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gas turbines

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Journal Articles
Alloy Digest (1985) 34 (9): SS-463.
Published: 01 September 1985
... CARPENTER MOLY ASCOLOY is a chromium-nickel-molybdenum-vanadium hardenable martensitic stainless steel designed for service up to 1200 F (649 C). It is utilized in steam turbine buckets and in compressor components in gas turbines and in other high-temperature applications. This datasheet provides...
Journal Articles
Alloy Digest (1969) 18 (1): SS-219.
Published: 01 January 1969
... Crucible CG27 is a forgeable iron-nickel base alloy having an excellent combination of high temperature stress-rupture and tensile properties. It resists oxidation up to 1500 F and is recommended for gas turbine engines and turbine wheels. This datasheet provides information on composition...
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 (2014) 63 (10): Ni-719.
Published: 01 October 2014
... Alloy IN 939 was developed for turbine airfoils and has been used extensively in industrial gas turbines. However, the development of the alloy and the joining technology required for application to large structural components in aero engines includes risks. This datasheet covers a weldable...
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 (1986) 35 (2): Ni-328.
Published: 01 February 1986
... CARPENTER WASPALOY is a precipitation-hardening nickel-base alloy designed for use at elevated temperatures. It is used for gas turbine engine parts requiring considerable strength and corrosion resistance up to 1600 F. The alloy is usually vacuum-induction melted or vacuum induction plus vacuum...
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 (1986) 35 (11): SS-478.
Published: 01 November 1986
..., gas turbines, turbochargers and missiles. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well...
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 (2001) 50 (8): Ti-118.
Published: 01 August 2001
... TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. This datasheet provides information on composition, physical properties...
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 (1996) 45 (12): Ni-519.
Published: 01 December 1996
... ANVAL 625 is a corrosion- and oxidation-resistant coating superalloy. Applications include the restoration of equipment for the pulp and paper, chemical process, and gas turbine industries. This datasheet provides information on composition, physical properties, and hardness. It also includes...
Journal Articles
Alloy Digest (1997) 46 (5): Fe-56.
Published: 01 May 1997
... Pyromet CTX-1 is a high-strength, precipitation-hardenable superalloy exhibiting a low coefficient of thermal expansion and high strength up to about 1200 deg F. The alloy possesses high hot hardness and good thermal fatigue resistance. Its applications include components for gas turbine engines...
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 (1999) 48 (7): Ni-557.
Published: 01 July 1999
... Haynes alloy 75 is an 80 nickel-20 chromium alloy with both good oxidation resistance and good mechanical properties at high temperatures. It is amenable to all forms of fabrication and welding. A typical application for sheet metal is fabrications in gas turbine engines. This datasheet provides...
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 (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 (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...