Search Results for modulus of elasticity

RMI Beta C is a heat-treatable titanium-base alloy that develops a tensile strength of over 200,000 psi in the solution-treated-and-aged condition. It has good ductility and toughness, good fabricability and a low elastic modulus. It has good resistance to general corrosion and it resists hot, aggressive environments containing ferric chloride, sodium chloride, carbon dioxide and hydrogen sulfide. Its applications include coil springs, fasteners, rivets and downhole oil-production 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: Ti-87. Producer or source: RMI Company.

N1-SPAN-C alloy 902 is an age-hardenable, nickel-iron-chromium alloy. Its outstanding characteristic is a controllable thermoelastic coefficient. Proper combination of cold work and thermal treatment can produce an essentially constant modulus of elasticity from -50 F to +150 F. The alloy is especially suitable for many types of precision equipment where elastic members are subject to temperature fluctuations. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Fe-32. Producer or source: Huntington Alloy Products Division, An INCO Company.

ISO-ELASTIC is an iron-nickel alloy having low temperature coefficient of the modulus of elasticity. It is suitable for precision instrument springs. 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, and machining. Filing Code: Fe-14. Producer or source: John Chatillon & Sons.

Carpenter Low Expansion 43-PH is an age hardenable iron/nickel austenitic alloy. It differs from most metals and alloys in that it has a constant modulus of elasticity over a temperature range of -30 to +150 F(-47 to +66 C). Its thermal elastic coefficient can be adjusted to zero or near zero by varying the aging temperature and degree of cold work prior to aging. The alloy possesses high strength and good formability. 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, and joining. Filing Code: Fe-91. Producer or source: Carpenter.

Wieland Duro Tungsten is unalloyed tungsten produced from pressed-and-sintered billets. The high melting point of tungsten makes it an obvious choice for structural applications exposed to very high temperatures. Tungsten is used at lower temperatures for applications that can benefit from its high density, high modulus of elasticity, or radiation shielding capability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on machining. Filing Code: W-34. Producer or source: Wieland Duro GmbH.

REVERE NO. 770 is an 18% nickel silver alloy having high malleability, high modulus of elasticity and high resistance to corrosion. It is a spring stock alloy. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cu-130. Producer or source: Revere Copper and Brass Inc..

Climelt Molybdenum-0.5% Ti is a molybdenum alloy having high strength at elevated temperatures, high modulus of elasticity, low coefficient of expansion, and high thermal conductivity. It has exceptionally high rupture properties above 1600 F. 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, joining, and surface treatment. Filing Code: Mo-2. Producer or source: Climax Molybdenum Company.

NI-SPAN C is an age-hardenable iron-nickel-chromium-titanium alloy having a constant modulus, with advantages for control, measuring and timing equipment that temperature changes between -50 and 150 deg. F cannot weaken or soften. Temperature changes between -50 and 150 deg. F do not change its elastic properties. It is one of a series of four Ni-Span alloys. 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, and machining. Filing Code: Fe-2. Producer or source: Henry Wiggin & Company Ltd.

INCOLOY alloy 903 is a precipitation hardenable nickel-iron-cobalt alloy whose outstanding characteristics are a constant low coefficient of thermal expansion, a constant modulus of elasticity and high strength. 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: Fe-50. Producer or source: Huntington Alloy Products Division, An INCO Company.

Precision C is a heat-treatable nickel-iron alloy used in critical diaphragm applications. The alloy composition provides a unique constant elastic modulus value over a temperature range of -50 to 150 deg F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. Filing Code: FE-113. Producer or source: Hamilton Precision Metals Inc.

Vanadis 30 is cobalt alloyed high-performance, high-speed steel made by powder metallurgy. The cobalt addition of approximately 8.5% has a positive influence on the hot strength, hot hardness, temper resistance, and modulus of elasticity. Punches are a suitable application for this alloy. This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes information on wear resistance as well as heat treating and surface treatment. Filing Code: TS-566. Producer or source: Uddeholm Tooling AB.

ALCOA Alloy 2090 is an aluminum-lithium alloy with 8% lower density and 12% higher elastic modulus than 7075-T6, a major high-strength alloy used in aircarft structures. Special facilities and practices required for casting commercial size aluminum-lithium ingots have been developed to cope with the highly reactive nature of lithium in molten aluminum. In general, the alloy should be considered for use in light-weight structures requiring high strength and stiffness. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-299. Producer or source: Aluminum Company of America.

Alcan 2196 T8511 is produced as extrusions for applications where compression is critical. 2196 Al-Li alloy, with high strength and elastic modulus but low density, is used for floor beams, seat tracks, welded applications, and wing stringers. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: AL-426. Producer or source: Alcan Inc.

HPM Precision C is heat treatable and has a constant elastic modulus value. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming. Filing Code: Fe-153. Producer or source: Hamilton Precision Metals.

LOCKALLOY is a beryllium-aluminum alloy that was developed for aerospace structural applications where high modulus and low density are design criteria. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Be-1. Producer or source: Kawecki Berylco Industries Inc..

ELINVAR EXTRA is an age-hardenable iron-nickel-chromium-titanium alloy having a constant modulus with a zero thermoelastic coefficient over a limited range of temperature from minus 50 deg. F. to a plus 150 deg. F. 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, joining, and surface treatment. Filing Code: Fe-12. Producer or source: Allied Products Division.

NODULOY is a magnesium inoculated ductile cast iron in which the graphite is in the nodular form. It offers excellent castability, high mechanical properties, good machinability, pressure tightness, high modulus, and excellent shock resistance. It has extraordinary high ductility in the annealed state. This datasheet provides information on composition, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, and machining. Filing Code: CI-1. Producer or source: Dominion Wheel & Foundries Ltd.

AlBeMet AM 162 is a beryllium, 38% aluminum alloy produced in extruded bar, rolled sheet, and hot isostatic pressed (HIP) billets that combines the high-modulus and low-density characteristics of beryllium with the fabrication and mechanical behavior of aluminum. The alloy is weldable, can be formed, machined and brazed like conventional aluminum alloys. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on machining. Filing Code: BE-8. Producer or source: Brush Wellman Inc.

This pure aluminum matrix composite contains 60 volume% alumina. The aluminum ceramic fiber is Nextel 610. The fiber effects the longitudinal direction, resulting in a high longitudinal specific modulus and a specific strength with good off-axis properties. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength. It also includes information on corrosion resistance as well as casting. Filing Code: AL-344. Producer or source: 3M.

3M TITANIUM MATRIX COMPOSITES are produced by electron-beam evaporation to apply Ti-6Al-4V coating to high-strength, high-modulus silicon carbon fibers. The resulting composite has increased strength and stiffness over monolithic titanium/titanium alloy parts. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as creep and fatigue. It also includes information on surface treatment. Filing Code: TI-111. Producer or source: 3M Metal Matrix Composites Program.