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1-20 of 27
Alpha and near alpha titanium alloys
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Journal Articles
Alloy Digest (2022) 71 (6): Ti-186.
Published: 01 June 2022
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Austral Wright Titanium Grade 7 (UNS R52400) is a corrosion resistant alpha titanium alloy with mechanical properties similar to those of the commercially pure grades. The presence of 0.12–0.25 % palladium in this alloy improves its corrosion resistance, particularly in mineral acids and strong brines. It is used in applications where the medium is mildly reducing or fluctuates between oxidizing and reducing. 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-186. Producer or source: Austral Wright Metals.
Journal Articles
Alloy Digest (2021) 70 (12): Ti-185.
Published: 01 December 2021
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Smiths Ti-6Al-2Sn-4Zr-2Mo-Si is a near-alpha titanium alloy that was developed for use at elevated temperatures. It exhibits high strength and toughness, excellent creep resistance, and high temperature stability at temperatures up 550 °C (1020 °F). 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 joining. Filing Code: Ti-185. Producer or source: Smiths Metal Centres Limited.
Journal Articles
Alloy Digest (2020) 69 (8): Ti-169.
Published: 01 August 2020
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ATI 6-2-4-2 is a near-alpha, high strength, titanium alloy that exhibits a good combination of tensile strength, creep strength, toughness, and long-term stability at temperatures up to 425 °C (800 °F). Silicon up to 0.1% frequently is added to improve the creep resistance of the alloy. This datasheet provides information on composition, physical properties, hardness, 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: Ti-169. Producer or Source: ATI.
Journal Articles
Alloy Digest (2017) 66 (3): Ti-158.
Published: 01 March 2017
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ATI 6-2-4-2 alloy is a near-alpha high strength titanium alloy. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ti-158. Producer or source: Allegheny Technologies Inc..
Journal Articles
Alloy Digest (2014) 63 (3): Ti-152.
Published: 01 March 2014
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Timetal 8-1-1 is a near alpha alloy with excellent creep resistance. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on forming. Filing Code: Ti-152. Producer or source: Timet.
Journal Articles
Alloy Digest (2007) 56 (6): Ti-140.
Published: 01 June 2007
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Timetal 6-2-4-2 has a combination of tensile strength, creep strength, toughness, and high-temperature stability for long-term application at temperatures up to 538 deg C (1000 deg F). This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: TI-140. Producer or source: Timet.
Journal Articles
Alloy Digest (2001) 50 (8): Ti-118.
Published: 01 August 2001
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TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. 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 forming and heat treating. Filing Code: TI-118. Producer or source: Timet.
Journal Articles
Alloy Digest (2001) 50 (7): Ti-116.
Published: 01 July 2001
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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.
Journal Articles
Alloy Digest (1998) 47 (8): Ti-113.
Published: 01 August 1998
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TIMETAL 5111 is a near-alpha titanium alloy of intermediate strength for use where high toughness and corrosion to marine environments are important. 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. Filing Code: TI-113. Producer or source: Titanium Metals Corporation (Timet).
Journal Articles
Alloy Digest (1997) 46 (9): Ti-109.
Published: 01 September 1997
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Sandvik Ti-3Al-2.5V Grade 9 titanium-aluminum alloy offers excellent corrosion resistance, especially to chloride media, and has a high strength-to-weight ratio, which is especially suitable for use in aerospace applications. Tubing can be produced having a CSR (contractile strain ratio) that enhances the fatigue endurance limit. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fatigue. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: TI-109. Producer or source: Sandvik.
Journal Articles
Alloy Digest (1993) 42 (2): Ti-104.
Published: 01 February 1993
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TIMETAL 1100, a near alpha alloy, was developed for elevated temperature use around 1100 F (600 C). The alloy is to be used in the beta processed condition. The alloy offers the highest combination of strength, creep resistance, fracture toughness, and stability of any commercially available titanium alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: TI-104. Producer or source: Timet.
Journal Articles
Alloy Digest (1991) 40 (8): Ti-98.
