FIELD: reconditioning of corroded parts made of superalloy or high-temperature steel, for instance, members of gas turbine, particular, gas turbine blades whose surfaces show products of corrosion. SUBSTANCE: the offered method of reconditioning corroded parts from superalloy or high-temperature steel with products of corrosion on their surfaces includes preliminary cleaning of the surfaces from products of corrosion, particular, by chemical and/or mechanical method and subsequent treatment by application of aluminum coating to cleaned surface and its removal with products of corrosion, particular, by chemical and/or mechanical method. EFFECT: higher efficiency. 22 cl, 3 dwg , 1 tbl
Title |
Year |
Author |
Number |
COVERING FOR TURBINE BLADES |
2005 |
|
RU2362832C2 |
PROTECTIVE LAYER FOR PROTECTING PART AGAINST CORROSION, OXIDATION, AND THERMAL OVERLOADING, AND METHOD OF PREPARATION THEREOF |
1995 |
- Shmitts Fridkhel'M
- Chekh Norbert
|
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2011 |
- Menjue,Zhjustin
- Mali,Andre,Juber,Lui
|
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1996 |
|
RU2165478C2 |
METHOD FOR PROTECTION OF PARTS FROM HIGH-TEMPERATURE CORROSION AND PART PROTECTED WITH THE SAID METHOD |
2007 |
- Uolker Pol Meht'Ju
- Uajtkherst Mik
|
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2018 |
- Saboundji, Amar
- Jaquet, Virginie
|
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2018 |
- Saboundji, Amar
- Jaquet, Virginie
|
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2010 |
|
RU2521924C2 |
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2008 |
- Karlen Maksim
- Lans'O Ljusi
- Le Ehnanff Filipp
|
RU2489513C2 |
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|
RU2334022C2 |