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Journal Articles
Alloy Digest (2004) 53 (7): Al-391.
Published: 01 July 2004
... Originally developed as a high-strength alloy for the aircraft industry, this alloy was further developed and optimized to satisfy the most demanding applications of the mold construction industry. The resulting mold construction alloy, Hokotol, exhibits very high strength and wear resistance...
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View articletitled, HOKOTOL: High-Strength Aluminum Alloy
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for article titled, HOKOTOL: High-Strength Aluminum Alloy
Originally developed as a high-strength alloy for the aircraft industry, this alloy was further developed and optimized to satisfy the most demanding applications of the mold construction industry. The resulting mold construction alloy, Hokotol, exhibits very high strength and wear resistance, as well as excellent uniformity of strength properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance. Filing Code: AL-391. Producer or source: Corus Aluminum Rolled Products USA.
Journal Articles
Alloy Digest (2008) 57 (5): Al-413.
Published: 01 May 2008
... Kaiser aluminum alloy 2124 is a high-purity version of 2024 with tighter controls on the iron and silicon for an increase in strength and toughness. It is primarily used as plate in the aircraft industry. This data sheet applies to sheet, coil, and plate in the T851 temper. This datasheet provides...
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View articletitled, KAISER ALUMINUM ALLOY 2124: Aluminum Aerospace Alloy
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for article titled, KAISER ALUMINUM ALLOY 2124: Aluminum Aerospace Alloy
Kaiser aluminum alloy 2124 is a high-purity version of 2024 with tighter controls on the iron and silicon for an increase in strength and toughness. It is primarily used as plate in the aircraft industry. This data sheet applies to sheet, coil, and plate in the T851 temper. 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: AL-413. Producer or source: Tennalum, A Division of Kaiser Aluminum.
Journal Articles
Alloy Digest (1971) 20 (12): Cu-246.
Published: 01 December 1971
... COMPO H is an oil-impregnated sintered bronze, produced by powder metallurgy techniques, which is widely used in automotive, applicance, farm equipment, and aircraft industry applications. This datasheet provides information on composition, physical properties, tensile properties, and compressive...
Abstract
View articletitled, COMPO H: Self Lubricated Bearing Alloy
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for article titled, COMPO H: Self Lubricated Bearing Alloy
COMPO H is an oil-impregnated sintered bronze, produced by powder metallurgy techniques, which is widely used in automotive, applicance, farm equipment, and aircraft industry applications. This datasheet provides information on composition, physical properties, tensile properties, and compressive strength. and bearing strength It also includes information on corrosion resistance Filing Code: Cu-246. Producer or source: Bound Brook Bearing Corporation of America.
Journal Articles
Alloy Digest (2007) 56 (5): Ni-650.
Published: 01 May 2007
... Boehler L311 VMR is a nickel alloy having high creep and rupture strength up to 760 deg C (1400 deg F) and scaling resistance in air to 850 deg C (1560 deg F). It is used in the aircraft and gas turbine industries as shafts, blades, and discs. This datasheet provides information on composition...
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View articletitled, BOEHLER L311 VMR: Age-Hardening Nickel Alloy
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for article titled, BOEHLER L311 VMR: Age-Hardening Nickel Alloy
Boehler L311 VMR is a nickel alloy having high creep and rupture strength up to 760 deg C (1400 deg F) and scaling resistance in air to 850 deg C (1560 deg F). It is used in the aircraft and gas turbine industries as shafts, blades, and discs. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-650. Producer or source: Böhler-Uddeholm Specialty Metals Inc.
Journal Articles
Alloy Digest (1963) 12 (5): SA-146.
Published: 01 May 1963
... Udimet B is a series of four 18%-nickel steels of ultra high strength and good toughness at room and at elevated temperatures. They are easily fabricated and weldable, and are recommended for the aircraft and missile industries for high temperature components. This datasheet provides information...
