Search Results for Nickel-Titanium alloys

BERYLCO NICKEL ALLOY 440 is an age-hardenable nickel-beryllium-titanium alloy that offers high strength, excellent spring properties outstanding formability, good high-temperature mechanical properties, and resistance to corrosion and fatigue. Complex shapes can be produced in the solution-treated (soft) condition and then aged to a minimum tensile strength of 215,500 psi. It is used for mechanical and electrical/electronic components in the temperature range -320 to 800 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. 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-94. Producer or source: Kawecki Berylco Industries Inc.. Originally published September 1964, revised September 1975.

Superelastic and high-temperature superelastic alloys are binary nickel-titanium alloys better known as shape memory or Nitinol alloys. This is the first of several data sheets that cover these materials; this data sheet covers materials with an austenite start temperature of 10 deg C (14 deg F). This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming and machining. Filing Code: Ni-643. Producer or source: Special Metals, Shape Memory Alloy Division.

Body-Temperature Ni-Ti alloys are binary nickel-titanium alloys better known as shape memory or nitinol alloys. This is the second of several data sheets that cover these materials by austenite start temperature. This data sheet covers materials with an austenite start temperature of approximately 15 ± 5 deg C (59 ± 9 deg F). This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming and machining. Filing Code: Ni-654. Producer or source: Special Metals, Shape Memory Alloy Division.

Austral Wright Titanium Grade 12 (UNS R53400) is a titanium alloy that contains small additions of nickel and molybdenum. It is considerably superior to unalloyed titanium in several aspects, and is characterized by high strength, good ductility, and outstanding corrosion resistance. Austral Wright Titanium Grade 12 is used in mildly reducing conditions, or where conditions vary from oxidizing to reducing. It is particularly resistant to crevice corrosion in hot brines. AS 1210, and ASME Boiler and Pressure Vessel Code pre-qualify Austral Wright Titanium Grade 12 for use in pressure vessels up to 300 ºC (572 ºF). 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: Ti-187. Producer or source: Austral Wright Metals.

TiCode-12 is a titanium-base alloy developed for corrosion-resisting applications. It contains nominally 0.8% nickel and 0.3% molybdenum; these additions affect corrosion resistance profoundly. They also provide an added benefit by significantly strengthening the titanium through the introduction of a small amount of beta phase into the structure and through solution effects. TiCode-12 has many applications in the process industries where its excellent corrosion resistance is needed. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-71. Producer or source: Titanium Metals Corporation of America.

Armco 321 is an austenitic nickel-stainless-steel with the carbon stabilized by titanium for welding and elevated temperature service. It is useful when the weldment is not annealed after welding. This alloy is nonmagnetic when annealed but is slightly magnetic when cold worked. It has excellent resistance to corrosion and oxidation, possesses high creep strength, and may be used at temperatures up to 871 C (1600 F). Titanium is added to this alloy to impart substantial immunity to intergranular corrosion. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-810. Producer or source: AK Steel Inc.

ALLEGHENY LUDLUM AL 29-4-2 alloy is a high-purity ferritic stainless steel designated to provide superior resistance to corrosion by aggressive environments. It also offers fabrication characteristics that (along with E-BRITE Alloy) are unique among highly alloyed ferritic materials. The combination of properties available in AL 29-4-2 alloy makes it an attractive, cost-effective alternative to titanium, high-nickel and nickel-base alloys for many harsh environments. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-480. Producer or source: Allegheny Ludlum Corporation.

ATI X-751 is a high-aluminum version of ATI X-750. It is a high-strength, precipitation hardenable, nickel-chromium alloy that employs nickel and titanium as the hardening elements. The alloy has good creep-rupture strength up to 815 °C (1500 °F), and excellent oxidation and corrosion resistance up to 980 °C (1800 °F). This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-776. Producer or source: ATI.

AISI No. 664 is a nickel-base high-temperature alloy that can be precipitation hardened because of its contents of aluminum and titanium. Vacuum melting is used in its production to provide excellent quality and reproducability. It is used for applications requiring a good combination of creep and stress-rupture properties up to about 1500 F. Typical applications are gas-turbine components, airframes and fasteners. 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-269. Producer or source: Nickel alloy producers.

