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

Crucible Compaction Metals Rene Supersolvus Rene 95 Nickel Based Superalloy
Categories: Metal; Nonferrous Metal; Nickel Alloy; Superalloy

Material Notes: Supersolvus P/M Rene 95 is designed to provide even higher temperature creep resistance and stress rupture strength than subsolvus Rene 95. Chemistry is not modified. These properties are obtained by processing above the gamma prime solvus to provide a larger grain size than subsolvus processed Rene 95. Although this results in a small reduction in room temperature and elevated temperature strength, substantial ductility is maintained and considerably higher temperature service is possible. The primary use of supersolvus Rene 95 is for high pressure turbine blades retainers for high thrust aircraft turbines. This material can also be used for hot work tooling where ferrous based tool steels cannot maintain adequate strength

Supersolvus Rene 95 is available as-HIP preforms in the same size ranges as standard Rene 95. As-HIP parts can range up to 46 inches (1.2 m) in diameter and weighs up to 16,000 lb (7,200 kg). Extruded billet up to 12 inches (.3 m) in diameter is produced from compacts containing up to 8,000 lb (3,600 kg) of powder.

Advantages:

  • Higher temperature creep resistance and stress rupture strength than standard Rene 95
  • Larger grain size than standard Rene 95

Information provided by Crucible Compaction Metals.

Key Words: Powder Metallurgy
Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Mechanical PropertiesMetricEnglishComments
Tensile Strength, Ultimate  215 MPa
@Temperature 650 °C
31200 psi
@Temperature 1200 °F
 230 MPa
@Temperature 23.0 °C
33400 psi
@Temperature 73.4 °F
Tensile Strength, Yield  150 MPa
@Temperature 650 °C
21800 psi
@Temperature 1200 °F
 170 MPa
@Temperature 23.0 °C
24700 psi
@Temperature 73.4 °F
Elongation at Break  15 %
@Temperature 650 °C
15 %
@Temperature 1200 °F
 17 %
@Temperature 23.0 °C
17 %
@Temperature 73.4 °F
Reduction of Area  17 %
@Temperature 650 °C
17 %
@Temperature 1200 °F
 19 %
@Temperature 23.0 °C
19 %
@Temperature 73.4 °F
Creep Strength  620 MPa
@Temperature 705 °C,
Time 990000 sec
89900 psi
@Temperature 1300 °F,
Time 275 hour
0.2% Creep
 850 MPa
@Temperature 650 °C,
Time 1.26e+6 sec
123000 psi
@Temperature 1200 °F,
Time 350 hour
0.2% Creep
Rupture Strength  620 MPa
@Temperature 760 °C,
Time 198000 sec
89900 psi
@Temperature 1400 °F,
Time 55.0 hour
 1035 MPa
@Temperature 650 °C,
Time 324000 sec
150100 psi
@Temperature 1200 °F,
Time 90.0 hour
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 3.3 - 3.7 %3.3 - 3.7 %
Boron, B 0.0060 - 0.015 %0.0060 - 0.015 %
Carbon, C 0.040 - 0.090 %0.040 - 0.090 %
Chromium, Cr 12 - 14 %12 - 14 %
Cobalt, Co 7.0 - 9.0 %7.0 - 9.0 %
Molybdenum, Mo 3.3 - 3.7 %3.3 - 3.7 %
Nickel, Ni 59.325 - 65.424 %59.325 - 65.424 %As Balance
Niobium, Nb (Columbium, Cb) 3.3 - 3.7 %3.3 - 3.7 %
Titanium, Ti 2.3 - 2.7 %2.3 - 2.7 %
Tungsten, W 3.3 - 3.7 %3.3 - 3.7 %
Zirconium, Zr 0.030 - 0.070 %0.030 - 0.070 %

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:
Crucible Compaction Metals Rene 95 Nickel Based Superalloy
Haynes Hastelloy® C-22® alloy, 0.71-3.2 mm thick sheet, solution heat treated
Rene 100 Nickel Alloy (UNS N13100)
ATI Allvac® 718-OP® UNS N07718 Nickel Superalloy
ATI Allvac® 706 Nickel Superalloy, Heat Treatment: 954°C (1750°F) + Age

NCRUC102 / 16066

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.