GH3030 / Nimonic 75 Sheet High Temp Alloy for Turbine Engine Combustor Components

Physical properties

>Density (g/cm³): 8.4

>Melting point (): 1374~1420

Application: This alloy be used for turbine engine combustor components operating below 800 degrees Celsius and in 1100 degrees Celsius under load requirements antioxidant but small high temperature components

Feature: At 800 degrees Celsius with a satisfactory heat resistance and high ductility, and has good resistance to oxidation, thermal fatigue, cold stamping and welding performance. For single-phase austenitic alloys course after solution treatment and stable organization.

Description:

Chemical composition(%)

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