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jet engine components

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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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
Journal Articles
Alloy Digest (1959) 8 (3): Co-17.
Published: 01 March 1959
...: Haynes Stellite Company Copyright ┬ę 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...