Search Results for aerospace industry

VascoJet 2000 was developed to meet the needs of the aerospace industry. It also has been used for special tooling applications. It is a vacuum-melted modification of AISI H12 hot-work die steel. VascoJet 2000 has a tensile strength of 200,000 psi (1500 MPa) at room temperature and exceptional toughness. It is used for gears and shafts in helicopter and other aerospace applications. 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: TS-425. Producer or source: Teledyne Vasco.

ATI 425 was originally developed for hot-rolled armor plate to provide ballistic protection comparable to Ti-6Al-4V and has been evaluated against a variety of projectile threats for use as armor. While processing the alloy for armor plate applications, it was observed that the material exhibited very good hot workability, permitting a more lenient window of processing parameters than necessary for Ti-6Al-4V. Versatility then expanded, and applications now exist in the chemical process industry (CPI) and in the aerospace industry. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance. Filing Code: TI-133. Producer or source: ATI Wah Chang, Allegheny Technologies. Originally published March 2004, revised July 2004.

Zapp TiAl6V4 is an alpha-beta titanium alloy that is used in the annealed or solution heat treated and aged condition for applications requiring high strength, relatively low weight, and excellent corrosion resistance. It is typically used in the low to moderate temperature range (up to about 400 °C, or 750 °F). Ti-6Al-4V is the most widely used titanium alloy, accounting for more than 50% of the total titanium used. The aerospace industry accounts for more than 80% of this usage. 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-173. Producer or source: Zapp AG.

NeoNickel L605/25 is a solid-solution strengthened cobalt-chromium-tungsten-nickel alloy that combines excellent high temperature strength with good oxidation resistance up to 980 °C (1800 °F). It is most commonly used in the aerospace industry due to its strength and durability in high temperature environments. It is also used for the manufacture of surgical implants. 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: Co-141. Producer or source: NeoNickel.

TIMETAL 10-2-3 is a high fracture toughness titanium-base alloy. It is metallurgically near-beta and is capable of attaining a wide variety of strength levels, depending uopn the selection of heat treatment. Major advantages of this alloy are: (1) Its excellent forgeability, (2) Its high toughness in air and salt-water environments and (3) Its high hardenability which provides good properties in sections up to five inches thick. It is used in the aerospace industry for applications up to 600 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength 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: Ti-80. Producer or source: Titanium Metals Corporation (Timet). Originally published as Ti-10V-2Fe-3Al, December 1980, revised October 1992.

Nicrofer 7520 is a high temperature creep resistant nickel-base alloy with good scaling resistance to 2000 deg F (1100 deg C). Many applications are in the aerospace industry. The alloy is sometimes called alloy 75. 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: Ni-496. Producer or source: VDM Technologies Corporation.

HAYNES X-750 alloy is an age-hardening nickel-base alloy with good strength to 649 C (1200 F). The alloy shows good oxidation resistance and has important applications in the aerospace industry. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ni-553. Producer or source: Haynes International Inc. Originally published June 1999, corrected July 1999.

TIMETAL 834 is a Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C alloy with high strength and creep resistance up to 593 C (1100 F). The alloy is workable and weldable. It is used in the aerospace industry for rings and compressor disks. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as heat treating. Filing Code: TI-116. Producer or source: Timet.

Allvac Ti-15Mo is a metastable beta alloy melted in a vacuum arc remelting (VAR) furnace to minimize segregation. The alloy has a unique combination of properties and is used in the medical, chemical, and aerospace industries. This datasheet provides information on composition. Filing Code: TI-136. Producer or source: Allvac, an Allegheny Technologies Company.

Timetal 685 is a titanium alloy with 6 Al, 5 Zr, 0.5 Mo, and 0.25 Si. It is a near-alpha alloy with high strength and creep resistance. Applications are in the aerospace industry. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness and creep. It also includes information on forming, heat treating, and joining. Filing Code: TI-142. Producer or source: Timet.

Boehler L080A is a nickel-base alloy with good creep resistance to 805 deg C (1480 deg F). The alloy has excellent oxidation resistance. It is used in the aerospace industry. 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, and machining. Filing Code: Ni-656. Producer or source: Böhler-Uddeholm North America.

Crucible 422 has a structure of tempered martensite to give the alloy high strength. It is useful in the aerospace industry for structurals with high strength/weight ratios. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. 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-1004. Producer or source: Crucible Service Centers.

Alcan 5086 is used in the aerospace industry, particularly when good mechanical properties and outstanding corrosion resistance are required. This datasheet covers Alcan 5086 alloy in O and several H tempers as tubing. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, machining, and joining. Filing Code: AL-420. Producer or source: Alcan Inc.

J and L TYPE 304-N is a nitrogen-bearing, high strength stainless steel which is stronger than Type 304 but retains the other characteristics of the latter. It has many applications in the aerospace, industrial, and instrument fields. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength 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: SS-244. Producer or source: Jones & Laughlin Steel Corporation.

METGLAS MBF-20A is a general-purpose, nickel-base filler metal well suited for brazing stainless steels and heat-resisting nickel alloys. It is supplied as ductile, flexible metallic-glass foil that can be stamped or cut into precision preforms to fit complex joints; it acts as its own shim. It is 100% metal, 100% dense and contains no organic binders to remove by baking. At elevated temperatures in brazed joints it has an outstanding combination of strength, fatigue properites and resistance to oxidation and corrosion. It is used in the aerospace industry for joining internal assemblies. This datasheet provides information on composition, physical properties, microstructure, tensile properties. It also includes information on heat treating. Filing Code: Ni-262. Producer or source: Allied Chemical Corporation.

FERRO-TIC MS-5 is comprised of ultrahard titanium carbide grains cemented by an age-hardenable martensitic stainless steel matrix. Its unique combination of wear, heat and corrosion resistance and toughness make it well suited for abrasion-resistant components in the aerospace, chemical and food industries. Its maximum operating temperature is 850 F. This datasheet provides information on composition, physical properties, hardness, and elasticity as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and surface treatment. Filing Code: TS-269. Producer or source: Chromalloy Metal Tectonics Company.

TIMETAL 550 is a medium strength forgeable alpha beta alloy for applications in the aerospace and automotive industries. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: TI-112. Producer or source: Titanium Metals Corporation (Timet).

Wieland Duro Molybdenum is unalloyed molybdenum produced from pressed-and-sintered billets. Its unique combination of physical, mechanical, and chemical properties makes it ideal for exacting applications in the electronics, aerospace, nuclear, and metalworking industries. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and machining. Filing Code: Mo-19. Producer or source: Wieland Duro GmbH.

Arcam Ti6Al4V is a titanium-based alloy that is used for the production of additively manufactured components using electron beam melting (EBM). These components are used in applications that demand high levels of reliable performance as in aerospace, automotive, biomedical, chemical, power generation, oil and gas extraction, sports, and other major industries. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: Ti-174. Producer or source: Arcam AB (a GE Additive company).

INCONEL Alloy 601 is a nickel-chromium solid-solution alloy with excellent high-temperature properties which make it attractive for many application in aerospace and process industries. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-152. Producer or source: Huntington Alloy Products Division, An INCO Company.