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Master Bond adhesives

A286 IRON BASED 15Cr-26Ni-1.3Mo-2.1Ti-0.3V SUPERALLOY FORGINGS FOR GAS TURBINE DISCS
Categories: Metal; Ferrous Metal; Stainless Steel; Superalloy; Iron Base

Material Notes:

Creep and rupture data provided by NIMS

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Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 304304
Tensile Strength, Ultimate 1035 MPa150100 psi
Tensile Strength, Yield 760 MPa110000 psi
Elongation at Break 25 %25 %
Rupture Strength  110 MPa
@Temperature 675 °C,
Time 3.60e+8 sec
16000 psi
@Temperature 1250 °F,
Time 100000 hour
 95.0 - 143 MPa
@Temperature 650 °C,
Time 3.60e+8 sec
13800 - 20700 psi
@Temperature 1200 °F,
Time 100000 hour
 139 - 186 MPa
@Temperature 625 °C,
Time 3.60e+8 sec
20200 - 27000 psi
@Temperature 1160 °F,
Time 100000 hour
 205 - 247 MPa
@Temperature 600 °C,
Time 3.60e+8 sec
29700 - 35800 psi
@Temperature 1110 °F,
Time 100000 hour
 281 - 321 MPa
@Temperature 575 °C,
Time 3.60e+8 sec
40800 - 46600 psi
@Temperature 1070 °F,
Time 100000 hour
 364 - 394 MPa
@Temperature 550 °C,
Time 3.60e+8 sec
52800 - 57100 psi
@Temperature 1020 °F,
Time 100000 hour
 
Component Elements PropertiesMetricEnglishComments
Chromium, Cr 13 - 17 %13 - 17 %
Iron, Fe 53 - 55 %53 - 55 %
Molybdenum, Mo 1.1 - 1.5 %1.1 - 1.5 %
Nickel, Ni 24 - 28 %24 - 28 %
Titanium, Ti 2.0 - 2.2 %2.0 - 2.2 %
Vanadium, V 0.20 - 0.40 %0.20 - 0.40 %

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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NIMS030 / 77547

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