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gas turbine blades

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Journal Articles
Alloy Digest (2004) 53 (12): Co-109.
Published: 01 December 2004
... Udimet L-605 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. This datasheet provides information on composition, physical properties, and tensile properties as well as creep...
Journal Articles
Alloy Digest (2005) 54 (1): Co-110.
Published: 01 January 2005
... Udimet 188 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. The alloy has a tenacious oxide film. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1965) 14 (5): Co-44.
Published: 01 May 1965
... Deloro-Stellite-7 is a cobalt base casting alloy possessing excellent corrosion resistance and high temperature strength together with good ductility and excellent resistance to thermal shock. It is recommended for gas turbine blades, brass casting dies and extrusion dies. This datasheet provides...
Journal Articles
Alloy Digest (2009) 58 (6): Ni-669.
Published: 01 June 2009
...-hardening, nickel-base alloy that was originally developed as an industrial gas turbine blade alloy. Later, this alloy was used for aircraft engine disks and blades. The alloy is solid solution strengthened by additions of chromium, cobalt, molybdenum, and tungsten, while additions of titanium and aluminum...
Journal Articles
Alloy Digest (1960) 9 (11): Ni-33.
Published: 01 November 1960
... for aircraft use requiring ade- quate strength for forged aircraft gas turbine blades at temperatures up to 1650 deg. F. It can operate at a working temperature approximately 150 deg. higher than lnconel X alloy. Its mechanical prop- erties at 1650 deg. F. are very similar to those of Inconel X at I500 deg...
Journal Articles
Alloy Digest (2007) 56 (12): Ni-656.
Published: 01 December 2007
.... It also has high resistance to fatigue under very arduous conditions. These properties combined with the high oxidation resistance inherent in the nickel-chromium alloys, makes L080A an ideal materials for gas turbine blades and other highly stressed components operating within the recommend limits...
Journal Articles
Alloy Digest (1990) 39 (2): Ni-379.
Published: 01 February 1990
... as high as 155OOF (843°C) for short time service. Avoid exposure to sulfur-containing atmospheres. The alloy is machinable, hot and cold work- able, and weldable by arc and resistance methods. Forms Available: Billets, bars, forgings and parts. Applications: Jet engine turbine blading, stationary gas...
Journal Articles
Alloy Digest (1998) 47 (2): Ni-537.
Published: 01 February 1998
... is a unique single crystal casting superalloy devel- oped for gas turbine engine blade and vane applications where demanding strength and environmental issues prevail. This non- rhenium containing alloy exhibits short-term creep rupture strengths that are similar to lower chromium-containing, first generation...
Journal Articles
Alloy Digest (1959) 8 (2): Ni-50.
Published: 01 February 1959
... Characteristics: Inconel 713C nickel-chromium cast alloy has outstand- ing rupture strength at 1700 F. combined with ex- cellent resistance to thermal fatigue and good casta- bility. Forms Available: Investment castings. Applications: Gas turbine blades in jet engines. Manufacturer: The International Nickel...
Journal Articles
Alloy Digest (1989) 38 (12): Ni-377.
Published: 01 December 1989
... shafts or seamless tubulars. Applications: Gas turbine blades and other components which operate at very high temperatures. Producer: Teledyne Allvac Monroe, North Carolina 28 1 lo-053 1 Teledyne Vasco Latrobe, Pennsylvania 15650. ...
Journal Articles
Alloy Digest (1972) 21 (4): Ni-172.
Published: 01 April 1972
... to 18OOoF combined with corrosion resistance enabling it to withstand long exposure to the hot corrosive environments associated with the engine. Forms Available: Investment castings. Applications: industrial gas turbine blades and vanes. Manufacturer: Licensees of lnternationai Nickel New York, N.Y. 10004. ...
Journal Articles
Alloy Digest (2023) 72 (8): Ni-785.
Published: 01 August 2023
... N07080 NiCr20TiAl (2.4952) General Characteristics Creep resistant up to 850 °C (1560 °F); excellent oxidation resistance. Product Forms Bar; forgings. Applications Highly stressed components such as chambers for diesel engines, combustion valves, discs, gas turbine blades, and shafts; bolts and nuts...
Journal Articles
Alloy Digest (1974) 23 (9): SS-300.
Published: 01 September 1974
... UNITEMP 1415NW is a high-strength modification of the hardenable, martensitic 12% chromium stainless steel. It has both corrosion and oxidation resistance through its useful temperatures range which is up to about 1050 F. Its applications include compressor blades of gas turbines and turbine discs...
Journal Articles
Alloy Digest (1963) 12 (6): Ni-44.
Published: 01 June 1963
... on an inquiry basis at the present time. ) Applications: Aircraft, marine and land-based gas turbine blades, combustion chambers and associated parts, rotor discs with and without integral blades, high temperature springs. Manufacturer: Utica Metals Division Kelsey-Hayes Company Ucica 4, New York ...
Journal Articles
Alloy Digest (1972) 21 (8): Ni-178.
Published: 01 August 1972
.... Its properties are developed by a solution heat treatment followed by a double aging treatment. The alloy is used for gas turbine blades and other highly stressed components operating within the recommended limits of temperature and stress. Forms Available: Reforging bar and billet, machining stock...
Journal Articles
Alloy Digest (2023) 72 (7): Ni-784.
Published: 01 July 2023
... for applications exposed to temperatures of up to 900 °C (1650 °F). Typical applications include casings, discs, exhaust reheaters, forging hammers, gas turbine blades, hot work tools, pressing tools, shafts, shear blades, springs, and swaging dies. Copyright © 2023, ASM International®. All rights reserved. Alloy...
Journal Articles
Alloy Digest (2007) 56 (5): Ni-650.
Published: 01 May 2007
... Boehler L311 VMR is a nickel alloy having high creep and rupture strength up to 760 deg C (1400 deg F) and scaling resistance in air to 850 deg C (1560 deg F). It is used in the aircraft and gas turbine industries as shafts, blades, and discs. This datasheet provides information on composition...
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 (1983) 32 (7): Ni-288.
Published: 01 July 1983
... resistance to oxidation and sulfidation. Alloy MA 6000 was developed as a blade material for advanced gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature...
Journal Articles
Alloy Digest (1987) 36 (1): Ni-51.
Published: 01 January 1987
... UDIMET 700 is a wrought nickel-base alloy produced by vacuum-induction melting and further refined by vacuum-arc remelting. It has excellent mechanical properties at high temperatures. Among its applications are blades for aircraft, marine and land-based gas turbines and rotor discs...