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Journal Articles
Alloy Digest (1978) 27 (8): Al-95.
Published: 01 August 1978
... ALUMINUM 2218 is an aluminum-copper-nickel-magnesium alloy (formerly designated B18S Alloy). It is a standard forging alloy and is recommended for elevated-temperature service. It is used for aircraft and jet engine components. This datasheet provides information on composition, physical...
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ALUMINUM 2218 is an aluminum-copper-nickel-magnesium alloy (formerly designated B18S Alloy). It is a standard forging alloy and is recommended for elevated-temperature service. It is used for aircraft and jet engine components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-95. Producer or source: Various aluminum companies. Originally published September 1960, revised August 1978.
Journal Articles
Alloy Digest (1980) 29 (7): Ti-78.
Published: 01 July 1980
...) of 80,000 psi at 1000 F. Its uses include elevated-temperature service and jet-engine components. 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 corrosion...
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RMI 5A1-5Sn-2Zr-2Mo-Si is an alpha-type titanium alloy recommended for high-temperature applications in the 800-1000 F range. In the mill annealed condition it has a typical room-temperature yield strength of 126,000 psi and a typical yield strength (in short-time elevated-temperature tensile test) of 80,000 psi at 1000 F. Its uses include elevated-temperature service and jet-engine components. 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 corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-78. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1981) 30 (4): Ni-267.
Published: 01 April 1981
... in sheet form; consequently, it is used widely for jet engine components. Other uses include turbine buckets, turbine wheels, rings and high-temperature fasteners and springs. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
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UNITEMP 41 is a nickel-base, precipitation-hardenable alloy that retains high strength and finds most use in the temperature range 1200 to 1800 F. It is produced by one or more vacuum melting practices. This alloy is one of the strongest high-temperature alloys that can be formed and welded in sheet form; consequently, it is used widely for jet engine components. Other uses include turbine buckets, turbine wheels, rings and high-temperature fasteners and springs. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. 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-267. Producer or source: Cyclops Corporation.
Journal Articles
Alloy Digest (1998) 47 (6): SS-719.
Published: 01 June 1998
... Allegheny Ludlum Type 310 is an austenitic chromium-nickel steel with high heat resisting properties. It is recommended for furnace equipment, heat treating boxes, burners, heat recovery systems, jet engine components, and heat exchangers. This datasheet provides information on composition...
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Allegheny Ludlum Type 310 is an austenitic chromium-nickel steel with high heat resisting properties. It is recommended for furnace equipment, heat treating boxes, burners, heat recovery systems, jet engine components, and heat exchangers. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness, creep, and fatigue. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: SS-719. Producer or source: Allegheny Ludlum Corporation.
Journal Articles
Alloy Digest (1970) 19 (1): Co-60.
Published: 01 January 1970
... CML-605 is a cobalt-base alloy having high strength, heat and oxidation resistance at elevated temperatures above 1600 F. It is recommended for gas turbine and jet engine components operating in the 1600 to 2000 F temperature range. This datasheet provides information on composition, physical...
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CML-605 is a cobalt-base alloy having high strength, heat and oxidation resistance at elevated temperatures above 1600 F. It is recommended for gas turbine and jet engine components operating in the 1600 to 2000 F temperature range. 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, machining, and joining. Filing Code: Co-60. Producer or source: Cannon-Muskegon Corporation.
Journal Articles
Alloy Digest (1970) 19 (3): SA-250.
Published: 01 March 1970
... REPUBLIC RSM 250 is an 18% nickel-cobalt-molybdenum age-hardening steel designed to develop 250,000 psi yield strength with good toughness. It is recommended where a combination of strength, toughness and notch resistance is required such as aircraft landing gears and jet engine components...
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REPUBLIC RSM 250 is an 18% nickel-cobalt-molybdenum age-hardening steel designed to develop 250,000 psi yield strength with good toughness. It is recommended where a combination of strength, toughness and notch resistance is required such as aircraft landing gears and jet engine components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive 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: SA-250. Producer or source: Republic Steel Corporation, Titanium Division.
