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turbine blade

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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 (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
... -ah1 1992. Alloy Digsst inc. All riqhfs rclbewed PMMby: Ailoy Di9-W. Inc 1201677-9161 Dalashowllam~,norrobelJs6dlof 27 Canliild SlreeI. Orange. NJ. 07060 I U.S.A s&xdkaltiorlmal~ign. CMSX-6@ (Low Density Single Crystal Nickel-Base Turbine Blade Alloy) CMSX-6 is a proprietaq low density, single crystal...
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 (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 (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 (1966) 15 (11): SA-204.
Published: 01 November 1966
... HECLA EM, 20 is an iron-nickel-cobalt-chromium austenitic alloy steel having high oxidation and scaling resistance. It is recommended for high temperature service and medium loads up to 2000 F, such as turbine blading, jet engine exhaust stacks and combustion chambers. This datasheet provides...
Journal Articles
Alloy Digest (1967) 16 (5): SS-194.
Published: 01 May 1967
... ESSHETE 1250 is an austenitic creep resistant alloy steel recommended for high temperature service in the range 550-675 C. It is used for superheaters, pressure vessels, fasteners and turbine blades. This datasheet provides information on composition, physical properties, hardness, elasticity...
Journal Articles
Alloy Digest (1967) 16 (9): SS-200.
Published: 01 September 1967
... AISI No. 616 is a hardenable martensitic type stainless steel recommended for high temperature applications up to 1200 F. It is used for steam turbine blades and buckets, valves, jet engine components, and high temperature bolting. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (2004) 53 (4): Ni-620.
Published: 01 April 2004
... 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...
Journal Articles
Alloy Digest (2004) 53 (12): Co-109.
Published: 01 December 2004
... Udimet L-605 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. This datasheet provides information on composition, physical properties, and tensile properties as well as creep...
Journal Articles
Alloy Digest (2005) 54 (1): Co-110.
Published: 01 January 2005
... Udimet 188 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. The alloy has a tenacious oxide film. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1964) 13 (2): Ni-88.
Published: 01 February 1964
... SM-200 is a nickel-base alloy designed primarily as a cast turbine blade material which retains useful strength up to 1900 F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance...
Journal Articles
Alloy Digest (1964) 13 (11): Ni-95.
Published: 01 November 1964
... 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...
Journal Articles
Alloy Digest (1965) 14 (11): Ni-107.
Published: 01 November 1965
... MAR-M Alloy 200 is a nickel-base alloy designed primarily as a cast turbine blade material which retains useful strength up to 1900 F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature...
Journal Articles
Alloy Digest (1970) 19 (3): Ni-151.
Published: 01 March 1970
... IN-100 is a vacuum melted and investment cast nickel-base alloy recommended for turbine blades operating at 1850-1900 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes...
Journal Articles
Alloy Digest (1981) 30 (10): Co-79.
Published: 01 October 1981
... International aerospace components AISI No. 671 chemical composition corrosion-resistant alloys creep properties elasticity fatigue properties fracture toughness hardness heat treatability joinability machinability oxidation resistance physical properties tensile properties turbine blades...
Journal Articles
Alloy Digest (1981) 30 (12): SS-398.
Published: 01 December 1981
... CRUCIBLE 403 is a hardenable steel containing 11.50-13.00% chromium. Its composition and mill processing are controlled carefully to produce a product capable of meeting the severe requirements of steam turbine blading and other high-requirement uses. Crucible 403 is magnetic at all times...