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turbine discs
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Journal Articles
Publisher: Journals Gateway
Alloy Digest (1993) 42 (6): Ni-434.
Published: 01 June 1993
... turbine discs CRUCIBLE P/M RENE 95 AND z NM34 SUPERSOLVUS RENE 95 JUNE 1993 - DIGEST- DATA ON WORLD WIDE METALS AND ALLOYS CRUCIBLE P/M RENE 95 AND SUPERSOLVUS RENE 95 (High Strength High Temperature Nickel-Base Alloy) P/M RENE 95 is a high strength, high temperature alloy used for rotating jet turbine...
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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 disc. This datasheet provides information on composition and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating and powder metal forms. Filing Code: Ni-434. Producer or source: Crucible Compaction Metals.
Journal Articles
Publisher: Journals Gateway
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...
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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. 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 as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-300. Producer or source: Cyclops.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1956) 5 (12): SS-50.
Published: 01 December 1956
.../asm.ad.ss0050 Copyright © ASM International® 1996 Table 8 - TEMPERATURE IMPACT (Solution treated and aged bars) TUnperanUe OF. charpy %y$ V-Notch -234 31 * Table 9 - CREEF PROPERTIES (gas turbine discs) Test Temperature Stress MhlilXlUmcmpRate OP. 9% per hour 1200 35Eo 1.11 x 10-r (At 1000 hours the total...
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DISCALOY is an iron-base heat treatable alloy having good high temperature strength and oxidation resistance. It is corrosion and heat resistant. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SS-50. Producer or source: Westinghouse Electric Corporation.
Journal Articles
Publisher: Journals Gateway
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...
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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, 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 as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-175. Producer or source: Alloy steel mills and foundries.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1964) 13 (1): SS-151.
Published: 01 January 1964
... componenrs, chat is, large turbine discs, rotor forgings, etc. Its scaling index is 0.5 mgms/sq cm after 7 cycles at 75OoC and 2.0 mgms/sq cm after 7 cycles at 85OoC Fonns Available: Forgings, bars Applications: Turbine discs, rotor forgings, turbine blades, bolts and other parts for high temperature work...
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FIRTH-VICKERS 326 steel is an austenitic alloy steel especially developed for high temperature applications in which high strength requirements are paramount. Its resistance to scaling is also of a high order. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and deformation. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SS-151. Producer or source: Firth-Vickers Stainless Steels Ltd.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1989) 38 (2): Ni-368.
Published: 01 February 1989
... strength combined with ease of fabrication. Foms Available: Rods, bars, tube. sheet, strip, plate and wire. Applications: Turbine discs, shafts and cases; diffuser cases; compressor discs and shafts; engine mounts; and fasteners. Manufactufw: Prodwas of nickel and nickel alloys. ...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1957) 6 (5): SS-56.
Published: 01 May 1957
... developed as a turbine disc material so that advantage could be taken of its high proof strength, low thermal expansion, ease of machining and lower cost when compared with the austenitic materials or- iginally used for this application. It has recently been used for large rotor forgings for industrial gas...
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JESSOP H46 is a ferritic type stainless steel having high strength at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-56. Producer or source: Wm. Jessop & Sons Ltd.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1964) 13 (11): Ni-95.
Published: 01 November 1964
...-induction melted nickel-base superalloy recommended for increased operating temperatures for jet engine forged blading and turbine discs and rings. It is a precipitation hardenable alloy. It has superior forgeability, and stress-rupture proper ties applicable for use in gas-turbine buckets operating...
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Udimet N-115 is a vacuum-induction melted nickel-base alloy that responds to precipitation hardening. It is a superalloy for extended service to 1850 F. It has been thus far limited to barstock for turbine blading applications and may be suitable for existing or future large forging applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. 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-95. Producer or source: Special Metals Inc..
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1989) 38 (11): Ni-376.
Published: 01 November 1989
... TIG or MIG techniques. The alloy should be pro- tected from sulfur containing atmospheres when exposed to high temperatures as in heat treatment or heating for forging. Forms Available: Bar, billet. Applications: Turbine discs and shafts, compressor blades and discs, high-temperature bolting. some...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1962) 11 (9): Ni-32.
Published: 01 September 1962
... in forgings which wilI result in large and irregular gram growth in subsequent heat treatment. To avoid this problem, as a general guide, all forging temperatures should be kept welI in excess of 1800 deg. F. (as in the manufacture of turbine discs). Small reductions (of the order of l-10 must be avoided...
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ALLOY M252 is a high-strength nickel-base forging alloy recommended for heavy duty jet engine and gas turbine buckers. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-32. Producer or source: Crucible Steel Company of America. Originally published March 1957, revised September 1962.
