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13Cr-4.5Mo-0.75Ti-6Al-2.3(Nb+Ta)-Zr-B NICKEL BASED SUPERALLOY CASTINGS 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  33.0 - 40.0 MPa
@Temperature 975 °C,
Time 3.60e+8 sec
4790 - 5800 psi
@Temperature 1790 °F,
Time 100000 hour
 31.0 - 50.0 MPa
@Temperature 950 °C,
Time 3.60e+8 sec
4500 - 7250 psi
@Temperature 1740 °F,
Time 100000 hour
 39.0 - 62.0 MPa
@Temperature 925 °C,
Time 3.60e+8 sec
5660 - 8990 psi
@Temperature 1700 °F,
Time 100000 hour
 50.0 - 77.0 MPa
@Temperature 900 °C,
Time 3.60e+8 sec
7250 - 11200 psi
@Temperature 1650 °F,
Time 100000 hour
 63.0 - 94.0 MPa
@Temperature 875 °C,
Time 3.60e+8 sec
9140 - 13600 psi
@Temperature 1610 °F,
Time 100000 hour
 79.0 - 116 MPa
@Temperature 850 °C,
Time 3.60e+8 sec
11500 - 16800 psi
@Temperature 1560 °F,
Time 100000 hour
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 5.0 - 7.0 %5.0 - 7.0 %
Boron, B <= 0.025 %<= 0.025 %
Chromium, Cr 12 - 14 %12 - 14 %
Iron, Fe 69.6 - 77 %69.6 - 77 %As Balance
Molybdenum, Mo 3.5 - 5.5 %3.5 - 5.5 %
Nb + Ta 2.0 - 2.6 %2.0 - 2.6 %
Titanium, Ti 0.50 - 1.25 %0.50 - 1.25 %

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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NIMS032 / 77549

Specialty Compounds RTP Company

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