GH163 based on cobalt nickel - chromium - base, aluminium sheet, titanium aging strengthened alloy, under 800 ℃ has high yield strength and creep strength, strain aging crack tendency is small, thermal fatigue performance is good, and a satisfactory formability and weldability, the alloy is mainly used for aviation engine combustion chamber and reheater components. We can supply plate, bar, forging, ring, pipe and strip, etc.



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