RMI 6Al-4V

Alloy Digest ◽  
1987 ◽  
Vol 36 (9) ◽  
Keyword(s):  
Room Temperature ◽  
Base Alloy ◽  
Heat Treating ◽  
Pressure Vessels ◽  
Age Hardening ◽  
Bend Strength ◽  
Jet Engines ◽  
Annealed Condition ◽  
Room Temperature Yield Strength ◽  
Alpha Beta

Abstract RMI 6AI-4V is an alpha-beta type of titanium-base alloy that can be strengthened by age hardening. In the mill-annealed condition it has a guaranteed minimum room-temperature yield strength of 120,000 psi and this can be increased to as much as 160,000 psi by solution treating and aging. This alloy is tough and has attractive elevated-temperature properties. It is used widely for applications at temperatures up to 800 F. Typical applications are parts for jet engines, aircraft components and pressure vessels. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength 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, joining, and surface treatment. Filing Code: Ti-88. Producer or source: RMI Company.

RMI 6Al-ELI

Alloy Digest ◽  
1988 ◽  
Vol 37 (12) ◽  
Keyword(s):  
Fracture Toughness ◽  
High Pressure ◽  
Room Temperature ◽  
Base Alloy ◽  
Heat Treating ◽  
Age Hardening ◽  
Bend Strength ◽  
Annealed Condition ◽  
Room Temperature Yield Strength ◽  
Alpha Beta

Abstract RMI 6A1-4V ELI is an alpha-beta type of titanium-base alloy that can be strengthened by age hardening. In the mill-annealed condition it has a guaranteed minimum room-temperature yield strength of 120,000 psi and can be increased to as much as 160,000 psi by solution treating and aging. This alloy may be used for high-pressure cryogenic vessels down to 320 F. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-89. Producer or source: RMI Company.

CRUCIBLE C-120AV

Alloy Digest ◽  
1980 ◽  
Vol 29 (6) ◽  
Keyword(s):  
Base Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Pressure Vessels ◽  
Bend Strength ◽  
Annealed Condition ◽  
Temperature Performance ◽  
Heat Treated ◽  
Forming Characteristics ◽  
Alpha Beta

Abstract CRUCIBLE C-120AV is an alpha-beta type titanium-base alloy with 120,000 psi minimum yield strength in the annealed condition. It has good forming characteristics, is weldable with proper shielding and can be heat treated to high strength levels by solution treating and aging. Its many applications include components for gas-turbine compressors, air-frame forgings, pressure vessels and special ordnance equipment. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear and bend strength as well as fracture toughness, creep, and fatigue. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-77. Producer or source: Crucible Specialty Metals Division, Colt Industries.

RMI 8Mn

Alloy Digest ◽  
1981 ◽  
Vol 30 (4) ◽  
Keyword(s):  
Room Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Temperature Minimum ◽  
Bend Strength ◽  
Beta Titanium Alloy ◽  
Annealed Condition ◽  
Beta Titanium ◽  
Alpha Beta ◽  
Structural Parts

Abstract RMI 8Mn is an alpha-beta titanium alloy that provides a guaranteed room-temperature minimum tensile strength of 120,000 psi in the mill-annealed condition. This alloy offers good formability and excellent resistance to corrosion in applications requiring high strength-to-weight ratios at temperatures up to 700 F. Its uses include aircraft sheet components and structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength. 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-82. Producer or source: RMI Company.

FANSTEEL 85 METAL

Alloy Digest ◽  
1981 ◽  
Vol 30 (6) ◽  
Keyword(s):  
High Temperature ◽  
Physical Properties ◽  
Creep Strength ◽  
Room Temperature ◽  
Elevated Temperatures ◽  
Base Alloy ◽  
Heat Treating ◽  
Good Combination ◽  
Bend Strength ◽  
Temperature Performance

Abstract FANSTEEL 85 METAL is a columbium-base alloy characterized by good fabricability at room temperature, good weldability and a good combination of creep strength and oxidation resistance at elevated temperatures. Its applications include missile and rocket components and many other high-temperature parts. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, tensile properties, and bend strength as well as creep. It also includes information on low and high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cb-7. Producer or source: Fansteel Metallurgical Corporation. Originally published December 1963, revised June 1981.

