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turbine components

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Journal Articles
Alloy Digest (1992) 41 (10): Ni-415.
Published: 01 October 1992
... castability of CM 247 LC alloy has re- sulted in its selection for conventionally cast, large struc- tural turbine components for an advanced fighter engine. Industrial turbine applications for DS blade and vane components have developed in CM 247 LC alloy where natural gas is used as fuel. CM 247 LC alloy is...
Journal Articles
Alloy Digest (2007) 56 (2): SS-987.
Published: 01 February 2007
... freely in air. BOEHLER M314 EXTRA Filing Code: SS-987 Stainless Steel February 2007 BOEHLER M314 EXTRA (Tempered Turbine Blade Steel) Böhler M314 Extra is free machining with high sulfur, prehardened, and corrosion resistant with 16% Cr. It is used as holder frames for plastic mold tooling. Hardening...
Journal Articles
Alloy Digest (1993) 42 (6): Ni-434.
Published: 01 June 1993
... P/M RENE 95 is a high strength, high temperature alloy used for rotating jet turbine components. Supersolvus P/M Rene 95 provides even higher temperature creep and stress-rupture resistance than standard Rene 95. Both are available as-HIP performs. A typical application is a high pressure 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 (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 on...
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 on...
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 (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 as...
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 (1981) 30 (7): Ni-269.
Published: 01 July 1981
... 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 (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 (1969) 18 (9): Ni-147.
Published: 01 September 1969
... IN-102 is a nickel-chromium-iron alloy designed for long service at temperatures up to 1300 F. It combines high strength and high ductility at the elevated temperatures with a high degree of structural stability. It is used for aerospace, power and steam turbine components. This datasheet provides...
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, and...
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 (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 as...
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, and...
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 (4): SS-208.
Published: 01 April 1968
... Fifth-Vickers F.V. 520(S) is a corrosion resistant martensitic steel which is readily weldable and capable of being hardened by low temperature heat treatment. It is recommended for turbine components and supersonic aircraft parts. This datasheet provides information on composition, physical...