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Aircraft turbine engine components
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Journal Articles
Alloy Digest (2007) 56 (1): SA-559.
Published: 01 January 2007
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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 temperature performance as well as forming, heat treating, and joining. Filing Code: SA-559. Producer or source: Böhler-Uddeholm North America.
Journal Articles
Alloy Digest (2004) 53 (4): Ni-620.
Published: 01 April 2004
Abstract
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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 performance and corrosion resistance as well as heat treating. Filing Code: Ni-620. Producer or source: Special Metals Corporation.
Journal Articles
Alloy Digest (2001) 50 (7): Cu-670.
Published: 01 July 2001
Abstract
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ToughMet 3 is a Cu-15Ni-8Sn alloy. ToughMet is a line of spinoidal alloys for bearings capable of performing with a variety of shafting materials and lubricants. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion and wear resistance as well as machining. Filing Code: CU-670. Producer or source: Brush Wellman Inc.
Journal Articles
Alloy Digest (2000) 49 (4): Cu-649.
Published: 01 April 2000
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Olin C195 is a high-strength, high-conductivity copper alloy developed for applications in current-carrying parts. Typical applications are electrical springs, connectors, and clips. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: CU-649. Producer or source: Olin Brass.
Journal Articles
Alloy Digest (1999) 48 (9): SS-763.
Published: 01 September 1999
Abstract
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Carpenter Stainless Type 304HN is the high-nitrogen version of Type 304 and 304H stainless steels. Interstitial strengthening with both carbon and nitrogen provides this alloy with significantly higher yield and tensile strength as annealed. Typical applications include aerospace and power components, as well as marine shafting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-763. Producer or source: Carpenter. See also Alloy Digest SS-368, October 1979.
Journal Articles
Alloy Digest (1999) 48 (3): SA-498.
Published: 01 March 1999
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Lescalloy 6305 VAC-ARC steel is a modified AISI 4140 steel with higher molybdenum content and additional vanadium. The alloy is most frequently used in the quenched and tempered condition. Jet engine shafting is a typical application. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-498. Producer or source: Latrobe Steel Company.
Journal Articles
Alloy Digest (1998) 47 (9): Al-352.
Published: 01 September 1998
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Kaiser Aluminum alloy 2011 is one of the most popular screw machine stock alloys available. Tennalum, a division of Kaiser Aluminum, produces alloy 2011 in the T3 temper as Microchip II, which offers excellent machinability and surface finish. The chips from Tennalum’s Microchip II (T3 temper only) are known for being small in size. Alloy 2011 is typically used in connectors and fittings, brake pistons, computer parts, knobs, and meter shafts. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: AL-352. Producer or source: Kaiser Aluminum Corporation.
Journal Articles
Alloy Digest (1998) 47 (6): SS-719.
Published: 01 June 1998
Abstract
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Allegheny Ludlum Type 310 is an austenitic chromium-nickel steel with high heat resisting properties. It is recommended for furnace equipment, heat treating boxes, burners, heat recovery systems, jet engine components, and heat exchangers. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness, creep, and fatigue. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: SS-719. Producer or source: Allegheny Ludlum Corporation.
Journal Articles
Alloy Digest (1996) 45 (1): Ni-495.
Published: 01 January 1996
Abstract
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Colmonoy No. 635, a Nickel-base hard surfacing Alloy, contains a formulated mixture of both crushed and atomized powders. It achieves a hardness of RC 58-63 with tungsten carbide particles. Typical applications include hardfacing of pump components and shaft sleeves. It is supplied as a powder for aplication with Wall Colmonoy’s SPRAYWELD Process. This datasheet provides information on composition, physical properties, microstructure, and hardness. It also includes information on heat treating, machining, and powder metal forms. Filing Code: Ni-495. Producer or source: Wall Colmonoy Corporation.
Journal Articles
Alloy Digest (1995) 44 (7): SS-599.