Journal Articles
Publisher: Journals Gateway
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...
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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. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. 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-51. Producer or source: Special Metals Corporation. Originally published March 1959, revised January 1987.
Journal Articles
Publisher: Journals Gateway
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...
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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, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-650. Producer or source: Böhler-Uddeholm Specialty Metals Inc.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1966) 15 (2): Ni-111.
Published: 01 February 1966
... Udimet 901 is a nickel-base alloy having high creep and rupture strength at 1000 to 500 F. It is used in disc and other heavy forgings for commercial aircraft gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep...
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Udimet 901 is a nickel-base alloy having high creep and rupture strength at 1000 to 500 F. It is used in disc and other heavy forgings for commercial aircraft gas turbines. 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-111. Producer or source: Special Metals Inc.. See also Alloy Digest Ni-155, July 1970.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1993) 42 (4): Ni-428.
Published: 01 April 1993
... turbiie discs and containment rings for aircraft auxiliary power units (APU). Thousands of APU high pressure turbine discs made from Crucible Low Carbon Astmloy are in service worldwide on com- mercial and military airplanes. Applications: P/M Low Carbon Astmloy is available as near net shapes...
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P/M LOW CARBON ASTROLOY offers good ductility and oxidation resistance in addition to excellent strength at high temperatures. This datasheet provides information on composition, physical properties, microstructure, and elasticity as well as creep. It also includes information on high temperature performance as well as heat treating. Filing Code: Ni-428. Producer or source: Crucible Compaction Metals.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2007) 56 (1): SA-559.
Published: 01 January 2007
... for continuous operation is 560 °C (1040 °F). Applications: Highly stressed turbine blades and turbine discs, screws, shafts, bolts, pins, and rings. Producer: Bohler-Uddeholm North America Rolling Meadows, IL 60008 (800) 652-2520 (847) 577-8028 (905) 813-8659 (fax) www.bucorp.com In Austria: Böhler Edelstahl...
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Boehler T552 Extra is a hardened and tempered steel with a combination of properties for stressed turbine blades. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: SA-559. Producer or source: Böhler-Uddeholm North America.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1970) 19 (5): Ni-153.
Published: 01 May 1970
.... Forms Available: Bars and forgings. Applications: Jet engine and gas turbine components, high-temperature bolts and fasteners, turbine discs and shafts. Manufacturer: Henry W@ & Co.. Ltd. Hereford, England. ...
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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 tensile properties as well as creep. 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-153. Producer or source: Henry Wiggin & Company Ltd.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2004) 53 (4): Ni-620.
Published: 01 April 2004
... properties fracture toughness heat treatability high-temperature alloys microstructure turbine blades turbine discs UDIMET 720 Chemical Composition, wt (Nominal) Nickel 56.0 Cobalt 14.7 Molybdenum 3.0 Tungsten 1.25 Chromium, disk applications 16.0 Chromium, blade applications 18.0 Titanium 5.0...
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Udimet 720 is a nickel-base alloy used in turbine blade and disk applications requiring high-temperature strength and structural stability. This datasheet provides information on composition microstructure as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating. Filing Code: Ni-620. Producer or source: Special Metals Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1959) 8 (4): Ni-52.
Published: 01 April 1959
... gram growth in subsequent heat treatment. To avoid this problem, as a general guide, all forging temperatures shoilld be kept well in excess of 1800 deg. F. (as in the manufacture of turbine discs). Small re- ductions (of the order of l-105) must be avoided below about 1800 deg. F. It must be noted...
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Unitemp M-252 is a high-strength nickel-base forging alloy recommended for heavy duty jet engine and gas turbine buckets. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-52. Producer or source: Universal Cyclops Steel Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1970) 19 (11): Ni-159.
Published: 01 November 1970
... and thin strip may be obtained from converters. Applications: Turbine discs, shafts and cases; diffuser cases; compressor discs and shafts; engine mounts; and fasteners. Manufacturer: Huntington AUoy Products Division The International Nickel Co., Inc. Huntington, West Virginia 25720. ...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1963) 12 (1): SA-140.
Published: 01 January 1963
... creep-strength at temperatures up to 1112oF (6000C). Forms Available: Billets, bars, and forgings. (large diameters) Applications: Gas turbine discs, extrusion liners, marine rotors, high temperature components. Manufacturer: J essop-Saville, Ltd. Brightside Works Sheffield, England ...
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Jessop-Saville H.40 is an alloy steel recommended for high-temperature stressed components of gas turbines. 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 as well as forming, heat treating, machining, and joining. Filing Code: SA-140. Producer or source: Jessop-Saville Ltd, Brightside Works.