Description
UDIMET® alloy R41 (UNS N07041)
Table 1 – Limiting Chemical Composition, %
significant amounts of cobalt and molybdenum, along with lesser amounts of aluminum and titanium. Alloy R41 exhibits extremely high room and elevated temperature mechanical properties. Excellent corrosion resistance and fabricability have led to wide usage in critical aircraft engine components such as nozzle partitions, turbine blades and wheels, combustion chamber liners and structural hardware.
Chromium………………………………………………………. 18.0-20.0
Cobalt……………………………………………………………. 10.0-12.0
Molybdenum……………………………………………………… 9.0-10.5
Aluminum……………………………………………………….. 1.40-1.80
Titanium…………………………………………………………….. 3.0-3.3
Iron…………………………………………………………………. 5.0 max.
Boron………………………………………………………….. 0.003-0.010
Carbon………………………………………………………….. 0.12 max.
Nickel……………………………………………………………… Balance*
Typical Mechanical Properties
Table 3 – 1000-Hour Rupture Strength of Precipitation- Hardened UDIMET alloy R41
*Reference to the ‘balance’ of a composition does not guarantee this is exclusively of the element mentioned but that it predominates and others are present only in minimal quantities.
Physical Constants
Table 2 – Physical Constants
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Density, lb/in3……………………………………………………….. 0.298
g/cm3…………………………………………………………. 8.25
Melting Range, °F………………………………………….. 2250-2535
°C………………………………………….. 1232-1391
Specific Heat, Btu/lb•°F…………………………………………. 0.104
J/kg•°K……………………………………………… 435
Coefficient of Expansion, 70-200°F, 10-6 in/in•°F…………. 6.63
21-93°C, µm/m•°C……………… 11.9
Thermal Conductivity, Btu•in/ft2•h•°F…………………………… 62
W/m•°C……………………………………. 9.0
Available Products and Specifications
UDIMET alloy R41 is designated UNS N07041 and is available as forging billet, bar, sheet and plate.
Major specifications: AMS 5545
AMS 5712
AMS 5713
Figure 1. Typical mechanical properties of precipitation-hardened UDIMET alloy R41
Publication Number SMC-108 Copyright © Special Metals Corporation, 2004 (Sept 04)
UDIMET is a trademark of the Special Metals Corporation group of companies.
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