Abstract
View articletitled, UDIMET B: Ultra High-Strength Steel
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for article titled, UDIMET B: Ultra High-Strength Steel
Udimet B is a series of four 18%-nickel steels of ultra high strength and good toughness at room and at elevated temperatures. They are easily fabricated and weldable, and are recommended for the aircraft and missile industries for high temperature components. 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, joining, and surface treatment. Filing Code: SA-146. Producer or source: Special Metals.
Journal Articles
Alloy Digest (1962) 11 (12): Ni-77.
Published: 01 December 1962
... RAonel 600 is a corrosion and heat resisting nickel-base alloy having a combination of high strength and oxidation resistance along with hot and cold workability. It is recommended for component parts in the aircraft, chemical, petroleum and paper pulp industries. This datasheet provides...
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View articletitled, RAONEL 600: Heat Resisting Alloy
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for article titled, RAONEL 600: Heat Resisting Alloy
RAonel 600 is a corrosion and heat resisting nickel-base alloy having a combination of high strength and oxidation resistance along with hot and cold workability. It is recommended for component parts in the aircraft, chemical, petroleum and paper pulp industries. 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-77. Producer or source: Rolled Alloys Inc..
Journal Articles
Alloy Digest (1982) 31 (6): SS-410.
Published: 01 June 1982
... for highly stressed components in the 1800-2000 F temperature range. It is used in the aircraft, automotive, petroleum, petrochemical and power industries for a wide range of components and parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile...
Abstract
View articletitled, ACI TYPE HN: Heat Resistant Cast Stainless Steel
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for article titled, ACI TYPE HN: Heat Resistant Cast Stainless Steel
Type HN is an iron-chromium-nickel alloy containing sufficient chromium for good high-temperature corrosion resistance and with nickel content in excess of the chromium. This alloy has properties somewhat similar to the more widely used ACI Type HT alloy but with better ductility. Type HN is used for highly stressed components in the 1800-2000 F temperature range. It is used in the aircraft, automotive, petroleum, petrochemical and power industries for a wide range of components and parts. 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 casting, heat treating, machining, and joining. Filing Code: SS-410. Producer or source: Various stainless steel casting companies.
Journal Articles
Alloy Digest (2008) 57 (6): Al-414.
Published: 01 June 2008
... Kaiser Aluminum alloy 7175/7475 is a high-purity version of 7075 and is heavily used by the aircraft and ordinance industries because of its superior strength. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information...
Abstract
View articletitled, KAISER ALUMINUM ALLOY 7175/7475: Aluminum Aerospace Alloy
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for article titled, KAISER ALUMINUM ALLOY 7175/7475: Aluminum Aerospace Alloy
Kaiser Aluminum alloy 7175/7475 is a high-purity version of 7075 and is heavily used by the aircraft and ordinance industries because of its superior strength. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming and heat treating. Filing Code: AL-414. Producer or source: Tennalum, A Division of Kaiser Aluminum.
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...
Abstract
View articletitled, INCOLOY 901: High Temperature Alloy
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for article titled, INCOLOY 901: High Temperature Alloy
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 includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-38. Producer or source: The International Nickel Company Inc..
Journal Articles
Alloy Digest (1979) 28 (10): Ti-73.
Published: 01 October 1979
.... It has a guaranteed minimum yield strength of 70,000 psi with good ductility and formability. It has excellent resistance to corrosion by marine atmospheres and seawater. It is used ln the aircraft, marine and chemical process@ industries. l RMI is a registered trademark of the RMI Company. Composition...
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View articletitled, RMI 70: Commercially Pure Titanium
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for article titled, RMI 70: Commercially Pure Titanium
RMI 70 is the highest strength grade of commercially pure unalloyed titanium. It has a guaranteed minimum yield strength of 70,000 psi with good ductility and formability. It has excellent resistance to corrosion by marine atmospheres and seawater. It is used in the aircraft, marine and chemical processing industries. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and surface treatment. Filing Code: Ti-73. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1982) 31 (1): Bi-27.
Published: 01 January 1982
... characteristics make it of great use in industry for such applications as sprinkler and fire safety devices, support for bending pipe and tubing, anchoring aircraft parts for machining, and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical properties...
