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Ti (Titanium)
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Beta and near-beta titanium alloys
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Journal Articles
Alloy Digest (2021) 70 (7): Ti-180.
Published: 01 July 2021
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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.
Journal Articles
Alloy Digest (2020) 69 (11): Ti-172.
Published: 01 November 2020
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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.
Journal Articles
Alloy Digest (2005) 54 (7): Ti-136.
Published: 01 July 2005
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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.
Journal Articles
Alloy Digest (2005) 54 (6): Ti-94.
Published: 01 June 2005
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Ti-3Al-8V-6Cr-4Zr-4Mo alloy is a heat treatable beta grade titanium alloy. It is a high-strength alloy with fair weldability and is easier to melt than 13-11-3. 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: TI-94. Producer or source: Titanium alloys mills. Originally published as Ti-3Al-8V-6Cr-4Zr-4Mo BETA ALLOY, January 1990, revised June 2005.
Journal Articles
Alloy Digest (2004) 53 (7): Ti-134.
Published: 01 July 2004
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Allvac 38-644 is a metastable beta titanium alloy known for its ductility in the solution treated condition and its high strength and ductility in the solution treated and aged condition. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: TI-134. Producer or source: Allvac Metals Company.
Journal Articles
Alloy Digest (2002) 51 (9): Ti-130.
Published: 01 September 2002
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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.
Journal Articles
Alloy Digest (2001) 50 (12): Ti-124.
Published: 01 December 2001
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RMI Ti Beta-C/Pd alloy is a Ti-3Al-8V-6Cr-4Zr-4Mo-0.05Pd alloy also referred to as Grade 20. It is a palladium-containing version of RMI Beta-C alloy possessing equivalent physical and mechanical properties, but with enhanced corrosion resistance. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fracture toughness and creep. It also includes information on high temperature performance. Filing Code: TI-124. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1998) 47 (10): Ti-105.
Published: 01 October 1998
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TIMETAL 21S (Ti-15%Mo-3%Nb-3%Al-0.2Si) offers the good cold formability and weldability of a beta strip alloy, but with greatly improved oxidation resistance and creep strength. Aerospace applications include engine exhaust plug and nozzle assemblies. 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 and heat treating. Filing Code: TI-105. Producer or source: Titanium Metals Corporation (Timet). Originally published March 1993, revised October 1998.
Journal Articles
Alloy Digest (1992) 41 (12): Ti-102.
Published: 01 December 1992
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TIMETAL 62S, because iron is used for the beta stabilizer in lieu of more expensive elements, has a lower formulation cost than most titanium alloys, yet the properties and processing characteristics of Ti-6A1-2Fe-0. 1Si are equivalent to or better than those of the workhorses of the titanium industry, including Ti-6A1-4V. The combination of reasonable cost and excellent mechanical properties make TIMETAL 62S a practical substitute for other engineering materials in numerous industrial applications that require low weight and high corrosion resistance. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on heat treating. Filing Code: Ti-102. Producer or source: Timet.
Journal Articles
Alloy Digest (1992) 41 (11): Ti-101.
Published: 01 November 1992
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TIMETAL 15-3 is a metastable beta titanium alloy that offers substantial weight reductions over other engineering materials. In the solution treated condition, it has excellent cold formability; in the aged condition, it has high strength. TIMETAL 15-3 is usually acceptable for use at temperatures up to 550 F. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming and heat treating. Filing Code: Ti-101. Producer or source: Titanium Metals Corporation (Timet).
Journal Articles
Alloy Digest (1987) 36 (8): Ti-87.
Published: 01 August 1987
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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.
Journal Articles
Alloy Digest (1973) 22 (5): Ti-68.
Published: 01 May 1973
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Ti-8Mo-8V-2Fe-3A1 is a metastable beta titanium alloy that can be age hardened to high-strength levels. Aging in the range of 800-1200 F partially transforms beta to alpha to produce the high strength. 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: Ti-68. Producer or source: Titanium Metals Corporation of America.
Journal Articles
Alloy Digest (1970) 19 (7): Ti-59.
Published: 01 July 1970
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CRUCIBLE BETA III is a heat-treatable beta titanium alloy offering outstanding cold formability and simple heat treatment to high strengths. It is recommended for aircraft parts and fasteners. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear and bend strength as well as fracture toughness and creep. It also includes information on corrosion resistance as well as forming, heat treating, joining, and surface treatment. Filing Code: Ti-59. Producer or source: Crucible Steel Company of America, Titanium Division.
Journal Articles
Alloy Digest (1968) 17 (2): Ti-55.
Published: 01 February 1968
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Titanium IA1-8V-5Fe is an all beta type titanium alloy recommended for high temperature fasteners. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties 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-55. Producer or source: Reactive Metals Corporation.
Journal Articles
Alloy Digest (1960) 9 (12): Ti-28.
Published: 01 December 1960
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Crucible B-120VCA is a higher performance all-beta titanium alloy. It responds to age-hardening heat treatment and is designed to be stable for at least 1500 hours under stress up to temperatures of 550 F and to substantially higher temperatures for shorter times. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as creep, and deformation. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-28. Producer or source: Crucible Steel Company of America.
Journal Articles
Alloy Digest (1960) 9 (10): Ti-27.
Published: 01 October 1960
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Ti-13V-11Cr-3Al is a high strength, meta-stable beta titanium-base alloy recommended for service in the temperature range of -65 to plus 600 F. It responds to an age-hardening heat treatment. 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: Ti-27. Producer or source: Titanium Metals Corporation of America.
Journal Articles
Alloy Digest (1960) 9 (2): Ti-24.
Published: 01 February 1960
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MST 2.5A1-16V is a titanium-base alloy having a favorable combination of strength, formability and resistance to creep at elevated temperatures. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength 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: Ti-24. Producer or source: Mallory-Sharon Metals Company.