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engine components

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Journal Articles
Alloy Digest (2021) 70 (3): Al-474.
Published: 01 March 2021
... properties. It offers good strength in the as-cast condition and is often used that way. However, it is possible to increase strength considerably by heat treatment. In applications that experience high temperatures, as in engine components, it is common to employ a T5, T7, or O treatment. These treatments...
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): Cb-12.
Published: 01 September 1967
... Columbium WC-103 is a columbium-base alloy having good high temperature strength, good weldability and fabricability. It is recommended for high performance rocket engine components for temperatures up to 2800 F for controlled periods of time. This datasheet provides information on composition...
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 (1971) 20 (1): Co-62.
Published: 01 January 1971
... HAYNES Alloy No. 188 is a cobalt-base alloy which has excellent high-temperature strength, outstanding oxidation resistance, and good post-aging ductility. It is recommended for aircraft engine components. (U.S. Pat. 3,418,111 This datasheet provides information on composition, physical properties...
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 (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 (1964) 13 (4): Ti-39.
Published: 01 April 1964
... Harvey HA-7146 is an alpha-beta type titanium-base bar and forging alloy developed to combine high temperature strength and stability with good forgability. It is recommended for aircraft gas turbine engine components due to its improved stress stability and creep resistance. It responds to an age...
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 (1965) 14 (12): SS-175.
Published: 01 December 1965
... AISI No. 615 is a hardenable chromium-nickel-tungsten martensitic corrosion resistant steel used primarily at temperatures up to 1050 F. It is used for compressor blades, vanes, discs, and other gas turbine engine components. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1969) 18 (3): Al-185.
Published: 01 March 1969
... ALUMINUM 2014 is a heat treatable alloy having high tensile and fatigue strength. It is recommended for fittings, hardware, aircraft engine components, structures, etc. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear...
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 (1983) 32 (1): Ni-282.
Published: 01 January 1983
... the stresses caused by phase changes in carbon steels and martensitic stainless steels. Because of this combination of characteristics, it is used widely for joining aircraft engine components. This datasheet provides information on composition, physical properties, and microstructure. It also includes...