol 36 (7) ◽  
Keyword(s):  
Thermal Expansion ◽  
Corrosion Resistance ◽  
Gas Turbine ◽  
Coefficient Of Thermal Expansion ◽  
High Strength ◽  
Heat Treating ◽  
Turbine Engines ◽  
Gas Turbine Engines ◽  
Good Resistance ◽  
Hot Hardness

Abstract PYROMET CTX-3 is a high-strength precipitation-hardenable low-expansion superalloy. It exhibits a low coefficient of thermal expansion over a broad temperature range combined with high strength. The alloy possesses high hot hardness and good resistance to thermal fatigue. It is brazable, weldable and can be plated with chromium. CTX-3 uses comprise compressor and exhaust casings, seals and other components for gas turbine engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Fe-78. Producer or source: Carpenter.

ALUMINUM 5083

Alloy Digest ◽  
1978 ◽  
Vol 27 (10) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Shear Strength ◽  
Aluminum Alloy ◽  
High Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Storage Tanks ◽  
Temperature Performance ◽  
Aluminum 5083 ◽  
Wrought Aluminum

Abstract ALUMINUM 5083 is a non-heat-treatable wrought aluminum alloy possessing high strength, excellent welding characteristics and excellent resistance to corrosion. Among its many applications are structural towers, mobile cranes and chemical storage tanks. This datasheet provides information on composition, physical properties, 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-33. Producer or source: Various aluminum companies. Originally published October 1955, revised October 1978.

AA 5456

Alloy Digest ◽  
1991 ◽  
Vol 40 (5) ◽  
Keyword(s):  
Shear Strength ◽  
Magnesium Alloy ◽  
Low Temperature ◽  
Physical Properties ◽  
High Strength ◽  
Heat Treating ◽  
Temperature Performance ◽  
Structural Applications ◽  
Wrought Aluminum ◽  
Aluminum Magnesium Alloy

Abstract AA 5456 is a wrought aluminum-magnesium alloy of relatively high strength with good welding characteristics making it suitable for structural applications. (See also Aluminum 5456, Alloy Digest Al-70, September 1958.) This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on low temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-316. Producer or source: Various aluminum companies.

AA 7075

Alloy Digest ◽  
1990 ◽  
Vol 39 (11) ◽  
Keyword(s):  
Compressive Strength ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Aluminum Alloys ◽  
Physical Properties ◽  
Heat Treating ◽  
Temperature Performance ◽  
Aa 7075 ◽  
Wrought Aluminum Alloys ◽  
Wrought Aluminum

Abstract AA 7075 is the outstanding alloy of the 7000 series heat-treatable wrought aluminum alloys. It is used for highly stressed parts. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive strength. 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-309. Producer or source: Various aluminum companies.

Sign in / Sign up

Export Citation Format

Share Document