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TIMETAL 1100
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Journal Articles
Alloy Digest (1993) 42 (2): Ti-104.
Published: 01 February 1993
...@ 1100 Filing Code: Titanium Alloy II-104 FEBRUARY 1993 - DIGEST- DATA ON WORLD WIDE METALS AND ALLOYS rcloyrkEu- -by:A#oyDipsLInc/201%77-S161 -,a Z~C~W~SO~~D,NJ.O~USOIU.SA TIMETAL 1100 (I-1 100, a hbh strength, high temperature alloy) TIMETALe 1100, a near alpha alloy. was developed for elevated...
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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 (2001) 50 (7): Ti-116.
Published: 01 July 2001
... 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...
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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 (2007) 56 (6): Ti-140.
Published: 01 June 2007
... cool Second stage 785 1450 · · · Air cool Third stage 595 1100 2 Air cool Fig. 1 Typical microstructure at 200× Forgeability: Rough forging is carried out at 1038 1066 °C (1900 1950 °F). Finish forging is done at 954 982 °C (1750 1800 °F). General Characteristics: Timetal 6-2-4-2 has a combination of...
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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 (2007) 56 (8): Ti-141.
Published: 01 August 2007
... 675 98 262 38 (a) Annealed at 705 °C (1300 °F) for 1 h, air cooled. (b) STA = 885 °C (1630 °F) for 1 h, air cooled, plus 595 °C (1100 °F) for 8 h, air cooled. (c) STOA = 885 °C (1630 °F) for 1 h, air cooled, plus 705 °C (1300 °F) for 1 h, air cooled Fig. 2 Creep comparison (0.2%) between Timetal 6-2-4...
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Timetal 6-2-4-6 is an alpha-beta alloy with greater strength in thicker sections than Timetal 6-4. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on forming. Filing Code: TI-141. Producer or source: Timet.
Journal Articles
Alloy Digest (1998) 47 (7): Ti-112.
Published: 01 July 1998
.../asm.ad.ti0112 Table1 Guamntad Minimum Mechanical PropeWes Table 2 Room Temperature Tensile Properties As~6amcdo 1100 160 910 132 12 SaDin AsnrprpLsdcf-mDd 1120 162 948 137 6 >1004bsuprplrsoicfam- 1130 164 7 Table 3 Typical Notch Tensile and Fracture Toughness PrOptieS Bml-lguid 9% 144 1101 160 1.613) 65-69 59...
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TIMETAL 550 is a medium strength forgeable alpha beta alloy for applications in the aerospace and automotive industries. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: TI-112. Producer or source: Titanium Metals Corporation (Timet).
Journal Articles
Alloy Digest (2014) 63 (3): Ti-152.
Published: 01 March 2014
... + 593 ºC (1100 ºF)/24 h/ AC, GPa (106 psi) 24 ºC (75 ºF) 135 (20) 380 ºC (716 ºF) 113 (16) Ultimate tensile strength, forgings and rolled bar, MPa (ksi) 896 (130) 0.2% yield strength, forgings and rolled bar, MPa (ksi) 827 (120) Elongation, forgings and rolled bar, % 10 Reduction in area, % Forgings 20...
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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 (1998) 47 (10): Ti-105.
Published: 01 October 1998
... mctastablc-beta alloy but has been specifically designed for improved oxidation rcsistana, ckvated tcmpemure strength, creep resistance, and thermal stability. TIMETAL 21s is useful for applications from 228-593 C (550-1100 OF). The msistance of the alloy to aircraft hydraulic fluids such as Sky- drol is...
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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.