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Journal Articles
Alloy Digest (2007) 56 (1): SA-559.
Published: 01 January 2007
... 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...
Journal Articles
Alloy Digest (2007) 56 (2): SS-987.
Published: 01 February 2007
.... BOEHLER M314 EXTRA Filing Code: SS-987 Stainless Steel February 2007 BOEHLER M314 EXTRA (Tempered Turbine Blade Steel) Böhler M314 Extra is free machining with high sulfur, prehardened, and corrosion resistant with 16% Cr. It is used as holder frames for plastic mold tooling. Hardening. The tool must...
Journal Articles
Alloy Digest (1993) 42 (1): Ni-420.
Published: 01 January 1993
... turbine blade and vane airfoils are now replacing equiaxed and DS counmrparts in turbine en- gines. This development is stimulated by the increased tempemtur&ress capability and the superior thermal and cyclic fatigue properties of the single crystal compo- nents. Form Available: Cast single crystals...
Journal Articles
Alloy Digest (1992) 41 (10): Ni-415.
Published: 01 October 1992
... CM 247 LC alloy is a derivative of the MAR M 247 composition, specifically designed for directionally solidified (DS) turbine blade and vane applications. This datasheet provides information on composition and physical properties. It also includes information on casting and heat treating. Filing...
Journal Articles
Alloy Digest (1992) 41 (12): Ni-418.
Published: 01 December 1992
... CMSX-6 is a low density, single crystal alloy development to retrofit existing turbine designs. This datasheet provides information on composition and physical properties as well as creep. It also includes information on casting. Filing Code: Ni-418. Producer or source: Cannon-Muskegon Corporation...
Journal Articles
Alloy Digest (1981) 30 (4): Ni-267.
Published: 01 April 1981
... in sheet form; consequently, it is used widely for jet engine components. Other uses include turbine buckets, turbine wheels, rings and high-temperature fasteners and springs. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
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 (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 (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 (1969) 18 (1): SS-219.
Published: 01 January 1969
... Crucible CG27 is a forgeable iron-nickel base alloy having an excellent combination of high temperature stress-rupture and tensile properties. It resists oxidation up to 1500 F and is recommended for gas turbine engines and turbine wheels. This datasheet provides information on composition...
Journal Articles
Alloy Digest (2014) 63 (10): Ni-719.
Published: 01 October 2014
... Alloy IN 939 was developed for turbine airfoils and has been used extensively in industrial gas turbines. However, the development of the alloy and the joining technology required for application to large structural components in aero engines includes risks. This datasheet covers a weldable...
Journal Articles
Alloy Digest (2016) 65 (5): SA-753.
Published: 01 May 2016
... Böhler (or Boehler) T550 is a creep resisting steel, hardened and tempered. It is used for components requiring elevated high-temperature strength for use in thermal engines and power plants, such as turbine blades, turbine disks, screws, bolts, pins, and shafts. This datasheet provides...
Journal Articles
Alloy Digest (1991) 40 (11): Ni-104.
Published: 01 November 1991
... NIMONIC alloy 115 is a nickel/chromium/cobalt based alloy developed as a vacuum processed creep resisting alloy for service at temperatures up to about 1010 C (1850 F) as a turbine blade material for aircraft turbines. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1993) 42 (6): Ni-434.
Published: 01 June 1993
... 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...
Journal Articles
Alloy Digest (1964) 13 (6): Co-37.
Published: 01 June 1964
... Nivco 10 is a cobalt-base turbine alloy having a combination of high damping capacity, high strength and high ductility. It is a precipitation hardening alloy recommended for use at temperatures up to 1200 F, such as turbine blades. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1964) 13 (6): SS-157.
Published: 01 June 1964
... Uniloy 1409 TB is turbine quality 12% chromium stainless steel developed to meet the exacting demands of highly stressed parts where good strength and ductility along with corrosion resistance are required. It is recommended for applications in turbine construction. This datasheet provides...
Journal Articles
Alloy Digest (2020) 69 (4): Co-130.
Published: 01 April 2020
... UPM Nickel Alloy 188 (UNS R30188 / Werkstoff Number 2.4683) is a low-carbon, cobalt-nickel-chromium-tungsten alloy that combines excellent high-temperature strength with very good oxidation resistance up to 1095 °C (2000 °F). It is widely used in commercial and military aircraft gas turbine...
Journal Articles
Alloy Digest (1957) 6 (12): Ni-38.
Published: 01 December 1957
... INCOLOY 901 is a nickel-base alloy having creep and rupture strength at 1000 to 1400 F. It is recommended for use in aircraft and industrial gas turbine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also...
Journal Articles
Alloy Digest (1958) 7 (1): SS-67.
Published: 01 January 1958
... NIMONIC DS is a wrought, austenitic nickel-chromium-iron alloy having high oxidation and heat resistance. It is recommended for furnace parts and gas turbine components. This datasheet provides information on composition, physical properties, and elasticity as well as creep. It also includes...
Journal Articles
Alloy Digest (1959) 8 (4): Ni-52.
Published: 01 April 1959
... 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...