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aircraft gas turbine engine components

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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 (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 (2020) 69 (4): Co-130.
Published: 01 April 2020
..., nonmagnetic. Product Forms Bar, coil, sheet Applications Afterburner liners, aircraft engine components, combustor cans, flame holders, gas turbines, transition ducts Supplier United Performance Metals 3475 Symmes Road Hamilton, Ohio 45015, USA Tel: +1 513 860 6500 Web: www.upmet.com ISSN 002-614X Co-130B ...
Journal Articles
Alloy Digest (1970) 19 (7): Ni-155.
Published: 01 July 1970
... Udimet 901 is a nickel-base alloy having high tensile and rupture strength to 1200 F. It is recommended for use in aircraft, aerospace and gas turbine components. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep...
Journal Articles
Alloy Digest (1957) 6 (12): Ni-38.
Published: 01 December 1957
... INCOLOY 901 is a nickel-base alloy having creep and rupture strength at 1000 to 1400 F. It is recommended for use in aircraft and industrial gas turbine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also...
Journal Articles
Alloy Digest (1975) 24 (4): Ni-216.
Published: 01 April 1975
..., Ti) type. Pyromet 901 is used for components in aircraft and gas turbines. such as turbine rotors, compressor discs, hubs, and shafts. This alloy is available as induction- vacuum plus vacuumarc-remelted material. Forms Available: Forging billets, hot and cold finished bars, strip and wire...
Journal Articles
Alloy Digest (1967) 16 (10): Ni-128.
Published: 01 October 1967
... NIMONIC 110 is a highly alloyed nickel-base alloy having high creep and oxidation resistance. It is recommended for aircraft gas turbine components to resist the stresses at the very high temperatures of operation. This datasheet provides information on composition, physical properties, elasticity...
Journal Articles
Alloy Digest (1966) 15 (2): Ni-111.
Published: 01 February 1966
... be continued as low as 16OOoF minimum. Exposure at high temperatures to sulphurous atmospheres or to other sources of sulphur musr be avoided. Billers, bars, forgings, sheer and srrip Applications: Aircraft and industrial gas rurbincs components . turbine rotor and compressor discs, srructural members...
Journal Articles
Alloy Digest (2007) 56 (5): Ni-649.
Published: 01 May 2007
...: This alloy has been used primarily in the aerospace industry for items such as gas turbine rotor blades, gas turbine wheels, bolts, and other gas turbine structural parts. It has also found use in jet engine afterburners and airframe and missile structures. Non-aerospace applications include heat treat...
Journal Articles
Alloy Digest (1967) 16 (11): Co-54.
Published: 01 November 1967
... MAR-M Alloy 509 is a vacuum melted, cobalt-base alloy having high strength, low creep rates, and resistance to oxidation and thermal shock. It is recommended for aircraft and industrial gas turbine applications. This datasheet provides information on composition, physical properties, hardness...
Journal Articles
Alloy Digest (2009) 58 (7): Ni-671.
Published: 01 July 2009
... in aircraft turbine engines and land-based gas turbines, It is typically supplied in the solution-annealed condition and then age hardened by the customer after fabrication. The alloy is nickel based, but it also contains a significant amount of cobalt, which gives it superior high- temperature strength over...
Journal Articles
Alloy Digest (1968) 17 (4): SS-208.
Published: 01 April 1968
... pressings. Transformation ro marrensite occurs during deformation. Forms Available: Sheet and scrip Applications: Steam and gas turbine components, supersonic air- craft parts. Manufacturer: The minimum strength values are obtainable from welds where the weld metal is of the same composition or deposited...
Journal Articles
Alloy Digest (1960) 9 (11): Ni-33.
Published: 01 November 1960
.... F. This new alloy wiIl enable aircraft engine builders to either increase the performance of the current engines or to plan the designing of future engines to operate at a higher temperature range. Forms Available: Hot rolled bars and forgings. Applications: Forged aircraft gas turbine blades...
Journal Articles
Alloy Digest (1974) 23 (4): Ni-203.
Published: 01 April 1974
... on 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...
Journal Articles
Alloy Digest (1956) 5 (1): Ni-22.
Published: 01 January 1956
... in the annealed, as-forged or as-rolled condition. Its creep properties under certain conditions may be somewhat improved by high-temperature solution- treatment. Forms Available: Sheets, tubes, bars, sections, wires, forgings. Applications: Combustion chamber linings in gas turbines, aircraft engine components...
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 (1986) 35 (11): SS-478.
Published: 01 November 1986
... superalloy with a relatively high ratio of strength to alloying element content. It is capable of withstanding high static and dynamic stresses through at least I 200 F. It is used for various high-temperature applications such as components for jet engines. gas turbines. turbochargers and missiles...
Journal Articles
Alloy Digest (1972) 21 (9): Ni-179.
Published: 01 September 1972
... by conventional techniques. Suggested uses include gas-turbine aircraft-engine components and other applications involving high-temperature service. Forms Available: Sheet, strip, plate, rod, bar, tube. Applications: Gas turbine components such as combustion cans, transition liners, afterburner components, spray...
Journal Articles
Alloy Digest (1981) 30 (4): Ni-267.
Published: 01 April 1981
.... Forms Available: Billets, bars, sheet and forgings. Applications: Unitemp 41 is used for jet engine components such as after burner parts, turbine casing, nozzle diaphragm partitions and combustion liners. Other uses include airframe components for aircraft and missiles, turbine buckets, turbine wheels...
Journal Articles
Alloy Digest (1992) 41 (5): Ni-404.
Published: 01 May 1992
... 5828. welding wire. General Characteristics: ALLVAC WASPALOY. a gamma prime precipitation harden- ing high-temperature nickel-base alloy is produced by vacuum induction melting and consumm able electrode, vacuum arc or electroslag remelting. The alloy has good oxidation and gas turbine atmosphere...