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cryogenic gas turbines
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Journal Articles
Publisher: Journals Gateway
Alloy Digest (1966) 15 (7): Ni-115.
Published: 01 July 1966
... INCONEL alloy X-750 is an age-hardenable, nickel-chromium alloy used for its corrosion and oxidation resistance and high creep rupture strength at temperature up to 1500 F. It also has excellent properties at cryogenic temperatures. It was originally developed for use in gas turbines, but because...
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INCONEL alloy X-750 is an age-hardenable, nickel-chromium alloy used for its corrosion and oxidation resistance and high creep rupture strength at temperature up to 1500 F. It also has excellent properties at cryogenic temperatures. It was originally developed for use in gas turbines, but because of its low cost, high strength and weldability it has become the standards choice for a wide variety of applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-115. Producer or source: Huntington Alloy Products Division, An INCO Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1978) 27 (11): Ni-258.
Published: 01 November 1978
... that is precipitation hardenable. It exhibits exceptionally high yield strength up to 13OoOF, excellent cryogenic properties down to -42303 and superior weldability even in the fully-aged condition. This unusual combination of characteristics makes it suitable for elevated-temperature applications in gas turbines...
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UDIMET 718 is a nickel-base alloy that is precipitation hardenable. It exhibits exceptionally high yield strength up to 1300 F, excellent cryogenic properties down to -423 F and superior weldability even in the fully-aged condition. This unusual combination of characteristics makes it suitable for elevated-temperature applications in gas turbines and in critical components for missiles. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-258. Producer or source: Special Metals Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1974) 23 (5): SA-304.
Published: 01 May 1974
... range of 300 to 600 F, and components for spacecraft, jet engines and gas turbines. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature...
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UNIMAR 250 is a maraging alloy steel having high strength, good notch toughness, excellent cryogenic properties and deep hardenability. It is recommended for pressure vessels, solid-fuel rocket cases and pressure bottles, landing-gear components, processing equipment operating in the temperature range of 300 to 600 F, and components for spacecraft, jet engines and gas turbines. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-304. Producer or source: Cyclops Corporation.
Journal Articles
Publisher: Journals Gateway
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...
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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 tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-112. Producer or source: Firth Sterling Inc..
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Publisher: Journals Gateway
Alloy Digest (2012) 61 (2): Fe-158.
Published: 01 February 2012
... Cryogenic components and piping Laser components Liquefied natural gas (LNG): production and storage equipment; LNG tanker membranes Marine components Wind turbines Producer: Sandmeyer Steel Company Philadelphia, PA 19116-3598 USA Tel: 215-464-7100 Fax: 215-677-1430 Web: www.SandmeyerSteel.com ISSN...
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SSC Invar 36 was developed for use in applications where dimensional stability is essential. It is a nickel-iron alloy with a very low coefficient of thermal expansion from cryogenic temperatures to 200 deg C (390 deg F). It is utilized in aerospace composite tooling and die applications, as well as laser components, and cryogenic components and piping: liquefied natural gas production, storage, and transportation. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as forming. Filing Code: Fe-158. Producer or source: Sandmeyer Steel Company. Originally published December 2011, revised February 2012.
Journal Articles
Publisher: Journals Gateway
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...
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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 information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Ni-618. Producer or source: Rolled Alloys Inc.
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Publisher: Journals Gateway
Alloy Digest (2018) 67 (10): SS-1295.
Published: 01 October 2018
... resistance than 304. This material is a good choice for corrosion resistant re- bar and in heat exchangers, pressure vessels, piping, and the like. This material is used in aerospace gas turbine engine mounts and retaining rings, and has been used in gas turbine compressor blades. This material is approved...
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Electralloy Nitronic 33 was created with a high-yield strength, excellent toughness, and ductility. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as joining. Filing Code: SS-1295. Producer or source: Electralloy, a Division of G.O. Carlson Inc..
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Publisher: Journals Gateway
Alloy Digest (2013) 62 (4): SS-1142.