Abstract
View articletitled, INDALLOY 158: Low Melting Controlled Shrinkage Alloy
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for article titled, INDALLOY 158: Low Melting Controlled Shrinkage Alloy
INDALLOY 158 is a bismuth-base, eutectic alloy that has a melting point of 158 F (70 C). It is 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 low melting temperature and controlled-shrinkage characteristics make it of great use in industry for such applications as sprinkler and fire safety devices, support for bending pipe and tubing, anchoring aircraft parts for machining, 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, heat treating, and machining. Filing Code: Bi-27. Producer or source: Indium Corporation of America.
Journal Articles
Alloy Digest (1982) 31 (4): SS-405.
Published: 01 April 1982
.... Filing Code: SS-405. Producer or source: Crucible Specialty Metals Division, Colt Industries. Producer or Source: Crucible Specialty Metals Division, Colt Industries Copyright © ASM International® 1996 1996 ASM International aircraft heaters chemical composition creep properties CRUCIBLE...
Abstract
View articletitled, CRUCIBLE 309: Austenitic Stainless Steel
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for article titled, CRUCIBLE 309: Austenitic Stainless Steel
CRUCIBLE 309 is a non-hardenable austenitic chromium-nickel steel that has high heat-resisting characteristics. In the annealed condition it is non-magnetic or magnetic, depending on the composition. When cold worked it is very slightly magnetic. Typical applications include aircraft heaters and sulfite liquor handling equipment. 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 heat treating, machining, and joining. Filing Code: SS-405. Producer or source: Crucible Specialty Metals Division, Colt Industries.
Journal Articles
Alloy Digest (1983) 32 (5): SS-426.
Published: 01 May 1983
... worked. Among its many applications are aircraft-engine exhaust manifolds, furnace parts and expansion joints. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information...
Abstract
View articletitled, CRUCIBLE 321: Austenitic Stainless Steel
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for article titled, CRUCIBLE 321: Austenitic Stainless Steel
CRUCIBLE 321 is a non-hardenable austenitic chromium-nickel steel which is particularly adaptable for parts fabricated by welding without postweld annealing for use at temperatures between 800 and 1500 F. This grade is non-magnetic in the annealed condition but is slightly magnetic when cold worked. Among its many applications are aircraft-engine exhaust manifolds, furnace parts and expansion joints. 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, and joining. Filing Code: SS-426. Producer or source: Crucible Specialty Metals Division, Colt Industries.
Journal Articles
Alloy Digest (1983) 32 (10): Bi-32.
Published: 01 October 1983
...-shrinkage characteristics make it of great use in industry for such applications as sprinkler and fire safety devices, support for bending pipe and tubing, anchoring aircraft parts for machining, and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical...
Abstract
View articletitled, BISMUTH-26.7Pb-13.3Sn-10Cd: Low Melting Controlled Shrinkage Alloy
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for article titled, BISMUTH-26.7Pb-13.3Sn-10Cd: Low Melting Controlled Shrinkage Alloy
Bismuth-26.7Pb-13.3Sn-10Cd is a bismuth-base, eutectic alloy that is melted and cast easily and is ready for use as soon as it freezes. It has a melting point of 158 F (70 C). It can be recovered easily and recycled into new uses any number of times. Its low melting temperature and controlled-shrinkage characteristics make it of great use in industry for such applications as sprinkler and fire safety devices, support for bending pipe and tubing, anchoring aircraft parts for machining, 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-32. Producer or source: Producers of low-melting alloys.
Journal Articles
Alloy Digest (1983) 32 (12): SS-436.
Published: 01 December 1983
... CRUCIBLE F347 is a non-hardenable austenitic chromium-nickel steel that is particularly adaptable for use at temperatures between 800 and 1650 F. It is non-magnetic in the annealed condition but is slightly magnetic in the cold-worked condition. Among its many applications are aircraft-engine...
