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TIMET TIMETAL® 550 (Ti-4Al-4Mo-2Sn) Titanium Alloy Solution Treated
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy

Material Notes: High-Strength Forging Alloy

Industry Specifications: Germany Aerospace: 3.7184. France: T-A4DE. UK Aerospace Specifications BS TA. 45, 46, 47, 48,49, 50, 51, 57.

Features: TIMETAL 550, like TIMETAL 6-4, is readily forgeable and is generally used in a heat treated condition. It has superior room and elevated temperature tensile strength and fatigue strength compared to TIMETAL 6-4, and is creep resistant up to 400°C. It has applications in the aerospace industry, both as aeroengine and airframe components. Typical applications include compressor discs and flap tracks. The alloy has also found applications in high performance automotive engines. The alloy may be welded using controlled electron beam or laser welding techniques. Slow welding speeds and low cooling rates are necessary to achieve adequate weld properties. In sheet form, the alloy has good superplastic properties and excellent balance of strength and toughness.

Typical heat treatment for this alloy: Solution heat treatment: 900°C for 1 hr per 25 mm section, air cool. Aging treatment: 500°C for 24 hrs, air cool.

Data provided by TIMET.

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Physical PropertiesOriginal ValueComments
Density 4.60 g/ccTypical
 
Mechanical PropertiesOriginal ValueComments
Tensile Strength, Ultimate 1080 MPaTypical
Tensile Strength, Yield 930 MPa
@Strain 0.2 %
Typical
Elongation at Break 12 %Typical
Reduction of Area 20 %
Modulus of Elasticity 110 - 120 GPaDynamic
Fatigue Strength 540 - 650 MPaLimit; test specifics not reported
Fracture Toughness 57.0 - 70.0 MPa-m½K(IC); Typical Forging (heat treatment unspecified); Tangential
 65.0 - 69.0 MPa-m½K(IC); Typical Bar (heat treatment unspecified); Longitudinal
 
Thermal PropertiesOriginal ValueComments
CTE, linear 8.80 µm/m-°C
@Temperature 20.0 - 100 °C
 9.70 µm/m-°C
@Temperature 20.0 - 500 °C
Specific Heat Capacity 0.634 J/g-°C
Thermal Conductivity 7.52 W/m-K
Maximum Service Temperature, Air 400 °CGood tensile and creep to 400°C
Beta Transus 975 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 3.0 - 5.0 %
Hydrogen, H <= 0.0125 %
Iron, Fe <= 0.20 %
Molybdenum, Mo 3.0 - 5.0 %
O + 2N <= 0.27 %
Other, each 0.10 %
Other, total 0.40 %
Silicon, Si 0.30 - 0.70 %
Tin, Sn 1.5 - 2.5 %
Titanium, Ti 85.9 - 92.2 %Calculated as remainder

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

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NTIME550 / 19303

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