Published: 01 April 2013
..., and slightly better stress corrosion cracking resistance than 304, make Nitronic 33 a good choice for corrosion resistant rebar, and in heat exchangers, pressure vessels, piping, and the like. This alloy is used in aerospace gas turbine engine mounts and retaining rings, and has been used in gas turbine...
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Electralloy’s Nitronic 33 is a nitrogen strengthened austenitic stainless steel. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion and wear resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-1142. Producer or source: Electralloy, a Division of G.O. Carlson Inc.. See also Alloy Digest SS-324, January 1976.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1974) 23 (12): Ni-212.
Published: 01 December 1974
... matris. The alloy has excellent fatigue strength and stress-corrosion-craking resistance to chloride ions. Forms Available: Strip. billet. bar, wire and tubular products. Applications: Furnace hardware, gas turbine engine ductmg. heat shields. combustion liners and spray bars, chemrcal plant hardware...
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PYROMET 625 is a nonmagnetic alloy with outstanding strength and toughness from cryogenic temperatures to 2000 F. It has excellent fatigue strength and stress-corrosion-cracking resistance to chloride ions. Some typical applications are heat shields, chemical plant hardware and special seawater applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-212. Producer or source: Carpenter Technology Corporation.
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Publisher: Journals Gateway
Alloy Digest (2021) 70 (2): Ni-767.
Published: 01 February 2021
... to 700 °C (1290 °F). Wait for equalization of the temperature. Soak for 16 h. Air cool. Applications For applications up to 595 650 °C (1100 1200 °F) where ATI 80 A is typically used for turbine blading for jet engines greater creep-rupture ductility is desirable, a three-step and stationary gas turbines...
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ATI 80 A is a wrought, precipitation-hardenable, Ni-Cr-Ti-Al alloy that is generally used for high strength applications up to 760 °C (1400 °F), but may also be used at temperatures up to 845 °C (1550 °F) for short duration service. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ni-767. Producer or source: ATI.
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Alloy Digest (1988) 37 (8): Ni-359.
Published: 01 August 1988
... strength is required (gas turbine components) also for cryogenic conditions. Manufacturer: Haynes International, inc. Kokomo. Indiana 469049013 @ Registered trademark of HAYNES INTEXNA- TIONAL, INC. ...
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HAYNES alloy No. 718 is a precipitation-hardening nickel-base alloy with good ductility and excellent high-temperature strength and oxidation resistance. It is produced by vacuum melting and consumable electrode remelting, either electroslag or vacuum arc. The alloy welds readily and it excels in resisting post-weld (strain-age) cracking. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ni-359. Producer or source: Haynes International Inc..
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Publisher: Journals Gateway
Alloy Digest (2009) 58 (12): SS-1050.
Published: 01 December 2009
..., billet, bar, and coil rod sizes. Bar is available as either rounds or flats. Melt methods include: VIM-VAR and EAF-AOD-VAR. Applications: Typical applications include jet engine, gas turbine, and supercharger components such as turbine wheels, fasteners, nozzles, and exhaust parts. This alloy is also...
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LSS A286 is a precipitation-hardening, austenitic stainless steel designed for use at temperatures up to 704 deg C (1300 deg F), where high tensile strength, excellent creep strength, and good corrosion resistance are required. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: SS-1050. Producer or source: Latrobe Specialty Steel Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1978) 27 (9): Ni-257.
Published: 01 September 1978
... UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. This datasheet...
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UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-257. Producer or source: Special Metals Corporation.
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Publisher: Journals Gateway
Alloy Digest (2015) 64 (9): Ni-723.
Published: 01 September 2015
... for a variety of applications that require high elevated-temperature strength in larger section sizes along with good fabricability. The alloy has been used for turbine discs in large industrial gas turbines as well as aerospace turbines. Other turbine engine parts include shafts, cases, mounts, and fasteners...
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Pyromet alloy 706 has similarities to alloy 718, but improves fabricability and welding. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-723. Producer or source: Carpenter Specialty Alloys.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1973) 22 (12): Ni-198.
