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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, <span class="search-highlight">UDIMET</span> <span class="search-highlight">B</span>: Ultra High-Strength Steel
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for article titled, <span class="search-highlight">UDIMET</span> <span class="search-highlight">B</span>: 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 (2004) 53 (4): Ni-620.
Published: 01 April 2004
... 86 317 46 131 19 476 69 221 32 83 12 Alloy 713C Cast 566 82 297 43 145 21 448 65 207 30 90 13 Udimet 500 Cast 448 65 228 33 90 13 345 50 166 24 Table 2 Aged Charpy V-Notch Comparison Impact toughness(a) Alloy Form J ft lbf Udimet 720 Wrought 19(b) 14(b) Udimet 520 Wrought 16 12 Udimet 710...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> 720: Age-Hardening Nickel Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 720: Age-Hardening Nickel Alloy
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 (1987) 36 (1): Ni-51.
Published: 01 January 1987
...< for Udlmet 00 ib i&75-X5O F. Llechanica! bork:ng a: :cmpe:atures above this rangc zunli! uill cause surface cracking. while forging below about 1875°F allI introduce cold uork into the alloy. Care must be taken that the material IS well soaked on reheating between forging operations. Weldability: Udimet 700 usually applications. is not welded in aircraft or other critical (b) 2 lb. caustic soda and I I 2 lb. potassium permanganate gallon of uater. LOSSat hot as po,Gble. lmmcrse ior up IO 8 hour>. An! residue1 be removed b) lmmcrslon III IOr; julphuric acid. per can General Characteristics: Udimet 700 iJ a hIghI> elevated-temperature-tensile has rupcr creep reswancc. resistance. allobed nvzkel-bass alloy suhlhlting high and itrc>s-rupture ,trengrh. Thor allo! high latlgwslrsngth.and high oslddrlon Forms...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> 700: High Temperature Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 700: High Temperature Alloy
UDIMET 700 is a wrought nickel-base alloy produced by vacuum-induction melting and further refined by vacuum-arc remelting. It has excellent mechanical properties at high temperatures. Among its applications are blades for aircraft, marine and land-based gas turbines and rotor discs. This datasheet provides information on composition, physical properties, 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-51. Producer or source: Special Metals Corporation. Originally published March 1959, revised January 1987.
Journal Articles
Alloy Digest (1978) 27 (11): Ni-258.
Published: 01 November 1978
... UDIMET 718 is a nickel-base alloy that is precipitation hardenable. It exhibits exceptionally high yield strength up to 1300 F, excellent cryogenic properties down to -423 F and superior weldability even in the fully-aged condition. This unusual combination of characteristics makes it suitable...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> 718: Precipitation Hardening High-Temperature Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 718: Precipitation Hardening High-Temperature Alloy
UDIMET 718 is a nickel-base alloy that is precipitation hardenable. It exhibits exceptionally high yield strength up to 1300 F, excellent cryogenic properties down to -423 F and superior weldability even in the fully-aged condition. This unusual combination of characteristics makes it suitable for elevated-temperature applications in gas turbines and in critical components for missiles. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-258. Producer or source: Special Metals Corporation.
Journal Articles
Alloy Digest (1978) 27 (9): Ni-257.
Published: 01 September 1978
... UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. This datasheet...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> WASPALOY: High Temperature Superalloy
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for article titled, <span class="search-highlight">UDIMET</span> WASPALOY: High Temperature Superalloy
UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. 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, joining, and surface treatment. Filing Code: Ni-257. Producer or source: Special Metals Corporation.
Journal Articles
Alloy Digest (1964) 13 (6): Ni-92.
Published: 01 June 1964
... UDIMET 41 is a vacuum induction melted precipitation hardening nickel-base alloy having outstanding room and elevated temperature properties. It possesses excellent corrosion and oxidation resistance. It is designed for highly stressed components operating in the 1400-1700 deg F temperature range...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> 41: Heat and Corrosion Resisting Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 41: Heat and Corrosion Resisting Alloy
UDIMET 41 is a vacuum induction melted precipitation hardening nickel-base alloy having outstanding room and elevated temperature properties. It possesses excellent corrosion and oxidation resistance. It is designed for highly stressed components operating in the 1400-1700 deg 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 low and high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-92. Producer or source: Special Metals Inc..
