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commercial aircraft gas turbines

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Journal Articles
Alloy Digest (1966) 15 (2): Ni-111.
Published: 01 February 1966
... Udimet 901 is a nickel-base alloy having high creep and rupture strength at 1000 to 500 F. It is used in disc and other heavy forgings for commercial aircraft gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep...
Journal Articles
Alloy Digest (1979) 28 (4): Al-234.
Published: 01 April 1979
... 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 (2020) 69 (4): Co-130.
Published: 01 April 2020
... UPM Nickel Alloy 188 (UNS R30188 / Werkstoff Number 2.4683) is a low-carbon, cobalt-nickel-chromium-tungsten alloy that combines excellent high-temperature strength with very good oxidation resistance up to 1095 °C (2000 °F). It is widely used in commercial and military aircraft gas turbine...
Journal Articles
Alloy Digest (1974) 23 (4): Ni-203.
Published: 01 April 1974
... careful control of production processes to achieve high and consistent properties. Its primary usage is in gas turbine compressor and turbine components. This datasheet provides information on composition, physical properties, microstructure, and elasticity as well as fracture toughness, creep, and...
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 (1960) 9 (10): Ni-61.
Published: 01 October 1960
... formed readily using conventional techniques. D777 wire solution created at 195OoF and 205OoF has been successfullv cold headed. Sheets, scrips, bars, wire, foil forms, forgings, billets, and welded cubing. Applications: Aircraft gas rurbines, missiles, airframes, commercial turbines, shafts, discs...
Journal Articles
Alloy Digest (1980) 29 (6): Ti-77.
Published: 01 June 1980
... 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...
Journal Articles
Alloy Digest (1973) 22 (10): Ti-69.
Published: 01 October 1973
.... Bar roiling and extrusions can be accomplished in this temperature range. Sheets are rolled in the range 1750.19OOoF. Wddabil ity: Applications: Highcompressor components for aircraft jet engines and other rotating gas-turbine parts. Static !lat-rolled components where temperature resistance is...