
GH3030 has excellent thermal strength and high plasticity below 800 ° C, and has good resistance to oxidation, thermal fatigue, cold stamping, and welding process performance. GH3039 has moderate strength and good thermal fatigue resistance below 800 ° C, good oxidation resistance, and good cold formability and welding performance.
GH3030 is mainly used for combustion chamber components of turbine engines operating below 800 ° C and other high-temperature components that require anti-oxidation but have low load capacity below 1100C.
GH3039 aviation engine combustion chamber and afterburner components.