Crucible Compaction Metals Rene 95 Nickel Based Superalloy

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.

(Viewing data as-entered. Click here to return)

Crucible Compaction Metals Rene 95 Nickel Based Superalloy
Categories:	Metal; Nonferrous Metal; Nickel Alloy; Superalloy
Material Notes:	P/M Rene 95 is one of the highest strength alloys available for service in the range of 800°F to 1200°F (425°C to 650°C). The alloy also provides excellent high temperature creep resistance and low cycle fatigue life. Tens of thousands of high pressure turbine discs and turbine blades retainers made from Crucible Rene 95 are in service on commercial and military airplanes and helicopters worldwide. Rene 95 is available as either as-HIP preforms or extruded billet. 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: High Strength Excellent high temperature creep resistance Extended low cycle fatigue life 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.
Printer friendly version Download as PDF Download to Excel (requires Excel and Windows) Export data to your CAD/FEA program Add to Folder:

Mechanical Properties	Original Value	Comments

Tensile Strength, Ultimate	210 MPa @Temperature 650 °C
	240 MPa @Temperature 23.0 °C
Tensile Strength, Yield	160 MPa @Temperature 650 °C
	180 MPa @Temperature 23.0 °C
Elongation at Break	10 % @Temperature 650 °C
	14 % @Temperature 23.0 °C
Reduction of Area	13 % @Temperature 650 °C
	17 % @Temperature 23.0 °C
Creep Strength	620 MPa @Temperature 705 °C, Time 72000 sec	0.2% Creep
	850 MPa @Temperature 650 °C, Time 864000 sec	0.2% Creep
Rupture Strength	620 MPa @Temperature 760 °C, Time 36000 sec
	1035 MPa @Temperature 650 °C, Time 198000 sec

Component Elements Properties	Original Value	Comments
Aluminum, Al	3.3 - 3.7 %
Boron, B	0.0060 - 0.015 %
Carbon, C	0.040 - 0.090 %
Chromium, Cr	12 - 14 %
Cobalt, Co	7.0 - 9.0 %
Molybdenum, Mo	3.3 - 3.7 %
Nickel, Ni	59.325 - 65.424 %	As Balance
Niobium, Nb (Columbium, Cb)	3.3 - 3.7 %
Titanium, Ti	2.3 - 2.7 %
Tungsten, W	3.3 - 3.7 %
Zirconium, Zr	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 go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
Crucible Compaction Metals Rene Supersolvus Rene 95 Nickel Based Superalloy
Techmer ES Luriblend® POM CO AF15
Bohler-Uddeholm UDDEHOLM ALVAR 14 Hot Work Tool Steel
ATI Allvac® WASPALOY® Nickel Superalloy, Heat Treatment: 1010°C (1850°F) + Age
Hexcel® HexPly® 913 125°C Curing Epoxy Matrix

NCRUC101 / 16065

	Advertise with MatWeb!
	Data sheets for over 180,000 metals, plastics, ceramics, and composites.
	HOME • SEARCH • TOOLS • SUPPLIERS • FOLDERS • ABOUT US • FAQ • LOG IN

System Message