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gas turbine components

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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 (1958) 7 (1): SS-67.
Published: 01 January 1958
... NIMONIC DS is a wrought, austenitic nickel-chromium-iron alloy having high oxidation and heat resistance. It is recommended for furnace parts and gas turbine components. This datasheet provides information on composition, physical properties, and elasticity as well as creep. It also includes...
Journal Articles
Alloy Digest (1967) 16 (9): Ni-127.
Published: 01 September 1967
... CM-R41 is a vacuum-melted, precipitation hardening nickel-base alloy possessing outstanding properties in the temperature range of 1200 F to 1800 F. It is recommended for jet engine and gas turbine components operating at high temperatures. This datasheet provides information on composition...
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 (1968) 17 (8): SS-212.
Published: 01 August 1968
... CMN-155 is an austenitic iron-base alloy having high oxidation and heat resistance combined with good high temperature properties. It is recommended for jet engine and gas turbine components, high temperature fasteners, and rocket chambers. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1981) 30 (7): Ni-269.
Published: 01 July 1981
... and stress-rupture properties up to about 1500 F. Typical applications are gas-turbine components, airframes and fasteners. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature...
Journal Articles
Alloy Digest (1964) 13 (9): Co-40.
Published: 01 September 1964
... Haynes Alloy No. 152 is a cobalt-base, high-temperature casting alloy. It is designed for gas-turbine components requiring high strength properties in the 1000 to 2000 F temperature range. This datasheet provides information on composition, physical properties, and tensile properties as well...
Journal Articles
Alloy Digest (1966) 15 (3): Ni-112.
Published: 01 March 1966
... FIRTH FS-718 is an austenitic nickel-base alloy having good cryogenic properties, and excellent strength and oxidation resistance up to 1300 F. It is highly recommended for missile and gas turbine components. This datasheet provides information on composition, physical properties, elasticity...
Journal Articles
Alloy Digest (1970) 19 (5): Ni-153.
Published: 01 May 1970
... NIMONIC 93 is a nickel-base alloy having high elevated temperature strength, high oxidation resistance and good corrosion resistance. It is recommended for jet engine and gas turbine components. This datasheet provides information on composition, physical properties, hardness, elasticity...
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 (1978) 27 (3): Ni-187.
Published: 01 March 1978
... PYROMET 680 is a nonmagnetic nickel-base alloy that derives its exceptional properties up to 2200 F (1200 C) from solid solution strengthening. Among its applications are gas turbine components and furnace hardware. This datasheet provides information on composition, physical properties, hardness...
Journal Articles
Alloy Digest (2003) 52 (12): Ni-618.
Published: 01 December 2003
... RA718 is a nickel alloy precipitation hardened by gamma prime and double prime. It is readily fabricated and is weldable even in the aged condition. The alloy is used for gas turbine components at temperatures up to 650 deg G (1200 deg F) as well as for cyogenic equipment. This datasheet provides...
Journal Articles
Alloy Digest (1990) 39 (7): Cer-4.
Published: 01 July 1990
... SILICON NITRIDE SN-220 has found its niche in industrial applications in engine and gas turbine components. It has excellent high-temperature strength and thermal shock resistance. This datasheet provides information on composition, physical properties, elasticity, and bend strength as well...
Journal Articles
Alloy Digest (1986) 35 (8): SS-473.
Published: 01 August 1986
... INCOLOY Alloy DS is a wrought, austenitic nickel-chromium-iron alloy with high resistance to heat and oxidation. Its many applications include furnace parts, woven-wire conveyor belts for continuous furnaces, radiant heat tubes and gas-turbine components. This datasheet provides information...
Journal Articles
Alloy Digest (1988) 37 (2): Fe-83.
Published: 01 February 1988
... INCOLOY alloy 907 is a high-strength alloy having a low coefficient of thermal expansion. It is a precipitation hardening alloy. INCOLOY alloy 907 is useful for gas-turbine components where it provides for closer control of clearances and tolerances. This datasheet provides information...
Journal Articles
Alloy Digest (1974) 23 (5): SS-296.
Published: 01 May 1974
... PYROMET 350 is a chromium-nickel-molybdenum stainless steel that can be hardened by transformation to martensite and/or preciptation hardening. It is used for gas turbine components and similar parts where high strength is required at room intermediate temperatures. This datasheet provides...
Journal Articles
Alloy Digest (1996) 45 (4): Ni-339.
Published: 01 April 1996
... Nimonic alloy 901 is a nickel-base alloy strengthened by additions of molybdenum, titanium, and aluminum. It possesses high creep and rupture strength from 1000 to 1400 deg F. Applications include components for gas turbines, bolting, and valve stems for power applications. This datasheet provides...
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 (1971) 20 (3): Ni-163.
Published: 01 March 1971
... solutions. It also resists chloride-ion stress corrosion. The alloy can be forged at temperatures above 18000F and can be cold worked in the soft condition. It can be joined by resistance welding and by the inert-gas tungsten arc process. It is used for gas turbine components, air frameand missile...
Journal Articles
Alloy Digest (1987) 36 (9): Ni-351.
Published: 01 September 1987
... are suitable with high-speed steel tooling; water-soluble lubricants are recommended with carbide tools. Workability: NIMONIC ALLOY 86 was developed asa sheetalloy with improved workability as an objective. The alloy has very good workability. It is capable of being formed into gas turbine components...