MatWeb - Material Property Data Advertise with MatWeb!     Register Now
Data sheets for over 180,000 metals, plastics, ceramics, and composites.
MatWeb - Material Property Data HOME  •   SEARCH  •   TOOLS  •   SUPPLIERS  •   FOLDERS  •   ABOUT US  •   FAQ  •   LOG IN    
Recently Viewed Materials (most recent at top)  

Login to see your most recently viewed materials here.

Or if you don't have an account with us yet, then click here to register.

  Searches:   Advanced  | Category  | Property  | Metals  | Trade Name  | Manufacturer  | Recently Viewed Materials
  

Master Bond adhesives

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.

Vendors: Visit metalmen for your metals needs. Products include special chemistry, tight tolerances, custom tempers, odd dimensions/forms, and small quantities. Phone 1-800-767-9494.

Click here to view all available suppliers for this material.

Please click here if you are a supplier and would like information on how to add your listing to this material.

 
Physical PropertiesMetricEnglishComments
Density 4.60 g/cc0.166 lb/in³Typical
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength, Ultimate 1080 MPa157000 psiTypical
Tensile Strength, Yield 930 MPa
@Strain 0.2 %
135000 psi
@Strain 0.2 %
Typical
Elongation at Break 12 %12 %Typical
Reduction of Area 20 %20 %
Modulus of Elasticity 110 - 120 GPa16000 - 17400 ksiDynamic
Fatigue Strength 540 - 650 MPa78300 - 94300 psiLimit; test specifics not reported
Fracture Toughness 57.0 - 70.0 MPa-m½51.9 - 63.7 ksi-in½K(IC); Typical Forging (heat treatment unspecified); Tangential
 65.0 - 69.0 MPa-m½59.2 - 62.8 ksi-in½K(IC); Typical Bar (heat treatment unspecified); Longitudinal
 
Thermal PropertiesMetricEnglishComments
CTE, linear  8.80 µm/m-°C
@Temperature 20.0 - 100 °C
4.89 µin/in-°F
@Temperature 68.0 - 212 °F
 9.70 µm/m-°C
@Temperature 20.0 - 500 °C
5.39 µin/in-°F
@Temperature 68.0 - 932 °F
Specific Heat Capacity 0.634 J/g-°C0.152 BTU/lb-°F
Thermal Conductivity 7.52 W/m-K52.2 BTU-in/hr-ft²-°F
Maximum Service Temperature, Air 400 °C752 °FGood tensile and creep to 400°C
Beta Transus 975 °C1790 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 3.0 - 5.0 %3.0 - 5.0 %
Hydrogen, H <= 0.0125 %<= 0.0125 %
Iron, Fe <= 0.20 %<= 0.20 %
Molybdenum, Mo 3.0 - 5.0 %3.0 - 5.0 %
O + 2N <= 0.27 %<= 0.27 %
Other, each 0.10 %0.10 %
Other, total 0.40 %0.40 %
Silicon, Si 0.30 - 0.70 %0.30 - 0.70 %
Tin, Sn 1.5 - 2.5 %1.5 - 2.5 %
Titanium, Ti 85.9 - 92.2 %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 view all the property values for this datasheet as they were originally entered into MatWeb.

Users viewing this material also viewed the following:
TIMET TIMETAL® 550 (Ti-4Al-4Mo-2Sn) Titanium Alloy Solution Treated and Aged
ATI Allvac® 6-2-4-6 Titanium Alloy, Heat Treatment: 885°C (1625°F) + Age
ATI Allvac® 6-4ELI Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Titanium Ti-5Al-2Sn-2Zr-4Mo-4Cr (Ti-17) Alpha-Beta Processed
ATI Allegheny Ludlum Grade 23 (6-4 ELI) Titanium (UNS R56401)

NTIME550 / 19303

Please read our License Agreement regarding materials data and our Privacy Policy. Questions or comments about MatWeb? Please contact us at webmaster@matweb.com. We appreciate your input.

The contents of this web site, the MatWeb logo, and "MatWeb" are Copyright 1996-2024 by MatWeb, LLC. MatWeb is intended for personal, non-commercial use. The contents, results, and technical data from this site may not be reproduced either electronically, photographically or substantively without permission from MatWeb, LLC.