Search Results for aerospace components

WahChang W-25Re is a tungsten-rhenium alloy recommended for uses where high reliability at high temperatures and ductilities at low temperatures are required, such as, xray targets, cladding, thermocouples, nuclear and aerospace 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: W-15. Producer or source: Wah Chang, a Teledyne Corporation.

ALUMINUM 357.0 is a high-purity aluminum casting alloy that can be solution treated and aged to develop high tensile and yield strengths along with fairly good ductility. Among its uses are aircraft, missile and aerospace components and cylinder blocks for water-cooled engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-238. Producer or source: Various aluminum companies.

AMPCO D-4 is a copper-aluminum-iron-nickel alloy characterized by high hardness and strength, high toughness, good resistance to fatigue and wear, and excellent resistance to corrosion. Its as-cast mechanical properties can be improved by heat treating; in the heat-treated condition it is designated Ampco D-4HT. It is suited for service up to 750 F. Typical applications include aerospace components, marine hardware, valve seats, glands and stuffing box nuts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Cu-444. Producer or source: Ampco Metal Inc..

LESCALLOY 4335+V VAC-ARC is a low-alloy steel with high hardenability and good strength and toughness. It is produced by the vacuum consumable electrode melting process to provide optimum cleanliness and preferred ingot structure. Its uses include aircraft and aerospace components, gears, shafting, bolts and crankshafts. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-390. Producer or source: Latrobe Steel Company.

JESSOP JS600 is a nickel-chromium-iron alloy for use in environments requiring resistance to heat and/or corrosion. It has excellent mechanical properties and a combination of high strength and good workability. It performs well in applications with temperatures from cryogenic to more than 2000 F. Its many applications include aircraft/aerospace components, equipment for chemical and food processing and parts for heat-treating equipment. 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, joining, and surface treatment. Filing Code: Ni-287. Producer or source: Jessop Steel Company.

AMPCO M-4 is a copper-aluminum-nickel-iron-manganese alloy that possesses high hardness, high strength, good resistance to fatigue and wear, and excellent resistance to corrosion. It is used in both cast and wrought forms. Typical applications include marine hardware, aerospace components, wear plates, gears, bushing and pickling equipment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Cu-469. Producer or source: Ampco Metal Inc..

SAE 4820 is a low-carbon (nominally 0.20%) carburizing steel containing nominally 3.5% nickel and 0.25% molybdenum. It is deal for used that require a strong, tough core along with a highly wear-resistant carburized case. In addition, it offers a good combination of strength and low-temperature toughness for non-carburized applications. It is recommended for a wide range of moderately heavy-duty applications. Among its many uses are carburized gears, carburized aerospace components and non-carburized machinery parts. 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: SA-409. Producer or source: Alloy steel mills and foundries.

ALUMINUM 705.0 is an aluminum-zinc-magnesium-manganese-chromium casting alloy that is hardened by aging at room temperature. It offers high mechanical properties in the cast-and-aged condition. It has good castability and high resistance to corrosion. Among its many users are high-pressure oxygen valves, aerospace components, gears, fittings and washing machine agitators. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, and machining. Filing Code: Al-259. Producer or source: Various aluminum companies.

ALUMINUM 707.0 is an aluminum-base foundry alloy that can be hardened by aging at room temperature without a solution treatment. It offers good strength in the cast-and-aged condition. It has relatively good castability, excellent machinability and high resistance to corrosion. Its many uses include aircraft and aerospace components, gears, machinery parts, manifolds, valves and fittings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-260. Producer or source: Various aluminum companies.

ENPLATE NI-423 is a nickel-phosphorus alloy deposited by chemical reduction without electric current. It is deposited by a stable, relatively high-speed functional electroless nickel process that produces a low-stress coating with good ductility and excellent resistance to corrosion. Its many uses include equipment for chemicals and food, aerospace components, molds and electronic devices. This datasheet provides information on composition, physical properties, and hardness. It also includes information on corrosion and wear resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: Ni-343. Producer or source: Enthone Inc..

TECHALLOY Alloy 625 is a nonmagnetic nickel-base alloy with excellent resistance to corrosion and oxidation. It has outstanding strength and toughness from cryogenic temperatures to 2000 F. It also has exceptionally high fatigue strength and is resistant to chloride-ion stress-corrosion cracking. It has a wide range of applications among which are aerospace components, specialized sea-water equipment and nuclear power equipment. This datasheet provides information on composition, physical properties, 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-253. Producer or source: Techalloy Company Inc..

CANNON-MUSKEGON Nickel Alloy C is a cast nickel-base alloy with exceptionally high resistance to corrosion and with excellent high-temperature properties. It also has outstanding oxidation resistance and strength at elevated temperatures. Its many uses include heat-treating equipment, aerospace components and oil-refinery equipment. 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 as well as casting, heat treating, machining, and joining. Filing Code: Ni-255. Producer or source: Cannon-Muskegon Corporation.

CARPENTER STAINLESS TYPE 304HN is essentially a high-nitrogen version of AISI Type 304 stainless steel. By means of solid-solution strengthening, the nitrogen provides significantly higher yield strength and tensile strength as annealed than conventional Type 304, without adversely affecting ductility, corrosion resistance or nonmagnetic properties. Its applications include aircraft and aerospace components and marine hardware. 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: SS-368. Producer or source: Carpenter. See also Alloy Digest SS-763, September 1999.

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.

AL TECH POTOMAC A has well-balanced strength and toughness which make it especially suitable for a wide variety of hot-die steel applications, including those involving severe coolants. Its outstanding mechanical properties make it useful for many non-tooling requirements such as aerospace components. For more specialized needs, the manufacturer offers special melting processes that enhance this steel's fatigue properties and transverse tensile ductility. 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 as well as forming, heat treating, and machining. Filing Code: TS-478. Producer or source: AL Tech Specialty Steel Corporation.

Carpenter Touralloy 230 Plus stainless was originally developed for high-strength aerospace components, however, it may provide improved bar cycle fatigue durability, compared to other traditional golf face plate alloys. 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, and joining. Filing Code: SS-1084. Producer or source: Carpenter Specialty Alloys.

ATI Ti-5Al-2Sn-2Zr-4Cr-4Mo is known as Ti-17 alloy and is a beta-rich material for large aerospace components. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ti-149. Producer or source: ATI Allvac.

Carpenter Stainless Type 304HN is the high-nitrogen version of Type 304 and 304H stainless steels. Interstitial strengthening with both carbon and nitrogen provides this alloy with significantly higher yield and tensile strength as annealed. Typical applications include aerospace and power components, as well as marine shafting. 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: SS-763. Producer or source: Carpenter. See also Alloy Digest SS-368, October 1979.

Udimet 901 is a nickel-base alloy having high tensile and rupture strength to 1200 F. It is recommended for use in aircraft, aerospace and gas turbine components. 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 as well as forming, heat treating, machining, and joining. Filing Code: Ni-155. Producer or source: Special Metals Corporation. See also Alloy Digest Ni-111, February 1966.

IN-102 is a nickel-chromium-iron alloy designed for long service at temperatures up to 1300 F. It combines high strength and high ductility at the elevated temperatures with a high degree of structural stability. It is used for aerospace, power and steam turbine components. 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, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-147. Producer or source: International Nickel Company Inc..