Journal Articles
Alloy Digest (1961) 10 (12): Ni-28.
Published: 01 December 1961
... International® 1996 Heat Treatmentt The nod heat ueameot to produce maximum high tem- perature properties in for F Udimet 500 wnsits of a solutioo tmrmenc and a ouble aging as follows: 1975°F. 4hoIushc. 155OOF. 14OOOF. :dzkE as heattreaad is 38-40 Rockwell C be used in the barsto& form with no so b % ueor...
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View articletitled, <span class="search-highlight">UDIMET</span> 500: Heat Resistant Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 500: Heat Resistant Alloy
UDIMET is a nickel base alloy recommended for applications where high strength at elevated temperatures is required. This datasheet provides information on composition and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-28. Producer or source: Special Metals Inc.. Originally published October 1956, revised December 1961.
Journal Articles
Alloy Digest (1995) 44 (3): Ni-479.
Published: 01 March 1995
... resistivity Enthalpy Specific heat Coefficient, thermal expansion PROPERTIES Table 1 -THERMAL EXPANSION COEFFICIENT Comparison to other common high-temperature superalloys (in/mPF x l@) 70- 800°F 70-1000°F 70-12OO F 70-1300°F AEREX350 MP159 Waspaloy Udimet 720 7.5 8.09 7.6 7.67 7.7 8.29 7.8 7.88 8.0 8.39 8.0...
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View articletitled, AEREX 350: High Temperature Alloy
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for article titled, AEREX 350: High Temperature Alloy
AEREX 350 is a bolt alloy with a combination high temperature creep strength, notch toughness, and thermal stability. It was designed for aerospace bolting applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance. Filing Code: Ni-479. Producer or source: SPS Technologies.
Journal Articles
Alloy Digest (1963) 12 (6): Ni-44.
Published: 01 June 1963
... UDIMET 600 is a vacuum-induction melted nickel-base alloy having excellent mechanical properties at high temperatures. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as forming, heat...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> 600: High Temperature Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 600: High Temperature Alloy
UDIMET 600 is a vacuum-induction melted nickel-base alloy having excellent mechanical properties at high temperatures. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-44. Producer or source: Kelsey-Hayes Company. Originally published October 1958, revised June 1963.
Journal Articles
Alloy Digest (1972) 21 (7): Ni-175.
Published: 01 July 1972
...-resistant alloys creep properties elasticity heat treatability high-temperature alloys joinability machinability physical properties tensile properties UDIMET 105 workability Filing Code: Ni-175 UDIMET 105 Nickel Alloy JULY 1972 - DATA ON WORLD WIDE METALS AND ALLOYS Psblisbd b Enghering Alloys...
Abstract
View articletitled, <span class="search-highlight">UDIMET</span> 105: High Temperature Alloy
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for article titled, <span class="search-highlight">UDIMET</span> 105: High Temperature Alloy
UDIMET 105 is a nickel-base alloy which was developed for service at elevated temperatures. This datasheet provides information on composition, physical properties, 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-175. Producer or source: Special Metals Corporation.
Journal Articles
Alloy Digest (2020) 69 (5): Co-131.
Published: 01 May 2020
... W/(m K) (Btu/(h·ft·°F)) 9.4 (5.4) Specific heat capacity J/(kg K) (cal/(g °C)) 21 °C (70 °F) 385 (0.092) Electrical resistivity m circular-mil/ft) 24 °C (75 °F) 0.886 (533.2) Magnetic permeability(b) 1.002 Typical values. RT = room temperature. (a) Source: ATI. (b) At 200 Oersteds (15.9 kA/m...
Abstract
View articletitled, UPM COBALT ALLOY L605 (UNS R30605): Co-20Cr-15W-10Ni Alloy
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for article titled, UPM COBALT ALLOY L605 (UNS R30605): Co-20Cr-15W-10Ni Alloy
UPM Cobalt Alloy L605 (UNS R30605) is a solid-solution-strengthened, cobalt-20chromium-15tungsten-10nickel alloy. This corrosion- and heat-resistant alloy is typically used for intermittent service up to 870 °C (1600 °F), and for continuous service up to 1095 °C (2000 °F), but usage is not limited to such applications. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming and heat treating. Filing Code: Co-131. Producer or source: United Performance Metals.