Published: 01 August 1991
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ALLVAC 6A1-6V-2Sn is a highly beta stabilized alpha + beta titanium alloy, a modification of the 6 A1-4V system. Added vanadium plus copper and iron produce the stabilizing effect. 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, machining, and joining. Filing Code: Ti-98. Producer or source: Teledyne Allvac.
Journal Articles
Alloy Digest (1991) 40 (3): Ti-97.
Published: 01 March 1991
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ALLVAC 8A1-1Mo-1V alloy is predominantly alpha in microstructure, aluminum being the alpha stabilizing component and giving the alloy the lowest density of all commercial titanium based materials. 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 and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-97. Producer or source: Teledyne Allvac.
Journal Articles
Alloy Digest (1990) 39 (4): Ti-95.
Published: 01 April 1990
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Ti-3A1-2.5V is a near-alpha titanium alloy offering 20-50% higher tensile properties than the strongest commercially pure grade of titanium at both room and elevated temperatures. Normally furnished in the annealed, or in the cold-worked stress-relieved condition, Ti-3A1-2.5V titanium alloy features excellent cold formability and good notch tensile properties, as well as corrosion resistance in many environments. 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-95. Producer or source: Titanium alloy mills.
Journal Articles
Alloy Digest (1988) 37 (2): Ti-90.
Published: 01 February 1988
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RMI 5A1-2.5Sn is an alpha titanium alloy. It is not hardenable by heat treatment. The relatively high aluminum content gives the alloy good strength characteristics and resistance to elevated-temperature oxidation (up to 1100 F). RMI 5A1-2.5Sn is readily weldable. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength 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: Ti-90. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1983) 32 (7): Ti-85.
Published: 01 July 1983
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CABOT Ti-3A1-2.5V alloy is both lightweight and strong. It has a high strength-to-weight ratio which provides a major design advantage saving weight. It can be formed readily and it has good weldability. Seamless tubing of CABOT Ti-3A1-2.5V was developed for aircraft hydraulic and fuel systems and its performance has been proved by use in various types of aircraft and aerospace vehicles. CABOT Ti-3A1-2.5V is available as plate, sheet and seamless tubing and pipe. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ti-85. Producer or source: Cabot Wrought Products.
Journal Articles
Alloy Digest (1980) 29 (7): Ti-78.
Published: 01 July 1980
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RMI 5A1-5Sn-2Zr-2Mo-Si is an alpha-type titanium alloy recommended for high-temperature applications in the 800-1000 F range. In the mill annealed condition it has a typical room-temperature yield strength of 126,000 psi and a typical yield strength (in short-time elevated-temperature tensile test) of 80,000 psi at 1000 F. Its uses include elevated-temperature service and jet-engine components. This datasheet provides information on composition, physical properties, hardness, 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: Ti-78. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1980) 29 (2): Ti-75.
Published: 01 February 1980
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RMI 5A1-2.5Sn ELI (ELI = Extra Low Interstitials) is an alpha titanium alloy that was developed for use at cryogenic temperatures. It has a guaranteed minimum yield strength of 100,000 psi at room temperature with good ductility and formability; its yield strength and elongation increase substantially as temperature is lowered. It is used successfully for high-pressure vessels at temperatures below -320 F. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as fracture toughness. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-75. Producer or source: RMI Company.
Journal Articles
Alloy Digest (1968) 17 (3): Ti-56.
Published: 01 March 1968
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Ti-0.20Pd is an alpha-type titanium alloy recommended for the chemical industry applications where environments are moderately reducing, or fluctuate between oxidizing and reducing. 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: Ti-56. Producer or source: Reactive Metals Corporation.
Journal Articles
Alloy Digest (1967) 16 (8): Ti-52.
Published: 01 August 1967
Abstract
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Ti-6Al-2Sn-4Zr-2Mo is a super-alpha titanium alloy providing an excellent combination of creep strength, tensile strength, toughness and stability to 1050 F. It is recommended for airframe and gas turbine engine requirements. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-52. Producer or source: Titanium Metals Corporation of America.
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