Carpenter titanium alloy 6Al-4V is an alpha-beta alloy that contains alpha and beta stabilizers and can be heat treated. This alloy accounts for more than 50% of total titanium usage, mostly in aerospace applications. 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: TI-60. Producer or source: Carpenter Technology Corporation. Originally published as Carpenter Titanium 6-4, October 1970, revised August 2002.

CARPENTER TITANIUM 6-6-2 is an alpha-beta titanium alloy offering good corrosion resistance in applications requiring high strength-to-weight ratios to 750 F (400 C). 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, joining, and surface treatment. Filing Code: Ti-61. Producer or source: Carpenter.

CarTech Ti 15V-3Cr-3Sn-3Al (UNS R58153) is a metastable beta titanium alloy that offers substantial weight reduction in comparison with other engineering materials. If used in the solution heat treated condition, the alloy has excellent cold formability. In the aged condition, the alloy has high strength. It is acceptable for use up to 230 °C (550 °F). 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, and joining. Filing Code: Ti-180. Producer or source: Carpenter Technology Corporation.

Carpenter titanium alloy Ti 3Al-8V-6Cr-4Mo-4Zr, or Ti-3-8-6-4-4, is a beta alloy that contains large amounts of beta stabilizers (molybdenum and vanadium) and can be heat treated. The alloy is commonly known as Beta C. A specialized application for this alloy is aircraft springs. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: TI-130. Producer or source: Carpenter Technology Corporation.

Carpenter titanium alloy Ti 6Al-4V ELI is a high-purity (extra-low-interstitial) version of Ti 6Al-4V (see Alloy Digest Ti-60, August 2002). The alloy is alpha plus beta and has good biocompatibility. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: TI-129. Producer or source: Carpenter Technology Corporation.

Aubert & Duval TA6V ELI (UNS R56401) is an alpha-beta, titanium-aluminum-vanadium alloy that is normally used in the annealed condition. It is a purer version of Aubert & Duval TA6V, with a lower oxygen and iron content. Aubert & Duval TA6V ELI is especially popular due to its ductility at cryogenic temperatures and its excellent biocompatibility with the human body. 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-192. Producer or source: Aubert & Duval S.A.

Rem-Cru C-130AM titanium-base alloy was developed with a minimum yield strength of 130,000 psi for fabrication into bars and forgings. It was formerly known as Rem-Cru RC-130B. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive 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, joining, and surface treatment. Filing Code: Ti-3. Producer or source: Rem-Cru Titanium Inc..

Aubert & Duval TA6V (UNS R56400) is an alpha–beta, titanium-aluminum-vanadium alloy that is used in the annealed or the solution heat treated and aged condition. It is characterized by high specific strength and excellent corrosion resistance, and is one of the most commonly used titanium alloys. 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-191. Producer or source: Aubert & Duval S.A.

ALUMINUM 356 is a heat treatable aluminum casting alloy recommended for high strength, pressure-tight castings, and intricate shapes. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as heat treating, machining, and joining. Filing Code: Al-21. Producer or source: Aluminum Company of America.

Reynolds R301 is a composite material, constituted of a core of high strength aluminum alloy, clad with a corrosion-resistant aluminum alloy. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Al-16. Producer or source: Reynolds Metals Company.

Carpenter 286-LNi Alloy is a precipitation-hardenable Fe-Ni-Cr alloy designed to resist corrosion while providing high strength at temperatures up to 704 deg C (1300 deg F). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming and heat treating. Filing Code: SS-1021. Producer or source: Carpenter Technology Corporation.

ALUMINUM 355 is a heat treatable aluminum alloy containing silicon and copper as the major alloying elements. It is recommended for light weight, high strength, pressure tight castings. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance as well as heat treating, machining, and joining. Filing Code: Al-18. Producer or source: Aluminum Company of America.

ALCAN 135 is a heat treatable aluminum casting alloy having high strength, pressure tightness, and is capable of being cast in intricate shapes. It has high corrosion resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Al-20. Producer or source: Aluminum Company of Canada Ltd.

PYROMET V-57 is an austenitic, iron-base precipitation-hardening alloy designed for service up to 1400 F (760 C) with good corrosion resistance at operating temperatures. The alloy is usually consumable-electrode, vacuum melted. 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: SS-474. Producer or source: Carpenter.

Frontier 40-E aluminum alloy is a high strength natural aging aluminum-zinc-magnesium-chromium-titanium alloy. It requires no heat treatment to develop high strength, has high shock resistance, exceptional corrosion resistance, high yield strength, excellent machinability, and pressure tightness. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-2. Producer or source: Frontier Bronze Corporation.

Nimonic 80 and Nimonic 80A are nickel-base alloys containing a high percentage of chromium, with aluminum and titanium as hardening agents. They are made to the same compositional specification, but Nimonic 80A is produced to meet a more severe requirement with respect to resistance to creep when stressed at higher temperatures than Nimonic 80. Both alloys show high strength at high temperature levels and are very resistant to scaling, oxidation, heat and corrosion. 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-10. Producer or source: Henry Wiggin & Company Ltd.

CarTech Ti-3Al-8V-6Cr-4Mo-4Zr, also known as Ti-3-8-6-4-4 and Beta C, is a metastable beta alloy used in the solution heat treated or solution heat treated and aged condition. It is appropriate for applications where very high strength, minimum weight, and corrosion resistance are important. Ti-3Al-8V-6Cr-4Mo-4Zr has gained in popularity among beta alloys because it is easier to melt and process, exhibiting low segregation, good workability, and good heat-treating properties. 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-172. Producer or source: Carpenter Technology Corporation.

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.

PYROMET A-286 is an age-hardenable austenitic iron-nickel-chromium alloy designed for service up to 1300 F (704 C) on jobs requiring high strength and good corrosion resistance at the operating temperature. It offers high ductility in notched sections. Pyromet A-286 is used in jet engines and superchargers for various high-temperature components. 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 and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-340. Producer or source: Carpenter.

ATI 6-4 is an alpha-beta, Ti-6Al-4V alloy that is used in the annealed condition, or in the solution heat treated and aged condition. This high-strength alloy can be used at cryogenic temperatures up to about 425 °C (800 °F). Ti-6Al-4V is the most widely used titanium alloy. 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, machining, and joining. Filing Code: Ti-171. Producer or source: ATI.