Alloy 282 is a new, wrought, gamma-prime strengthened superalloy developed for high temperature structural applications, especially those in aero and industrial gas turbine engines. It possesses a unique combination of creep strength, thermal stability, weldability, and fabricability not found in currently available commercial alloys.
The new alloy has excellent creep strength in the temperature range of 1200 to 1700°F (649 to 927°C). The features of Alloy 282 alloy make it suitable for critical gas turbine applications, such as sheet fabrications, seamless and flash butt-welded rings, and cases found in compressor, combustor, and turbine sections. In augmented aircraft gas turbines, the new alloy will be useful for exhaust and nozzle components. In industrial gas turbines, the alloy is a good candidate for transition sections and other hot-gas-path components.
|Physical and Chemical properties|
|Chemical composition||Ni 57 %
Cr 19,5 %
Co 10 %
Mo 8,5 %
Ti 2,1 %
Al 1,5 %
Mn 0,3 %
Fe 1,5 %
C 0,06 %
Si 0,15 %
B 0,005 %
|Physical properties||Density (Solution Annealed)||8.27 g/cm3|
|Density (Age-Hardened)||8,29 g/cm3|
|Mechanical properties||Test Method||As Built||Heat Treated|
The information presented are typical values intended for reference and comparison purposes only. They should not be used for design specifications or quality control purposes.
End-use material performance can be impacted (+/-) by, but not limited to, part design, end-use conditions, etc. Actual values will vary with build conditions.
Product specifications are subject to change without notice.
The performance characteristics of these materials may vary according to application, operating conditions, or end use. Each user is responsible for determining that the material is safe, lawful and technical suitable for the intended laws and regulations. Zare makes no warranties of any kind, express or implied, including, but not limited to, the warranties of merchantability, fitness for a particular use, or warranty against patent infringement. All Trademarks included in this document are property of the respective owner.