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JET FORGE
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Journal Articles
Alloy Digest (1960) 9 (2): TS-90.
Published: 01 February 1960
... JET FORGE is a hot work die steel for forging high temperature alloys. It offers toughness and high wear resistance on high temperature applications involved in forging jet parts. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness...
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JET FORGE is a hot work die steel for forging high temperature alloys. It offers toughness and high wear resistance on high temperature applications involved in forging jet parts. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, machining, and joining. Filing Code: TS-90. Producer or source: Vanadium Alloys Steel Company.
Journal Articles
Alloy Digest (1962) 11 (9): Ni-32.
Published: 01 September 1962
... ALLOY M252 is a high-strength nickel-base forging alloy recommended for heavy duty jet engine and gas turbine buckers. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on forming...
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ALLOY M252 is a high-strength nickel-base forging alloy recommended for heavy duty jet engine and gas turbine buckers. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-32. Producer or source: Crucible Steel Company of America. Originally published March 1957, revised September 1962.
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...
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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 on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-52. Producer or source: Universal Cyclops Steel Corporation.
Journal Articles
Alloy Digest (1978) 27 (8): Al-95.
Published: 01 August 1978
... ALUMINUM 2218 is an aluminum-copper-nickel-magnesium alloy (formerly designated B18S Alloy). It is a standard forging alloy and is recommended for elevated-temperature service. It is used for aircraft and jet engine components. This datasheet provides information on composition, physical...
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ALUMINUM 2218 is an aluminum-copper-nickel-magnesium alloy (formerly designated B18S Alloy). It is a standard forging alloy and is recommended for elevated-temperature service. It is used for aircraft and jet engine components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-95. Producer or source: Various aluminum companies. Originally published September 1960, revised August 1978.
Journal Articles
Alloy Digest (1983) 32 (3): TS-412.
Published: 01 March 1983
... the many uses for this steel are hot-die applications, structural parts for jet engines and missiles, extrusion mandrels and forging dies. This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes information on forming, heat treating, machining...
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GUTERL H-11 is a 5% chromium hot-work tool steel with an excellent combination of red hardness, shock resistance (toughness) and resistance to abrasion; these are the properties needed for good hot-work characteristics. It will withstand drastic cooling from maximum operating temperatures. Among the many uses for this steel are hot-die applications, structural parts for jet engines and missiles, extrusion mandrels and forging dies. This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: TS-412. Producer or source: Guterl Special Steel Corporation.
Journal Articles
Alloy Digest (1967) 16 (5): Ni-124.
Published: 01 May 1967
... and forgings, wire, sheer, strip, place, ingots and ocher forms. Applications: Heavy-duty jet engine and gas turbine buckets, high temperature bolting, jet engine turbine wheels and ocher critical jet engine components. Manufacturer: Special Metals, Inc. New Hartford, New York ...
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UDIMET M-252 is a vacuum induction method alloy recommended for heavy-duty high temperature applications in the range 1300-1600 F. It has good stress-rupture strength, fatigue strength and mechanical strength at elevated temperatures. The alloy responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-124. Producer or source: Special Metals Inc..
Journal Articles
Alloy Digest (1986) 35 (11): SS-478.
Published: 01 November 1986
.... such as in many heat- resisting applications. This is the treatment regularly applied co bar stock and forgings for jet engine. gas turbine and turbocharger bolting. rotors and blades. for service below 1 3005 F. Machinability: AISI No. 651 is readily machinable. usingthe techniques commonly used for the AlSl 300...
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AISI No. 651 is an austenitic iron-base superalloy with a relatively high ratio of strength to alloying element content. It is capable of withstanding high static and dynamic stresses through at least 1200 F. It is used for various high-temperature applications such as components for jet engines, gas turbines, turbochargers and missiles. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-478. Producer or source: Stainless steel mills.
Journal Articles
Alloy Digest (1973) 22 (9): Ni-195.
Published: 01 September 1973
... application is for jet engine and gas turbine buckets. Forms Available: Billets for forging and bars in hot-roIled, anneaksd or heat-treated condition. Applications: Jet-engine and gas-turbine buckets. Manufacturer: Carpenter Technology Corporation Reading, Pennsylvania 19603. ...
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CARPENTER M-252 is an age-hardenable nickel-base alloy designed for highly stressed parts operating at temperatures up to 1600 F. Its prime application is for jet-engine and gas-turbine buckets. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-195. Producer or source: Carpenter.
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...
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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 information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SA-204. Producer or source: Union Carbide Corporation (Licensor).
Journal Articles
Alloy Digest (1970) 19 (1): Co-60.
Published: 01 January 1970
..., strip, bar, and forging stock. Applications: Parts in the afterburner and other hot sections of the jet engine. Support rings, burner liners, exhaust cone assemblies, nozzle diaphragm valves, high temperature valves and springs, gas turbine rotors and buckets. Highly stressed parts that must operate...
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CML-605 is a cobalt-base alloy having high strength, heat and oxidation resistance at elevated temperatures above 1600 F. It is recommended for gas turbine and jet engine components operating in the 1600 to 2000 F temperature range. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-60. Producer or source: Cannon-Muskegon Corporation.
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...
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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, tensile properties, and shear strength as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-190. Producer or source: Stainless steel mills.
Journal Articles
Alloy Digest (1969) 18 (1): SS-219.
Published: 01 January 1969
... in the form of fasteners and sheet. Forms Available: Bars and forgings. Applications: Forged rotating and stationary jet engine and gas turbine parts, turbine wheels, high temperature fasteners. Manufacturer: Crucible Steel Corp. Syracuse Division Syracuse, New York *Recommended by the editor. ...
