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Journal Articles
Publisher: Journals Gateway
Alloy Digest (1979) 28 (9): Bi-13.
Published: 01 September 1979
... CERROLOW-136 Alloy is a bismuth-base eutectic alloy that melts at 136 F (57.8 C), hence its identifying number. It is widely used in industry because of its low melting temperature and controlled-shrinkage characteristics. Among tis many applications are (1) Anchoring parts such as jet blades...
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CERROLOW-136 Alloy is a bismuth-base eutectic alloy that melts at 136 F (57.8 C), hence its identifying number. It is widely used in industry because of its low melting temperature and controlled-shrinkage characteristics. Among tis many applications are (1) Anchoring parts such as jet blades for machining, testing and inspection, (2) In the foundry for fusible cores in compound cores and (3) Low-melting solder. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, heat treating, and machining. Filing Code: Bi-13. Producer or source: Cerro Metal Products.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1984) 33 (2): Bi-35.
Published: 01 February 1984
... for use soon after it freezes. The alloy can be recovered easily and recycled into new uses any number of times. Among its many applications are (1) Anchoring parts such as jet blades for machining, testing and inspection, (2) In the foundry for fusible cores in compound corse and (3) Low-melting solder...
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Bismuth-21In-18Pb-12Sn is a bismuth-base eurectic alloy that melts at 136 F (57.8 C). It is widely used in industry because of is low melting temperature and its controlled-shrinkage characteristics. It provides the scientist, engineer and technician with an easily castable material that is ready for use soon after it freezes. The alloy can be recovered easily and recycled into new uses any number of times. Among its many applications are (1) Anchoring parts such as jet blades for machining, testing and inspection, (2) In the foundry for fusible cores in compound corse and (3) Low-melting solder. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, heat treating, machining, and joining. Filing Code: Bi-35. Producer or source: Producers of low-melting alloys.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1980) 29 (5): Bi-17.
Published: 01 May 1980
... and recycled into new uses any number of times. Its many uses include holding jet engine blades for machining, foundry patterns and fusible elements in safety devices. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information...
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OSTALLOY 281 is a bismuth-base eutectic alloy. Its melting temperature is 281 F (138 C); this is the highest melting point of the bismuth-base alloys commonly used in industry. It provides an easily castable material ready for use soon after it freezes. The alloy can be recovered easily and recycled into new uses any number of times. Its many uses include holding jet engine blades for machining, foundry patterns and fusible elements in safety devices. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, heat treating, and machining. Filing Code: Bi-17. Producer or source: Arconium Corporation of America, A.J Oster Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1980) 29 (9): Sn-10.
Published: 01 September 1980
... and recycled into new uses any number of times. Among its many uses are fusible mandrels for electroforming, proof casting in foundries, low-temperature solder, holding jet engine blades for machining and dies for wax patterns for investment casting. This datasheet provides information on composition, physical...
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INDALLOY 281-338 is a tin-base alloy that can be melted easily. It is non-eutectic alloy and melts through a temperature range of 281-338 F. It provides scientists and engineers with an easily castable material that is ready for use soon after it freezes; in addition, it can be recovered readily and recycled into new uses any number of times. Among its many uses are fusible mandrels for electroforming, proof casting in foundries, low-temperature solder, holding jet engine blades for machining and dies for wax patterns for investment casting. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, heat treating, and machining. Filing Code: Sn-10. Producer or source: Indium Corporation of America.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1980) 29 (11): Bi-20.
Published: 01 November 1980
... jet engine blades for machining and broaching, support for bending tubing and extrusions and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, forming, heat...
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OSTALLOY 158 is a bismuth-base, eutectic alloy that melts at 158 F (70 C). It provides engineers and technicians with an easily castable material that is ready for use as soon as it freezes. It can be recovered easily and recycled into new uses any number of times. Its many uses include holding jet engine blades for machining and broaching, support for bending tubing and extrusions and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, forming, heat treating, and machining. Filing Code: Bi-20. Producer or source: Arconium Corporation of America, A.J Oster Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1981) 30 (2): SS-382.
Published: 01 February 1981
... in continuous service to 1500 F and in intermittent service to 1800 F. Its many high-temperature applications include jet-engine turbine wheels and blades, bolting and afterburner parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
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AISI No. 660 is a heat-resistant iron-chromium-nickel alloy recommended for applications requiring high strength and good resistance to corrosion at temperatures up to 1300 F and for lower stresses at higher temperatures. This age-hardenable stainless steel has high resistance to oxidation in continuous service to 1500 F and in intermittent service to 1800 F. Its many high-temperature applications include jet-engine turbine wheels and blades, bolting and afterburner parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as 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: SS-382. Producer or source: Stainless steel mills.
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Publisher: Journals Gateway
Alloy Digest (1981) 30 (10): Co-79.
Published: 01 October 1981
... blades, parts for jet engines and aerospace components. 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...
