METHOD OF PROTECTING GAS TURBINE PARTS FROM NICKEL ALLOYS Russian patent published in 2012 - IPC C23C14/06 

Abstract RU 2452793 C1

FIELD: metallurgy.

SUBSTANCE: proposed method comprises sequential deposition in vacuum of first layer of condensed coat from nickel alloy on part outer surface and second aluminium-based layer to be annealed in vacuum. Said first layer contains the following elements, in wt %: chromium - 6-12.0, aluminium - 6-12.0, yttrium - 0.1-0.15, tantalum - 1.5-8.0, rhenium -0.3-2.5, hafnium - 0.2-1.5, nickel making the rest.

EFFECT: higher heat resistance at operating temperatures.

4 tbl, 3 ex

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RU 2 452 793 C1

Authors

Budinovskij Sergej Aleksandrovich

Mubojadzhjan Sergej Artemovich

Kos'Min Artem Aleksandrovich

Dates

2012-06-10Published

2011-06-22Filed