METHOD TO REPAIR GAS TURBINE ENGINE BLADES Russian patent published in 2009 - IPC B23P6/00 

Abstract RU 2367554 C2

FIELD: process engineering.

SUBSTANCE: proposed method comprises cleaning blade air-foil portion and blade attachment of operational pollution, hot isostatic pressing of blades with attachments protected against oxidation, removing the protective coat remnants and high-temperature oxidation and sulfide corrosion products in potassium bifluoride melt and by leaching. It comprises also thermal treatment in vacuum and application of protective heat-resistant coat on outer and inner surfaces on blade air-foil portion.

EFFECT: reduced labor input in repair, higher reliability of repaired blades.

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RU 2 367 554 C2

Authors

Poklad Valerij Aleksandrovich

Ospennikova Ol'Ga Gennadievna

Orlov Mikhail Romanovich

Shkretov Jurij Pavlovich

Terekhin Andrej Mikhajlovich

Minakov Aleksandr Ivanovich

Dates

2009-09-20Published

2007-11-08Filed