Journal Articles
Alloy Digest (1965) 14 (10): SS-173.
Published: 01 October 1965
... for turbine and jet engine components. 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...
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AISI Type 422 is a hardenable 12% chromium stainless steel recommended for applications requiring superior strength to Type 403 stainless steel at elevated temperatures. It retains high strength and exhibits excellent ductility over the temperature range from room to 1200 F. It is recommended for turbine and jet engine components. 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, joining, and surface treatment. Filing Code: SS-173. Producer or source: Stainless steel mills.
Journal Articles
Alloy Digest (1967) 16 (2): Ni-121.
Published: 01 February 1967
... INCONEL alloy 625 is a nickel-base alloy having excellent stress-rupture properties and good oxidation resistance to 1200 F. It is recommended for jet engine components, aerospace applications and chemical processing equipment. This datasheet provides information on composition, physical...
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INCONEL alloy 625 is a nickel-base alloy having excellent stress-rupture properties and good oxidation resistance to 1200 F. It is recommended for jet engine components, aerospace applications and chemical processing equipment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties 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: Ni-121. Producer or source: Huntington Alloy Products Division, An INCO Company.
Journal Articles
Alloy Digest (1967) 16 (7): SS-196.
Published: 01 July 1967
... Allegheny Ludlum 419 is a ferritic (martensitic) type chromium-tungsten alloy recommended for high temperature applications in the temperature range of 800-1200 F, such as turbine and jet engine components. This datasheet provides information on composition, physical properties, elasticity...
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Allegheny Ludlum 419 is a ferritic (martensitic) type chromium-tungsten alloy recommended for high temperature applications in the temperature range of 800-1200 F, such as turbine and jet engine components. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive 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: SS-196. Producer or source: Allegheny Ludlum Corporation.
Journal Articles
Alloy Digest (1967) 16 (7): SS-197.
Published: 01 July 1967
... AISI TYPE 310 is an austenitic chromium-nickel steel with high heat resisting properties. It is recommended for furnace equipment, heat treating boxes, jet engine components and heat exchangers. This datasheet provides information on composition, physical properties, hardness, elasticity...
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AISI TYPE 310 is an austenitic chromium-nickel steel with high heat resisting properties. It is recommended for furnace equipment, heat treating boxes, jet engine components and heat exchangers. 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, joining, and surface treatment. Filing Code: SS-197. Producer or source: Stainless steel mills.
Journal Articles
Alloy Digest (1967) 16 (9): SS-200.
Published: 01 September 1967
... AISI No. 616 is a hardenable martensitic type stainless steel recommended for high temperature applications up to 1200 F. It is used for steam turbine blades and buckets, valves, jet engine components, and high temperature bolting. This datasheet provides information on composition, physical...
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AISI No. 616 is a hardenable martensitic type stainless steel recommended for high temperature applications up to 1200 F. It is used for steam turbine blades and buckets, valves, jet engine components, and high temperature bolting. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive 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: SS-200. Producer or source: Alloy steel mills and foundries.
Journal Articles
Alloy Digest (1968) 17 (2): Ni-131.
Published: 01 February 1968
... GMR-235 Alloy is a nickel-base, precipitation-hardening alloy available in investment cast form for high temperature service. It is recommended for gas turbine and jet engine components operating in excess of 1400 F. This datasheet provides information on composition, physical properties, hardness...
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GMR-235 Alloy is a nickel-base, precipitation-hardening alloy available in investment cast form for high temperature service. It is recommended for gas turbine and jet engine components operating in excess of 1400 F. 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, joining, and surface treatment. Filing Code: Ni-131. Producer or source: Licensees of the General Motors Corporation.
Journal Articles
Alloy Digest (1962) 11 (1): Ti-32.
Published: 01 January 1962
... Ti-8A1-1Mo-1V is a titanium alloy having excellent creep resistance and stress-rupture life. It is recommended for jet engine components operating up to 900 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well...
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Ti-8A1-1Mo-1V is a titanium alloy having excellent creep resistance and stress-rupture life. It is recommended for jet engine components operating up to 900 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness and creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-32. Producer or source: Titanium Metals Corporation of America.
