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Ensinger PEI

B. 1900 Cast Nickel Superalloy
Categories: Metal; Superalloy; Nickel Base

Material Notes: Typical Applications: Jet engine blades.

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Physical PropertiesMetricEnglishComments
Density 8.22 g/cc0.297 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Rupture Strength  106 MPa
@Temperature 982 °C,
Time 3.60e+6 sec
15400 psi
@Temperature 1800 °F,
Time 1000 hour
 179 MPa
@Temperature 982 °C,
Time 360000 sec
26000 psi
@Temperature 1800 °F,
Time 100 hour
 379 MPa
@Temperature 816 °C,
Time 3.60e+6 sec
55000 psi
@Temperature 1500 °F,
Time 1000 hour
 503 MPa
@Temperature 816 °C,
Time 360000 sec
73000 psi
@Temperature 1500 °F,
Time 100 hour
 
Thermal PropertiesMetricEnglishComments
CTE, linear 11.7 µm/m-°C
@Temperature 20.0 - 100 °C
6.50 µin/in-°F
@Temperature 68.0 - 212 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 6.0 %6.0 %
Boron, B 0.015 %0.015 %
Carbon, C 0.10 %0.10 %
Chromium, Cr 8.0 %8.0 %
Cobalt, Co 10 %10 %
Iron, Fe <= 0.35 %<= 0.35 %
Manganese, Mn <= 0.20 %<= 0.20 %
Nickel, Ni 69.505 %69.505 %As Balance
Niobium, Nb (Columbium, Cb) <= 0.10 %<= 0.10 %
Silicon, Si <= 0.25 %<= 0.25 %
Tantalum, Ta 4.3 %4.3 %
Titanium, Ti 1.0 %1.0 %
Tungsten, W <= 0.10 %<= 0.10 %
Zirconium, Zr 0.080 %0.080 %

References for this datasheet.

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