TECHALLOY Nickel 205 is a wrought nickel-base alloy containing small additions of magnesium and titanium. It has a high Curie temperature and a high magnetostriction coefficient. It is used for many electrical and electronic components and for equipment employing magnetostrictive effects. 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: Ni-247. Producer or source: Techalloy Company Inc..

Nickel 230 is designed for use in active cathodes. The closely controlled composition of this material makes it useful for certain special electron-tube applications. Nickel 230 is essentially free from titanium. 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: Ni-256. Producer or source: Huntington Alloys Inc..

UNS No. N02230 was designed for use in active cathodes. It is essentially free from titanium. Its closely controlled composition makes it useful for certain special electron-tube applications. 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: Ni-346. Producer or source: Nickel and nickel alloy producers.

Langalloy K-500 is a nickel-copper alloy with both aluminum and titanium additions for age hardening. The additions give the alloy high strength and hardness. The alloy has excellent corrosion resistance along with resistance to chloride stress corrosion, high fatigue resistance in sea water, and good resistance to impingement attack. The alloying additions give it a low magnetic permeability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming and machining. Filing Code: Ni-653. Producer or source: Langley Alloys.

ASTM B 752 Grade 705C zirconium casting alloy is basically identical in composition and similar in properties to its wrought equivalent, UNS R60705, which is grade 705. Zirconium alloys are expensive, but are more corrosion resistant than stainless steels, nickel alloys, and titanium. The largest application for zirconium alloys is in the handling of hydrochloric acid. Grade 705C is one of the common casting grades. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: ZR-12. Producer or source: ATI Wah Chang, Allegheny Technologies.

Carlson alloy C825 is a wrought nickel-iron-chromium alloy with additions of molybdenum, copper, and titanium. It was developed to handle both reducing and oxidizing media. The alloy is resistant to chloride-ion stress-corrosion cracking, to pitting and crevice attack and many corrosive solutions. 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: Ni-419. Producer or source: G.O. Carlson Inc..

Nimonic alloy 901 is a nickel-base alloy strengthened by additions of molybdenum, titanium, and aluminum. It possesses high creep and rupture strength from 1000 to 1400 deg F. Applications include components for gas turbines, bolting, and valve stems for power applications. 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 as well as heat treating. Filing Code: Ni-339. Producer or source: Inco Alloys International Inc. Originally published September 1986, revised April 1996.

Nickelvac K-500 is a nickel-copper alloy with age-hardening properties imparted by alloying additions of aluminum and titanium. The alloy is characterized by excellent corrosion resistance in an extensive range of natural and chemical environments, excellent resistance to chloride-ion stress-corrosion cracking, and very high strength and hardness. 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 joining. Filing Code: Ni-595. Producer or source: Allvac Metals Company.

INCOLOY alloy 825 is a nickel-chromium-iron alloy with additions of molybdenum, copper, and titanium. It is resistant to chloride-ion stress-corrosion cracking, to pitting and crevice attack, and to corrosion in both oxidizing and reducing media. This datasheet provides information on composition, physical properties, 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: Ni-109. Producer or source: Inco Alloys International Inc.. Originally published December 1965, revised June 1988.

CABOT COLUMBIUM (NIOBIUM) finds one of its major uses as an alloy of Columbium 1% Zirconium for sodium lamp applications. Other uses include Nickel and Ferro Columbium as an alloy additive for the super alloy industry and as Columbium Titanium for superconducting applications. 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 joining. Filing Code: Cb-23. Producer or source: Cabot Corporation.

NIMONIC ALLOY 105 is a wrought nickel-cobalt-chromium-base alloy strengthened by additions of molybdenum, aluminum and titanium. It has been developed for service up to 950 C (1742 F). This datasheet provides information on composition, physical properties, and elasticity 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-66. Producer or source: Inco Alloys International Inc.. Originally published August 1961, revised May 1991.