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gas turbine engines

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Journal Articles
Alloy Digest (1969) 18 (1): SS-219.
Published: 01 January 1969
... Crucible CG27 is a forgeable iron-nickel base alloy having an excellent combination of high temperature stress-rupture and tensile properties. It resists oxidation up to 1500 F and is recommended for gas turbine engines and turbine wheels. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1986) 35 (2): Ni-328.
Published: 01 February 1986
... CARPENTER WASPALOY is a precipitation-hardening nickel-base alloy designed for use at elevated temperatures. It is used for gas turbine engine parts requiring considerable strength and corrosion resistance up to 1600 F. The alloy is usually vacuum-induction melted or vacuum induction plus vacuum...
Journal Articles
Alloy Digest (2001) 50 (8): Ti-118.
Published: 01 August 2001
... TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1997) 46 (5): Fe-56.
Published: 01 May 1997
... 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...
Journal Articles
Alloy Digest (1998) 47 (1): Ni-533.
Published: 01 January 1998
... for gas turbine engine applications. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: Ni-533. Producer...
Journal Articles
Alloy Digest (1999) 48 (7): Ni-557.
Published: 01 July 1999
... 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...
Journal Articles
Alloy Digest (1967) 16 (11): Ni-129.
Published: 01 November 1967
... WASPALOY is a vacuum induction melted nickel-base alloy having outstanding tensil and stress-rupture strength up to 1400 F combined with high oxidation resistance up to 1600 F. It is recommended for gas turbine engines, airframe assemblies and missile systems. This datasheet provides information...
Journal Articles
Alloy Digest (1967) 16 (8): Ti-52.
Published: 01 August 1967
... Ti-6Al-2Sn-4Zr-2Mo is a super-alpha titanium alloy providing an excellent combination of creep strength, tensile strength, toughness and stability to 1050 F. It is recommended for airframe and gas turbine engine requirements. This datasheet provides information on composition, physical properties...
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 (2006) 55 (5): Ti-138.
Published: 01 May 2006
... Timetal 551 is an improved-strength version of Timetal 550 alloy that retains good forging characteristics. The alpha-beta alloy has a nominal composition of Ti-4Al-4Mo-4Sn-0.5 Si, and it is used in gas turbine engine parts. This datasheet provides information on composition, physical properties...
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 (1981) 30 (9): Ni-271.
Published: 01 September 1981
... 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...
Journal Articles
Alloy Digest (1978) 27 (9): Ni-257.
Published: 01 September 1978
... 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...
Journal Articles
Alloy Digest (1979) 28 (4): Al-234.
Published: 01 April 1979
... 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...
Journal Articles
Alloy Digest (2000) 49 (3): Ni-560.
Published: 01 March 2000
... 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...
Journal Articles
Alloy Digest (1987) 36 (7): Fe-78.
Published: 01 July 1987
... 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...
Journal Articles
Alloy Digest (2020) 69 (4): Co-130.
Published: 01 April 2020
... International UPM Nickel Alloy 188 chemical composition physical properties workability joinability aircraft gas turbine engines thermal properties DOI: 10.31399/asm.ad.co0130 UPM NICKEL ALLOY 188 (Low-Carbon, Cobalt-Nickel-Chromium-Tungsten Alloy) Filing Code: Co-130 Cobalt :: April 2020...
Journal Articles
Alloy Digest (1971) 20 (4): Co-63.
Published: 01 April 1971
... to 0.03O-inch diameter has been produced using conventional techniques. Weldability: MAR-M 918 is a vacuum melted cobalt-base alloy for use in applications where high strength and oxidation resistance are required, as would be encountered in the burner can assembly of a gas turbine engine. The alloy can...
Journal Articles
Alloy Digest (2001) 50 (11): Ni-574.
Published: 01 November 2001
... conditions of fre- quent thermal cycling and in continuous exposure to temperatures up to 1038 °C (1900 °F). It has performed well in atmospheres found in gas turbine engine service and in salt-spray environments. Solution- treated material offers the best levels of corrosion resistance. Specification...
Journal Articles
Alloy Digest (1965) 14 (11): Ni-107.
Published: 01 November 1965
...-2450 0.105 0.108 0.122 1:; 198 6.0 7.3 8.2 9.7 30.8 27.1 21.4 Forms Available: Vacuum castings in either shell or investment molds. Applications: Turbine blades and vanes in aircraft gas turbine engines. Manufacturer: Martin Metals Company, Wheeling, Illinois DOI: 10.31399/asm.ad.ni0107 Copyright © ASM...