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Ti-2.5Cu


Description

Ti-230
TITANIUM ALLOY

Ti-2.5Cu titanium alloy, also known as Ti-230 titanium alloy, is a binary alloy with 2.5% copper added to improve mechanical properties (particularly at elevated temperatures (up to 662 °F)) compared to unalloyed titanium while maintaining the formability and weldability. Aged Ti-2.5Cu alloy is more creep-resistant than the hardest grade of commercially pure titanium at all temperatures. Since 1959, the alloy has been used in annealed condition as sheet, forgings and extrusions for fabricating components such as bypass ducts of gas-turbine engines. By the development of an ageing treatment, it also has been used in airframe industry. Ageing treatment can raise its room temperature tensile properties by ~25% and nearly double the elevated temperature properties.

Chemical Component

TiFeONCHCuOthers
Balance0.20% max0.20% max0.03% max0.08% max0.01% max2.0-3.0%0.10% max (each);
0.40% max (total);

Basic Information

ItemsTi-2.5Cu
CatalogACAM-Ti-A004
Density0.165 lb/in3 (4.56 g/cm3)
Mean Coefficient of Thermal Expansion5.0 x 10-6 in in-1 °F-1 (9.0 x 10-6 m m-1 °C-1)
Thermal Conductivity7.50 Btu hr-1 ft-1 °F-1 (12.97 W m-1K-1)
Electrical Resistivity26 µΩ·in (0.65 µΩ·m)
Beta Transus1640 °F (890 °C)
Magnetic PermeabilityNonmagnetic

Material Forms

Alfa Chemistry offers Ti-2.5Cu in a variety of forms, including Forging Stock, Forgings, Extrusions, Plate, Sheet, Bars and Billets.

Mechanical Properties

PropertiesConditionsUltimate Tensile Strength>0.2% Yield StrengthElongationReduction of Area
Minimum tensile properties-88 ksi (610 Mpa)71 ksi (490 Mpa)10%25%
Typical tensile propertiesSheet ST90 ksi (620 Mpa)77 ksi (530 Mpa)24% (on 50mm)-
Sheet STA175-185 ksi (1207-1276 Mpa)96 ksi (660 Mpa)20% (on 50mm)-
Bar & Rod ST91 ksi (630 Mpa)72 ksi (500 Mpa)27%45%
Bar & Rod STA107 ksi (740 Mpa)84 ksi (580 Mpa)22%41%
Extrusions ST91 ksi (630 Mpa)72 ksi (500 Mpa)30%40%
Extrusions STA115 ksi (790 Mpa)97 ksi (670 Mpa)28%30%

Additional Properties

Forming: It is amenable to cold forming by conventional methods, such as pressing, stretch forming, spinning, etc., as applied to the stainless steels.
Welding: Ti-2.5Cu Alloy can be joined by fusion, resistance, flash-butt and pressure welding.
Heat Treatment: The full heat treatment consists of solution treatment at 805 ± 10 °C followed by a rapid cool and a duplex ageing process of 8-24 h at 400 °C and 8 h at 475 °C.

Applications

Ti-2.5Cu is used both in the airframe and in components such as bypass ducts for gas-turbine engines.

* Technical data included herein should be used as a guideline only, and should not be construed as maximum or minimum values for specification or for final design, or for a particular use or application. The data may be revised anytime without notice.

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