PYROMET 88

Alloy Digest ◽  
1989 ◽  
Vol 38 (8) ◽  
Keyword(s):  
Base Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Annealed Condition ◽  
Technology Corporation ◽  
Carpenter Technology Corporation ◽  
Nickel Base ◽  
Corrosion And Oxidation ◽  
Effect Of Age

Abstract PYROMET alloy 88 is an age hardenable nickel-base alloy with high strength good corrosion and oxidation resistance. It possesses low creep rate in the temperature range 1200-1500 F (650-820 C). Above 1500 F (820 C), the effect of age hardening is lost and the alloy is used in the annealed condition. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-185. Producer or source: Carpenter Technology Corporation. Originally published February 1973, revised August 1989.

RMI 6Al-6V-2Sn

Alloy Digest ◽  
1980 ◽  
Vol 29 (9) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Rocket Engine ◽  
High Strength ◽  
Heat Treating ◽  
Bend Strength ◽  
Beta Titanium Alloy ◽  
Annealed Condition ◽  
Good Corrosion Resistance ◽  
Beta Titanium ◽  
Alpha Beta

Abstract RMI 6A1-6V-2Sn is an alpha-beta titanium alloy that provides a tensile strength of 150,000 psi in the mill-annealed condition in section sizes up to 2 inches. It offers good corrosion resistance in applications requiring high strength-to-weight ratios at temperatures up to 750 F. Among its uses are rocket engine cases and ordnance components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, 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, joining, and surface treatment. Filing Code: Ti-79. Producer or source: RMI Company.

AISI No. 671

Alloy Digest ◽  
1981 ◽  
Vol 30 (10) ◽  
Keyword(s):  
High Temperature ◽  
Elevated Temperatures ◽  
Base Alloy ◽  
Turbine Blades ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Jet Engines ◽  
Cobalt Base Alloy ◽  
Cobalt Base

Abstract AISI No. 685 is a high-temperature, high-strength, cobalt-base alloy. It responds to an age-hardening heat treatment. At elevated temperatures it has high mechanical properties and excellent resistance to corrosion and oxidation. Its numerous applications include high-temperature hardware, turbine blades, parts for jet engines and aerospace components. 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, and joining. Filing Code: Co-79. Producer or source: High-strength, high-temperature alloy mills & foundries.

RMI 8Al-1Mo-1V

Alloy Digest ◽  
1982 ◽  
Vol 31 (2) ◽  
Keyword(s):  
Tensile Strength ◽  
Creep Resistance ◽  
High Strength ◽  
Heat Treating ◽  
Bend Strength ◽  
Beta Titanium Alloy ◽  
Annealed Condition ◽  
Jet Engine ◽  
Beta Titanium ◽  
Alpha Beta

Abstract RMI 8A1-1Mo-1V is an alpha-beta titanium alloy with a tensile strength of 135,000 psi in the mill-annealed condition. It has an excellent combination of tensile strength and creep resistance that makes it suitable for service to 1000 F. It is recommended for aircraft and jet-engine parts requiring high strength with superior creep resistance and toughness. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: Ti-84. Producer or source: RMI Company.

RMI 5Al-2.5Sn ELI

Alloy Digest ◽  
1980 ◽  
Vol 29 (2) ◽  
Keyword(s):  
Fracture Toughness ◽  
Yield Strength ◽  
Room Temperature ◽  
Heat Treating ◽  
Pressure Vessels ◽  
Cryogenic Temperatures ◽  
Bend Strength ◽  
Temperature Performance ◽  
Alpha Titanium ◽  
Minimum Yield

Abstract RMI 5A1-2.5Sn ELI (ELI = Extra Low Interstitials) is an alpha titanium alloy that was developed for use at cryogenic temperatures. It has a guaranteed minimum yield strength of 100,000 psi at room temperature with good ductility and formability; its yield strength and elongation increase substantially as temperature is lowered. It is used successfully for high-pressure vessels at temperatures below -320 F. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as fracture toughness. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-75. Producer or source: RMI Company.

HAYNES ALLOY No. 25

Alloy Digest ◽  
1961 ◽  
Vol 10 (12) ◽  
Keyword(s):  
High Temperature ◽  
Room Temperature ◽  
Base Alloy ◽  
Heat Treating ◽  
Annealed Condition ◽  
Subsequent Aging ◽  
Temperature Performance ◽  
Cobalt Base Alloy ◽  
Cobalt Base ◽  
Haynes Alloy

Abstract HAYNES# Alloy No. 25 is a wrought, high temperature, cobalt-base alloy that has exceptional mechanical properties at temperatures up to 1800 deg. F. in the fully annealed condition without subsequent aging. It is easy to fabricate because it has excellent ductility at room temperature. 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-5. Producer or source: Haynes Stellite Company. Originally published September 1953, revised December 1961.

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