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Rulon Bearings

15Cr-28Co-4Mo-2.5Ti-3Al NICKEL BASED SUPERALLOY BARS FOR GAS TURBINE BLADES
Categories: Metal; Ferrous Metal; Tool Steel; Air-Hardening Steel

Material Notes:

Creep and rupture data provided by NIMS

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Mechanical PropertiesMetricEnglishComments
Rupture Strength  64.0 MPa
@Temperature 825 °C,
Time 3.60e+8 sec
9280 psi
@Temperature 1520 °F,
Time 100000 hour
 85.0 - 92.0 MPa
@Temperature 800 °C,
Time 3.60e+8 sec
12300 - 13300 psi
@Temperature 1470 °F,
Time 100000 hour
 125 - 131 MPa
@Temperature 775 °C,
Time 3.60e+8 sec
18100 - 19000 psi
@Temperature 1430 °F,
Time 100000 hour
 164 - 173 MPa
@Temperature 750 °C,
Time 3.60e+8 sec
23800 - 25100 psi
@Temperature 1380 °F,
Time 100000 hour
 206 - 223 MPa
@Temperature 725 °C,
Time 3.60e+8 sec
29900 - 32300 psi
@Temperature 1340 °F,
Time 100000 hour
 255 - 272 MPa
@Temperature 700 °C,
Time 3.60e+8 sec
37000 - 39500 psi
@Temperature 1290 °F,
Time 100000 hour
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 2.0 - 4.0 %2.0 - 4.0 %
Chromium, Cr 13 - 17 %13 - 17 %
Cobalt, Co 26 - 30 %26 - 30 %
Iron, Fe 41 - 54 %41 - 54 %As Balance
Molybdenum, Mo 3.0 - 5.0 %3.0 - 5.0 %
Titanium, Ti 2.0 - 3.0 %2.0 - 3.0 %

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.

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