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compressors

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Journal Articles
Alloy Digest (2001) 50 (8): Ti-117.
Published: 01 August 2001
... strength up to 430 °C (800 °F). RMI 5Al-2Zr-2Sn-4Mo-4Cr (Ti-17) (Engine Compressor Alloy) Filing Code: Ti-117 Titanium August 2001 RMI 5Al-2Zr-2Sn-4Mo-4Cr (Ti-17) Chemical Composition, wt Aluminum 4.5 5.5 Chromium 3.5 4.5 Molybdenum 3.5 4.5 Tin 1.5 2.5 Zirconium 1.5 2.5 Iron 0.3 max Nitrogen 0.04 max...
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 (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...
Journal Articles
Alloy Digest (2001) 50 (7): Ti-116.
Published: 01 July 2001
... TIMETAL 834 is a Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C alloy with high strength and creep resistance up to 593 C (1100 F). The alloy is workable and weldable. It is used in the aerospace industry for rings and compressor disks. This datasheet provides information on composition, physical...
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 (1968) 17 (2): SA-222.
Published: 01 February 1968
... AISI No 602 is a low-alloy high-temperature constructional steel of the Cr-Mo-V-Si type that possesses useful strength after suitable heat treatment at temperatures up to 1000 F. It is used for jet engine compressor wheels and blading. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1968) 17 (9): SS-213.
Published: 01 September 1968
... Carpenter Pyromet 355 is a chromium nickel-molybdenum stainless steel which can be heat treated to high strength levels. It is recommended for gas turbine compressor parts where high strength is required at intermediate elevated temperatures. This datasheet provides information on composition...
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 (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 (1967) 16 (6): Ti-51.
Published: 01 June 1967
... HYLITE 50 is a complex alpha plus beta titanium alloy developed as a compressor blade and disc material, recommended for the highest duty service. It has high tensile and creep properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile...
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 (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 (2013) 62 (6): Ti-150.
Published: 01 June 2013
... ATI 17 Ti-5Al-2Sn-2Zr-4Cr-4Mo is also known as Ti-17. It was developed by General Electric for fan and compressor discs. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well...
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 (1977) 26 (9): CI-44.
Published: 01 September 1977
.... Typical applications are automotive equipment, compressors, machine tools and general machinery applications. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also...
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 (1995) 44 (5): SS-595.
Published: 01 May 1995
... SOLEIL C5 is a 13% chromium 4% nickel martensitic stainless steel with improved toughness and good corrosion resistance to fresh water. Shafts and compressor impellers for hydraulic applications is the area of primary usage. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1983) 32 (11): SA-395.
Published: 01 November 1983
... LESCALLOY U1-18 is a medium-carbon, low-alloy heat-resistant steel having high strength to 1000 F (538 C). It is made by vacuum-consumable-electrode melting to provide a preferred ingot solidification and superior microcleanliness. It is used for turbine and compressor rotor shafts. This datasheet...
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 (1955) 4 (6): SS-31.
Published: 01 June 1955
... 1420 WM is a high-strength modification of standard AISI turbine blading steel, 12% chromium Type 403. It has outstanding resistance to stress-cor- rosion cracking and has been used to overcome this problem in highly-stressed tiow compressor blad- ing Because of its high chromium intent it does...