Published: 01 December 1973
... and gas turbines, rocket engines, heat shields, furnace hardware, chemical plant hardware and in sea water environments. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes...
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PYROMET 102 is a nonmagnetic, nickel-chromium base alloy which is solid solution strengthened by the refractory metals niobium, tungsten and molybdenum. It possesses excellent corrosion properties, strength, ductility, toughness and structural stability. It is used as tubing and piping for steam and gas turbines, rocket engines, heat shields, furnace hardware, chemical plant hardware and in sea water environments. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-198. Producer or source: Carpenter Technology Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1989) 38 (2): Ni-368.
Published: 01 February 1989
.... Fabrica- tion of the alloy is enhanced by its good formability and welda- bility. in addition to its favorable machining characteristics. Ihe alloy has excellent resistance to postweld strain-age cracking. It is an ataactive material for gas-turbine components and other parts which must have high...
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UNS N09706 is a precipitation-hardenable, nickel-iron-chromium alloy with high strength at temperatures to 1200 F and with good resistance to oxidation and corrosion over a broad range of temperatures and environments. 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 performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-368. Producer or source: Nickel and nickel alloy producers.
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Publisher: Journals Gateway
Alloy Digest (2006) 55 (10): SS-977.
Published: 01 October 2006
... turbine applications with moderately high strength up to 705 °C (1300 °F) and oxidation resistance to 815 °C (1500 °F). Product Forms Available: A-286 is available in a wide variety of sizes and forms, including ingot, billet, bar, and coil rod. Applications: Typical applications include gas turbine disks...
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Electralloy A-286 is an austenitic precipitation-hardening Fe-Ni-Cr alloy. It is used for applications requiring high strength and corrosion resistance up to 650 deg C (1200 deg F), and for lower-stress applications at higher temperatures. It has applications at ambient temperatures where a heat treatable, nonmagnetic material is required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-977. Producer or source: Electralloy, a Division of G.O. Carlson Inc.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1974) 23 (2): Ni-201.
Published: 01 February 1974
... discs; aircraft parts such as frames and cases in the diffuser. burner. turbine and exhaust areas, and for fasteners; cryogenic uses; welded and redrawn heatexchanger tubing; hot-tooling applications demanding high-temperature hardness under severe thermal cycling and environmental conditions...
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UNITEMP 718 is a nickel-base austenitic precipitation-hardenable alloy for extended service at temperatures up to 1200 F. For short periods the alloy performs well to about 1300 F. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-201. Producer or source: Cyclops Corporation.
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Alloy Digest (1989) 38 (11): Ni-376.
Published: 01 November 1989
... for NICKEL- VAC-901 is 1600-18OO F (871-982 C). As with heat treatment, avoid sulfur contamination when heating for forging. The alloy may be cold formed in the solution treated condition to produce complex forms. Weldability: NICKELVAC-901 may be welded using gas tungsten-arc (TIG) or gas metal-arc (MIG...
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NICKEL VAC-901 is an iron-nickel base alloy with high strength and good oxidation resistance up to 1400 F (760 C). It is precipitation hardenable and is produced by vacuum induction melting followed by vacuum are remelting which greatly minimizes directionality of properties in large billets and forgings. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-376. Producer or source: Teledyne Allvac.
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Publisher: Journals Gateway
Alloy Digest (1970) 19 (11): Ni-159.
Published: 01 November 1970
... strain-age cracking. The properties of alloy 706 make it an attractive material for gas-turbine components and other parts which must have high strength combined with ease of fabrication. Forms Available: Rods, bars. tube, sheet, strip and plate. Popular forms and sizes are available from stock. Wire...
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INCONEL Alloy 706 is a precipitation-hardenable, nickel-iron-chromium alloy with high strength at temperatures to 1300 F and with good resistance to oxidation and corrosion over a broad range of temperatures and environments. Its characteristics are similar to those of INCONEL Alloy 718, except that Alloy 706 has greatly improved machinability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-159. Producer or source: Huntington Alloy Products Division, An INCO Company.
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