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AISI No. 685 is a high-temperature, high-strength, cobalt-base alloy. It responds to an age-hardening heat treatment. At elevated temperatures it has high mechanical properties and excellent resistance to corrosion and oxidation. Its numerous applications include high-temperature hardware, turbine blades, parts for jet engines and aerospace components. 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: Co-79. Producer or source: High-strength, high-temperature alloy mills & foundries.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1959) 8 (3): Co-17.
Published: 01 March 1959
... HAYNES Alloy No. 36 is a cobalt-base alloy having excellent strength at temperatures up to 1800 deg. F. It is the cast modification of wrought HAYNES Alloy No. 25 and has been used successfully in jet engine blading and nozzle vanes. This datasheet provides information on composition, physical...
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HAYNES Alloy No. 36 is a cobalt-base alloy having excellent strength at temperatures up to 1800 deg. F. It is the cast modification of wrought HAYNES Alloy No. 25 and has been used successfully in jet engine blading and nozzle vanes. This datasheet provides information on composition, physical properties, 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 heat treating, machining, and joining. Filing Code: Co-17. Producer or source: Haynes Stellite Company.
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Publisher: Journals Gateway
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
Publisher: Journals Gateway
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...
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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 properties, hardness, elasticity, tensile properties, and compressive strength 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: SS-200. Producer or source: Alloy steel mills and foundries.
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Publisher: Journals Gateway
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...
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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 properties, hardness, elasticity, and tensile properties as well as creep, and deformation. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-222. Producer or source: Alloy steel mills and foundries.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1960) 9 (2): TS-90.
Published: 01 February 1960
... a temperature above 700°F. Cool slowly in furnace or insulating material. Parts should be given a fuh anneal afta welding. General Characteristics: JET FORGE is a chromium, molybdenum, vanadium 9 pe hot work tool steed particukuly adapted for the orgiog of jet engine blades and otha high temperature and high...
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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.
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Publisher: Journals Gateway
Alloy Digest (2011) 60 (2): Co-121.
Published: 01 February 2011
... Jet Kote 117 is a premium quality tungsten carbide/cobalt powder for the deposition of high quality HVOF coatings. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion and wear resistance as well as surface treatment...
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Jet Kote 117 is a premium quality tungsten carbide/cobalt powder for the deposition of high quality HVOF coatings. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion and wear resistance as well as surface treatment and powder metal forms.Filing Code: Co-121. Producer or source: Stellite Coatings and Deloro Stellite.
Journal Articles
Publisher: Journals Gateway
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...
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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.
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Publisher: Journals Gateway
Alloy Digest (1977) 26 (6): SS-340.
Published: 01 June 1977
... that must provide maximum strength and corrosion resistance at temperatures up to 13000F (704OC). It is used in jet engines and superchargers for various high-temperature applications such as turbine wheels and blades. frames, casings, afterburner parts and bolts. Forms Available: Billets, hot-rolled...
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PYROMET A-286 is an age-hardenable austenitic iron-nickel-chromium alloy designed for service up to 1300 F (704 C) on jobs requiring high strength and good corrosion resistance at the operating temperature. It offers high ductility in notched sections. Pyromet A-286 is used in jet engines and superchargers for various high-temperature components. This datasheet provides information on composition, physical properties, 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, and joining. Filing Code: SS-340. Producer or source: Carpenter.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1964) 13 (11): Ni-95.
Published: 01 November 1964
...-induction melted nickel-base superalloy recommended for increased operating temperatures for jet engine forged blading and turbine discs and rings. It is a precipitation hardenable alloy. It has superior forgeability, and stress-rupture proper ties applicable for use in gas-turbine buckets operating...
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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. 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, joining, and surface treatment. Filing Code: Ni-95. Producer or source: Special Metals Inc..
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Alloy Digest (1994) 43 (11): Ni-469.
Published: 01 November 1994
... be conducted in many cases. General Characteristics Nicrobraz 150 offers strength at elevated temperatures and resistance to oxidation similar to that offered by Nicrobraz 125 (see Alloy Digest Ni-462), but it is formu- lated to permit the use of thinner base metal sections in the design of turbine blades, jet...
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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.
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Publisher: Journals Gateway
Alloy Digest (1994) 43 (6): Ni-455.
Published: 01 June 1994
... is excellent. Nicrobraz 125 is widely used for joining turbine blades, jet engine parts, and highly stressed sheet metal struc- tures, as well as assemblies subject primarily to corro sive conditions. Recommended Uses: Excellent for a wide variety of high-temperature service uses because of superior high...
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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
Publisher: Journals Gateway
Alloy Digest (1964) 13 (2): SS-152.
Published: 01 February 1964
... strength at temperatures up co and including 1100oF. Fom s Available: Billets, hot rolled and cold finished bars, wire, cold rolled strip, and special shapes. Applications: Jet engine and steam turbine components, aircraft structural parts. Turbine blades, wheels, discs and turbine shafts. Manufacturer...
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Pyromet X-12 is a martensitic stainless steel offering high strength at both room temperature and high heat. It is recommended for use in jet engines, steam turbines and aircraft 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 high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SS-152. Producer or source: Carpenter.
Journal Articles
Publisher: Journals Gateway
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.