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compressors components

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Journal Articles
Alloy Digest (1967) 16 (1): SS-190.
Published: 01 January 1967
... AISI No. 634 is a transformation and precipitation hardening stainless steel. It is used for applications such as pressure vessels, aircraft constructural components and jet engine compressor components. This datasheet provides information on composition, physical properties, hardness, elasticity...
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 (2007) 56 (6): Ti-140.
Published: 01 June 2007
... of tensile strength, creep strength, toughness, and high-temperature stability for long-term application at temperatures up to 538 °C (1000 °F). Its primary application is gas turbine compressor components such as blades, disc, and impellers. This alloy is also used in sheet metal form for engine afterburner...
Journal Articles
Alloy Digest (1968) 17 (1): Ti-54.
Published: 01 January 1968
... Hylite 60 is an alpha plus beta alloy having high tensile strength and good creep properties. It is suitable for compressor discs and blades and other highly stressed components up to 500 C. This datasheet provides information on composition, physical properties, elasticity, and tensile properties...
Journal Articles
Alloy Digest (1980) 29 (6): Ti-77.
Published: 01 June 1980
... include components for gas-turbine compressors, air-frame forgings, pressure vessels and special ordnance equipment. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear and bend strength as well as fracture toughness, creep, and fatigue...
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 (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 (1987) 36 (7): Fe-78.
Published: 01 July 1987
... and can be plated with chromium. CTX-3 uses comprise compressor and exhaust casings, seals and other components for gas turbine engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion...
Journal Articles
Alloy Digest (1968) 17 (9): SS-213.
Published: 01 September 1968
... or in the equalized and over-tempered condition.) Applications: Gas turbine compressor components, such es blades, discs, rotors end shafts. valves, high temperature components. Manufacturer: The Carpenter Steel Company Resdxng. Pennsylvania ...
Journal Articles
Alloy Digest (1962) 11 (1): Ti-5.
Published: 01 January 1962
... Available: Bars, plates, and forgings. Applications requiring a high strength-weight ratio at room temperature and moderately devated service temperatures. Jet engine compressor components are typical applications. Specification Equivalents: Manufacturer: tiv!S 4923 Titanium Met& Corporation of America EIL...
Journal Articles
Alloy Digest (1981) 30 (7): Ni-269.
Published: 01 July 1981
... successfully, using low speeds and heavy feeds to avoid excessive work hardening. Hot forging presents no unusual problems and the alloy can be welded. Forms Available: Billets, bars, rods, sheet, strip, wire, tubing and forgings. Applications: Aircraft gas turbine and compressor components, bolts, screws...
Journal Articles
Alloy Digest (2013) 62 (6): Ti-150.
Published: 01 June 2013
... Equivalents: UNS R58650 SAE AMS 4995 Billet General Characteristics: ATI 17 (Ti-5Al-2Sn-2Zr-4Cr-4Mo) alloy (UNS R58650) also known as Ti-17, was developed by General Electric as a high strength, deep hardening alloy for fan and compressor discs and for other large components. It has been classified as a beta...
Journal Articles
Alloy Digest (2012) 61 (1): Ti-149.
Published: 01 January 2012
... billet UNS R58650 General Characteristics: This alloy, also known as ATI Ti-17 alloy, was developed by General Electric as a high strength, deep hardening alloy for fan and compressor discs and for other large components. It has been classified as a beta-rich alpha-beta alloy. The alloy may...
Journal Articles
Alloy Digest (2003) 52 (2): SS-873.
Published: 01 February 2003
... very good strength and toughness properties in con- junction with reliable welding characteristics, NIROSTA 4313 is used for mechanically highly stressed components in fitting and pump construction, for compressors and turbines in hydroelectric power stations, and in mineral oil and refrigeration...
Journal Articles
Alloy Digest (1977) 26 (9): CI-44.
Published: 01 September 1977
... tools, automotive equipment, farm machinery, in the as-cast condition; however, it may be stress railway components, mining and ore-dressing equipment, relieved for dimensional stability, or after heavy mach- compressors, bushings, general machinery applications. ining. Stress Relief: Heat to 1050...
Journal Articles
Alloy Digest (1963) 12 (4): Ti-34.
Published: 01 April 1963
... HYLITE 40 is a titanium-aluminum-manganese alloy of high strength with excellent properties as forgings and bar stock. It is recommended for compressor dises and blades. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
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 (1974) 23 (9): SS-300.
Published: 01 September 1974
... of the turbine. Forms Available: Billets, forgings. bars. rods. sheet. s:rip and wire. Applications: High-temperature components such 3s compressor blades for gas turbines. turbine discs. rings ior jet engines. fasteners and valve parts. Manufacturer: UniversalCyclops Specialty Steel Division Cyclops Corporation...
Journal Articles
Alloy Digest (2004) 53 (11): Ti-135.
Published: 01 November 2004
... of its high chromium content. Specification Equivalents: UNS R58650 SAE AMS 4995 billet General Characteristics: This alloy was developed by General Electric as a high-strength deep-hardening alloy for fan and compressor discs and for other large components. It has been classified as a beta-rich alpha...
Journal Articles
Alloy Digest (1985) 34 (10): Al-261.
Published: 01 October 1985
... ALUMINUM 296.0 is an aluminum permanent-mold casting alloy that is recommended for applications requiring a combination of good machinability and high tensile properties. It can be age hardened by heat treatment. Among its uses are aerospace fittings and parts, compressor connecting rods...