Published: 01 July 1995
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BioDur TrimRite Stainless has a composition that is balanced to be fully martensitic in the hardened condition. The alloy possesses a moderately high level of corrosion resistance and is applied as valve parts, guides, shafting and cutlery, including surgical tools. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as heat treating and machining. Filing Code: SS-599. Producer or source: Carpenter.
Journal Articles
Alloy Digest (1995) 44 (6): Cu-601.
Published: 01 June 1995
Abstract
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HIDURON alloy 191 was developed for marine applications where both a combination of strength and good corrosion/ impingement resistance is needed. It finds applications in shafts, fasteners and valve stems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: CU-601. Producer or source: Langley Alloys Ltd.
Journal Articles
Alloy Digest (1995) 44 (5): SS-595.
Published: 01 May 1995
Abstract
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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, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness and fatigue. It also includes information on forming, heat treating, and joining. Filing Code: SS-595. Producer or source: Creusot-Marrel.
Journal Articles
Alloy Digest (1994) 43 (11): Ni-469.
Published: 01 November 1994
Abstract
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NICROBRAZ 150 is excellent for jet engine parts and similar highly stressed components. It has good strength at lower brazing temperatures. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion resistance as well as joining. Filing Code: Ni-469. Producer or source: Wall Colmonoy Corporation.
Journal Articles
Alloy Digest (1994) 43 (8): SA-212.
Published: 01 August 1994
Abstract
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LEDLOY 4140 is a lead and/or tellurized chromium-molybdenum alloy steel having free cutting characteristics. It is recommended for gears, shafts, fasteners and similar machinery parts. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-212. Producer or source: Inland Steel Company. Originally published as Incut 4140, June 1967, revised August 1994.
Journal Articles
Alloy Digest (1994) 43 (7): Ni-457.
Published: 01 July 1994
Abstract
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NICROBRAZ 30 is used for well diffused, high strength, heat resistant joints, and highly stressed structures such as jet engine parts. It is also used in nuclear reactors where boron cannot be tolerated. It has low base-metal penetration. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion resistance as well as joining. Filing Code: Ni-457. Producer or source: Wall Colmonoy Corporation.
Journal Articles
Alloy Digest (1994) 43 (6): Ni-455.
Published: 01 June 1994
Abstract
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NICROBRAZ 125 is for well diffused, high strength, heat resistant joints, and highly stressed structures such as jet engine parts. This datasheet provides information on composition and physical properties. It also includes information on joining. Filing Code: Ni-455. Producer or source: Wall Colmonoy Corporation.
Journal Articles
Alloy Digest (1993) 42 (6): Ni-434.
Published: 01 June 1993
Abstract
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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 disc. This datasheet provides information on composition and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating and powder metal forms. Filing Code: Ni-434. Producer or source: Crucible Compaction Metals.
Journal Articles
Alloy Digest (1991) 40 (11): Ni-104.
Published: 01 November 1991
Abstract
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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, elasticity, and tensile properties as well as creep. It also includes information on heat treating. Filing Code: Ni-104. Producer or source: INCO Alloys Limited. Originally published as Nimonic 115, August 1965, revised November 1991.
Journal Articles
Alloy Digest (1989) 38 (10): SA-440.
Published: 01 October 1989
Abstract
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AISI 8642 is a triple-alloy steel that can be hardened by austenitizing and quenching in oil. This steel has moderate hardenability with relatively high strength and toughness, especially in the quenched-and-tempered condition. It is used in a wide range of components, parts and tools; examples are bolts, shafts, gears, wrenches, axles and housings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on heat treating, machining, joining, and surface treatment. Filing Code: SA-440. Producer or source: Alloy steel mills and foundries.
Journal Articles
Alloy Digest (1988) 37 (12): SA-435.
Published: 01 December 1988
Abstract
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UNS H-86170 is a low-carbon nickel-chromium-molybdenum carburizing steel of good hardenability. Its core is characterized by good strength and toughness. It is recommended for heavy-duty applications such as cams, chains, fasteners, gears, shafts and piston pins. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-435. Producer or source: Alloy steel mills and foundries.
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