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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, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-219. Producer or source: Crucible Materials Corporation.
Journal Articles
Alloy Digest (1965) 14 (3): Ti-4.
Published: 01 March 1965
... and is the strongest titanium-base aRoy now in production. The impact strength remains neatly constant with increasing temperature from 500 deg. F to 1100 deg. F. Forms Available: Ingots, forgings, bars, rods, plates, and extrusions. Applications: Airframe and jet engine forgings and fittings, airframe extruded shapes...
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MST 3AL-5CR is a double melted titanium base alloy available in either ingot, bar, rod, plate, forging, or extrusion form. It possesses good creep and high strength properties at room and elevated temperatures to 800 deg. F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-4. Producer or source: Mallory-Sharon Titanium Corporation. Originally published June 1954, revised March 1965.
Journal Articles
Alloy Digest (1968) 17 (1): Cb-14.
Published: 01 January 1968
... Columbium SCB-291 is a columbium-base alloy having excellent high temperature properties and good fabricability. It is recommended for nuclear reactors, space vehicles, jet and missile components. This datasheet provides information on composition, physical properties, hardness, and tensile...
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Columbium SCB-291 is a columbium-base alloy having excellent high temperature properties and good fabricability. It is recommended for nuclear reactors, space vehicles, jet and missile components. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Cb-14. Producer or source: Stauffer Metals Division, Stauffer Chemical Company.
Journal Articles
Alloy Digest (1964) 13 (11): Ti-42.
Published: 01 November 1964
... Republic RS-110C is a moderate strength highly weldable titanium alloy recommended for jet engine welded rings, aircraft skins, and structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness...
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Republic RS-110C is a moderate strength highly weldable titanium alloy recommended for jet engine welded rings, aircraft skins, and structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-42. Producer or source: Republic Steel Corporation, Titanium Division.
Journal Articles
Alloy Digest (1992) 41 (5): Ni-404.
Published: 01 May 1992
... as 1900°F (1038°C) are satisfactorily resisted. The ahoy performs well in atmospheres encountered in jet engine service and in salt spray environments. Specification Equivalents: ASM 5544. plate, sheet and strip AMS 5704. forgings AMS 5706,5707, bars, forgings and rings AMS 5708.5709, bars, forgings AMS...
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ALLVAC WASPALOY, a nickel-base precipitation hardening alloy derives its high strength through the precipitation of gamma prime as a result of the aluminum and titanium additions and through the solid solution strengthening of other component elements. It is produced by vacuum induction melting followed by consummable vacuum are or electroslag remelting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-404. Producer or source: Allvac Inc..
Journal Articles
Alloy Digest (2002) 51 (4): SS-851.
Published: 01 April 2002
... to 700 °C (1300 °F) on engine tests against all atmospheres encountered in jet engine service. The oxidation resistance is as good as Type 310 stainless steel up to 980 °C (1800 °F). Specification Equivalents: AISI Type 660 UNS K66286 DIN 1.4980 For bar and forgings: AMS 5731, 5732, 5734, 5735, 5736...
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Crucible A-286 is an age-hardenable austenitic Fe-Ni-Cr alloy designed for service up to 704 deg C (1300 deg F) on jobs requiring high strength and good corrosion resistance at the operating temperature. The alloy offers high ductility in notched sections. Crucible A-286 is used in jet engines and superchargers for various high-temperature components and is one of the few age-hardenable alloys used for bolting in the ASME Boiler and Pressure Vessel Code. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-851. Producer or source: Crucible Specialty Metals.
Journal Articles
Alloy Digest (1965) 14 (10): SS-173.
Published: 01 October 1965
..., cold drawn bars, rods and forgings, Applications: special shapes, wire and cold rolled scrip. Sream turbine blades and buckets; valves and valve trim; gas turbine and jet engine components; high remperarure bolting; compressor and turbine wheels; and aircrafr parts. Manufacturer: Practically all...
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AISI Type 422 is a hardenable 12% chromium stainless steel recommended for applications requiring superior strength to Type 403 stainless steel at elevated temperatures. It retains high strength and exhibits excellent ductility over the temperature range from room to 1200 F. It is recommended for turbine and jet engine components. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-173. Producer or source: Stainless steel mills.
Journal Articles
Alloy Digest (1966) 15 (4): Co-47.
Published: 01 April 1966
... and information were taken from the publication of the American Iron and Steel Institute High Temperature High Strength Alloys. Forms Available: Forgings, billets, bars, sheet, tubing wire, and castings. Applications: Turbine blades, vanes, discs, combustion chambers, jet stacks, jer combs, aircraft afterburner...
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AISI No. 670 is a ductile cobalt-base alloy developed for high temperature service. It has exceptional mechanical properties at temperatures up to 1800 F. It is recommended for highly stressed parts operating at high temperature levels, such as in gas turbines and jet engines. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-47. Producer or source: Alloy steel mills and foundries.
Journal Articles
Alloy Digest (2007) 56 (3): Ni-647.
Published: 01 March 2007
... ingot, billet, block, forged round bar, hot-rolled shapes and rectangles, bar, rod, wire, plate, sheet, strip, and castings. Applications: Typical applications are highly stressed components in the compressor and turbine sections of jet engines. References: 1. W.D. Cao, Nickel-Base Alloy, U.S. Patent...
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Allvac 718Plus alloy is a variant of alloy 718 (Alloy Digest Ni-90, April 1964) made by adding new elements and adjusting others. The triple melting produces a stronger alloy with consistent properties in strength, stability, and forgeability. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-647. Producer or source: Allvac, an Allegheny Technologies Company.
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