Abstract
View articletitled, CRUCIBLE 347: Austenitic Stainless Steel
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for article titled, CRUCIBLE 347: Austenitic Stainless Steel
CRUCIBLE F347 is a non-hardenable austenitic chromium-nickel steel that is particularly adaptable for use at temperatures between 800 and 1650 F. It is non-magnetic in the annealed condition but is slightly magnetic in the cold-worked condition. Among its many applications are aircraft-engine exhaust manifolds, boiler shells and high-temperature handling equipment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-436. Producer or source: Crucible Specialty Metals Division, Colt Industries.
Journal Articles
Alloy Digest (1984) 33 (2): SS-440.
Published: 01 February 1984
... include aircraft structural members and equipment for the process industries. 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, joining...
Abstract
View articletitled, JESSOP JS17Cr-7Ni: Precipitation Hardenable Stainless Steel
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for article titled, JESSOP JS17Cr-7Ni: Precipitation Hardenable Stainless Steel
JESSOP JS17Cr-7Ni is a semi-austenitic precipitation-hardening steel. Its composition gives it a unique and attractive combination of corrosion resistance, cold formability, high strength and hardness, excellent fatigue properties and minimum distortion upon heat treatment. Typical applications include aircraft structural members and equipment for the process industries. 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, joining, and surface treatment. Filing Code: SS-440. Producer or source: Jessop Steel Company.
Journal Articles
Alloy Digest (1967) 16 (11): Co-54.
Published: 01 November 1967
... MAR-M Alloy 509 is a vacuum melted, cobalt-base alloy having high strength, low creep rates, and resistance to oxidation and thermal shock. It is recommended for aircraft and industrial gas turbine applications. This datasheet provides information on composition, physical properties, hardness...
Abstract
View articletitled, MAR-M Alloy 509: High Temperature Alloy
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for article titled, MAR-M Alloy 509: High Temperature Alloy
MAR-M Alloy 509 is a vacuum melted, cobalt-base alloy having high strength, low creep rates, and resistance to oxidation and thermal shock. It is recommended for aircraft and industrial gas turbine applications. 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 casting, heat treating, machining, and joining. Filing Code: Co-54. Producer or source: Martin Metals Division, Martin Marietta Corporation.
Journal Articles
Alloy Digest (1970) 19 (2): SS-234.
Published: 01 February 1970
... ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet...
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View articletitled, ALLEGHENY ALMAR-362: Age-Hardenable Stainless Steel
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for article titled, ALLEGHENY ALMAR-362: Age-Hardenable Stainless Steel
ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-234. Producer or source: Allegheny Ludlum Corporation.
Journal Articles
Alloy Digest (1965) 14 (12): Ni-108.
Published: 01 December 1965
... Sanicro 71 is a nickel-base alloy having good resistance to stress-corrosion, oxidation and creep at elevated temperatures. It is recommended for nuclear power reactor heat exchanger tubes, aircraft turbojet engines and for equipment in the textile, plastic, and chemical industries. This datasheet...
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View articletitled, SANICRO 71: Heat and Corrosion Resisting Alloy
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for article titled, SANICRO 71: Heat and Corrosion Resisting Alloy
Sanicro 71 is a nickel-base alloy having good resistance to stress-corrosion, oxidation and creep at elevated temperatures. It is recommended for nuclear power reactor heat exchanger tubes, aircraft turbojet engines and for equipment in the textile, plastic, and chemical industries. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. 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-108. Producer or source: Sandvik.
Journal Articles
Alloy Digest (2011) 60 (1): Cu-795.
Published: 01 January 2011
... requirements of the aircraft industry for an alloy having increased physical properties, hardness, and sufficient elongation to withstand important impacts and loads. It is recommended for use as bushings, bearings liners, inserts, piston parts, nuts, and slides, etc. Table 1 Mechanical properties Property...
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View articletitled, AMPCO 18.22 and 18.136: Copper Casting Alloy
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for article titled, AMPCO 18.22 and 18.136: Copper Casting Alloy
AMPCO 18.22 and 18.136 are variations of AMPCO 18 to produce a higher ultimate strength and to improve the impact resistance, respectively. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness and fatigue. It also includes information on casting. Filing Code: Cu-795. Producer or source: AMPCO Engineered Alloys.
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