Journal Articles
Alloy Digest (1952) 1 (2): Mg-2.
Published: 01 October 1952
... Flylite ZRE-1 is a creep resistant magnesium-base alloy primarily designed for jet engine components and other high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep...
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Flylite ZRE-1 is a creep resistant magnesium-base alloy primarily designed for jet engine components and other high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Mg-2. Producer or source: Howard Foundry Company.
Journal Articles
Alloy Digest (1970) 19 (5): Ni-153.
Published: 01 May 1970
... NIMONIC 93 is a nickel-base alloy having high elevated temperature strength, high oxidation resistance and good corrosion resistance. It is recommended for jet engine and gas turbine components. This datasheet provides information on composition, physical properties, hardness, elasticity...
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NIMONIC 93 is a nickel-base alloy having high elevated temperature strength, high oxidation resistance and good corrosion resistance. It is recommended for jet engine and gas turbine components. 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, joining, and surface treatment. Filing Code: Ni-153. Producer or source: Henry Wiggin & Company Ltd.
Journal Articles
Alloy Digest (1987) 36 (9): Ti-88.
Published: 01 September 1987
.... 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...
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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.
Journal Articles
Alloy Digest (1967) 16 (9): Ni-127.
Published: 01 September 1967
... CM-R41 is a vacuum-melted, precipitation hardening nickel-base alloy possessing outstanding properties in the temperature range of 1200 F to 1800 F. It is recommended for jet engine and gas turbine components operating at high temperatures. This datasheet provides information on composition...
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CM-R41 is a vacuum-melted, precipitation hardening nickel-base alloy possessing outstanding properties in the temperature range of 1200 F to 1800 F. It is recommended for jet engine and gas turbine components operating at high temperatures. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-127. Producer or source: Cannon-Muskegon Corporation.
Journal Articles
Alloy Digest (1981) 30 (8): Ti-83.
Published: 01 August 1981
... to 1050 F. It is recommended for use where high creep strength is required, as in components for jet engines. It has outstanding advantages for long-time use at temperature to 800 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength...
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RMI 6Al-2Sn-4Zr-2Mo is an alpha-beta titanium alloy that provides a tensile strength of 130,000 psi in the mill-annealed condition. It is characterized by an excellent combination of tensile strength, creep strength, toughness and high-temperature stability that makes it suitable for service to 1050 F. It is recommended for use where high creep strength is required, as in components for jet engines. It has outstanding advantages for long-time use at temperature to 800 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as 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-83. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1994) 43 (7): Ni-457.
Published: 01 July 1994
... composition corrosion-resistant alloys hardness jet engine components joinability nickel brazing filler metals Nicrobraz 30 physical properties thermal properties NICROBRAP30 Filing Code: Nickel Alloy Ni-457 - DIGEST- JULY 1994 DATA ON WORLD WIDE METALS AND ALLOYS PWsh6dby: Abay Oi. Inc. I2014%9161...
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NICROBRAZ 30 is used for well diffused, high strength, heat resistant joints, and highly stressed structures such as jet engine parts. It is also used in nuclear reactors where boron cannot be tolerated. It has low base-metal penetration. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion resistance as well as joining. Filing Code: Ni-457. Producer or source: Wall Colmonoy Corporation.
Journal Articles
Alloy Digest (1959) 8 (3): Co-17.
Published: 01 March 1959
...: Haynes Stellite Company Copyright © ASM International® 1996 1996 ASM International chemical composition corrosion-resistant alloys creep properties elasticity fracture toughness Haynes alloy no. 36 heat treatability high-temperature alloys jet engine components joinability...
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HAYNES Alloy No. 36 is a cobalt-base alloy having excellent strength at temperatures up to 1800 deg. F. It is the cast modification of wrought HAYNES Alloy No. 25 and has been used successfully in jet engine blading and nozzle vanes. 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 heat treating, machining, and joining. Filing Code: Co-17. Producer or source: Haynes Stellite Company.
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