Product Description
A precipitation hardenable nickel-base super-alloy with an exceptional combination of high temperature mechanical properties, corrosion resistance and forgeability characteristics. Developed for use in the 1400–1700°F (760–927°C) temperature range, the alloy has excellent structural stability and unusually good fabricability. Primary application is blading for aircraft and land-based gas turbines.
STANDARD PRODUCT FORMS
Forging bar.
MAJOR SPECIFICATIONS
PDS 15125A1
LIMITING CHEMICAL COMPOSITION, %
Limiting
C .......0.02 – 0.06
Cr ......18.0 – 20.0
Co .....11.0 – 14.0
Mo .........5.5 – 7.0
Ti ........2.9 – 3.25
Al ...........1.8 – 2.3
W ...........0.8 – 1.2
B ...0.004 – 0.010
Ni ............Balance
C .......0.02 – 0.06
Cr ......18.0 – 20.0
Co .....11.0 – 14.0
Mo .........5.5 – 7.0
Ti ........2.9 – 3.25
Al ...........1.8 – 2.3
W ...........0.8 – 1.2
B ...0.004 – 0.010
Ni ............Balance
PHYSICAL CONSTANTS AND THERMAL PROPERTIES
Density, Ib/in3 ........................................................................0.297
g/cm3 .........................................................................8.21
Melting Range, °F ...................................................2300 – 2560
°C ...................................................1260 – 1405
g/cm3 .........................................................................8.21
Melting Range, °F ...................................................2300 – 2560
°C ...................................................1260 – 1405
TYPICAL MECHANICAL PROPERTIES

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SHANGHAI KANGSHENG AVIATION MATERIALS TECHNOLOGY CO., LTD.
Address: No. 5999, Huyi Road, Waigang Town, Jiading District, Shanghai
Tel:13641813331
Technical support:13671903676
Emial:ksalloy@ksalloy.com
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