1-20 of 76 Search Results for

turbine discs

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
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 (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...
Journal Articles
Alloy Digest (2007) 56 (1): SA-559.
Published: 01 January 2007
... usual upper-temperature limit 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...
Journal Articles
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...
Journal Articles
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...
Journal Articles
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. This...
Journal Articles
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...
Journal Articles
Alloy Digest (1968) 17 (1): Ti-54.
Published: 01 January 1968
...). Weldability: Bars and billets for forging are normally supplied in the saess relieved (i.e. annealed) condition. Bars and billets for machining and forgings are normally supplied in the heat treated condition. Application= Jet engine components, airframe forgings, fasteners, turbine compressor discs...
Journal Articles
Alloy Digest (1962) 11 (9): Ni-32.
Published: 01 September 1962
... 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...
Journal Articles
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 at...
Journal Articles
Alloy Digest (1970) 19 (5): Ni-153.
Published: 01 May 1970
... resistance. 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. ...
Journal Articles
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 ...
Journal Articles
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...
Journal Articles
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...
Journal Articles
Alloy Digest (1981) 30 (9): Ni-271.
Published: 01 September 1981
... Available: Billets, bars, rods, casting stock. sheet, strip, tubing, wire and forgings Applications: Gas turbine engines; turbine discs, buckets and rings in jet engines; airframe assemblies; fasteners; missile systems; and a wide variety of other high-temperature uses. Manufacturers: Nickel aBoy miBs. ...
Journal Articles
Alloy Digest (1975) 24 (4): Ni-216.
Published: 01 April 1975
..., Ti) type. Pyromet 901 is used for components in aircraft and gas turbines. such as turbine rotors, compressor discs, hubs, and shafts. This alloy is available as induction- vacuum plus vacuumarc-remelted material. Forms Available: Forging billets, hot and cold finished bars, strip and wire...
Journal Articles
Alloy Digest (1964) 13 (2): SS-152.
Published: 01 February 1964
... strength at temperatures up co and including 1100oF. Fom s Available: Billets, hot rolled and cold finished bars, wire, cold rolled strip, and special shapes. Applications: Jet engine and steam turbine components, aircraft structural parts. Turbine blades, wheels, discs and turbine shafts. Manufacturer...
Journal Articles
Alloy Digest (1957) 6 (12): Ni-38.
Published: 01 December 1957
... temperarure. Light working without rensile or bending stresses could be conrinued as low as 1600 deg F., but no work should be at- tempted between 1600 deg F. and 1200 deg F. be- Aircraft and industrial gas turbines components, tur- bine rotor and compressor discs, structural parts. Manufacturer: The...
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 (1966) 15 (4): Co-47.
Published: 01 April 1966
... data and information were taken from the publication of the American Iron and Steel Institute High Temperature High Strength Alloys. Forms Available: Forgings, billets, bars, sheet, tubing wire, and castings. Applications: Turbine blades, vanes, discs, combustion chambers, jet stacks, jer combs...