Product Description
A nickel-base alloy solid solution strengthened with tungsten and molybdenum and precipitation hardened with titanium and aluminum. The alloy combines high strength with metallurgical stability, as demonstrated by excellent impact strength retention after long exposures at elevated temperatures. Good oxidation and corrosion resistance combined with high strength make the alloy useful in gas turbine blades and disc applications.
STANDARD PRODUCT FORMS
Forging billet and bar.
MAJOR SPECIFICATIONS
EMS 55477, EMS 73105, MSRR 7252, C50TF105, MTS 5013
LIMITING CHEMICAL COMPOSITION, %
Limiting
Ni ............Balance
Cr ......15.5 – 16.5
Co .....14.0 – 15.5
Mo ....2.75 – 3.25
W ......1.00 – 1.50
Ti ......4.75 – 5.25
Al ......2.25 – 2.75
C .......0.01 – 0.02
Zr ...0.025 – 0.05
B ......0.01 – 0.02
Ni ............Balance
Cr ......15.5 – 16.5
Co .....14.0 – 15.5
Mo ....2.75 – 3.25
W ......1.00 – 1.50
Ti ......4.75 – 5.25
Al ......2.25 – 2.75
C .......0.01 – 0.02
Zr ...0.025 – 0.05
B ......0.01 – 0.02
PHYSICAL CONSTANTS AND THERMAL PROPERTIES
Density, Ib/in3........................................................................0.292
g/cm3 .........................................................................8.08
Melting Range, °F ...................................................2180 – 2440
°C ...................................................1194 – 1338
Coefficient of Expansion, 70 – 200°F, 10-6 in/in • °F........6.8
21 – 93°C, µm/m • °C ..........12.24
g/cm3 .........................................................................8.08
Melting Range, °F ...................................................2180 – 2440
°C ...................................................1194 – 1338
Coefficient of Expansion, 70 – 200°F, 10-6 in/in • °F........6.8
21 – 93°C, µm/m • °C ..........12.24
TYPICAL MECHANICAL PROPERTIES

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Key words:
720
ndash
and
deg
in
with
strength
alloy
2.75
limiting
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