METHOD FOR LOCALLY REMOVING OXIDIZED CORROSION PRODUCT FROM SURFACE OF PARTS OF TURBINE ENGINE

PROBLEM TO BE SOLVED: To provide a method for selectively removing combustion product from surface of parts of a gas turbine after the long term exposure in the high temperature oxidizing and corrosive environment of exhaust gas of the gas turbine without affecting metal or film of adjacent substrat...

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Hauptverfasser: FARR HOWARD JOHN, CONNER JEFFREY ALLEN
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creator FARR HOWARD JOHN
CONNER JEFFREY ALLEN
description PROBLEM TO BE SOLVED: To provide a method for selectively removing combustion product from surface of parts of a gas turbine after the long term exposure in the high temperature oxidizing and corrosive environment of exhaust gas of the gas turbine without affecting metal or film of adjacent substrates which are not altered, and a material composition therefor. SOLUTION: Loose contamination is removed from the surface of parts of the gas turbine engine, a moldable reactive metallic composition including more than one kinds of metals having affinity with oxygen selected from the group consisting of Al, Si, Ti and Zr is applied to the corrosion part which is heated to about 1800-2000 deg. F in a non-reactive environment to generate the reaction between the combustion product and the reactive metal. Thereby, the combustion product of the corrosion part on the surface if decomposed to occur a by-product, which is cooled thereafter. The by-product can be removed optionally from the surface of parts.
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SOLUTION: Loose contamination is removed from the surface of parts of the gas turbine engine, a moldable reactive metallic composition including more than one kinds of metals having affinity with oxygen selected from the group consisting of Al, Si, Ti and Zr is applied to the corrosion part which is heated to about 1800-2000 deg. F in a non-reactive environment to generate the reaction between the combustion product and the reactive metal. Thereby, the combustion product of the corrosion part on the surface if decomposed to occur a by-product, which is cooled thereafter. 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SOLUTION: Loose contamination is removed from the surface of parts of the gas turbine engine, a moldable reactive metallic composition including more than one kinds of metals having affinity with oxygen selected from the group consisting of Al, Si, Ti and Zr is applied to the corrosion part which is heated to about 1800-2000 deg. F in a non-reactive environment to generate the reaction between the combustion product and the reactive metal. Thereby, the combustion product of the corrosion part on the surface if decomposed to occur a by-product, which is cooled thereafter. 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SOLUTION: Loose contamination is removed from the surface of parts of the gas turbine engine, a moldable reactive metallic composition including more than one kinds of metals having affinity with oxygen selected from the group consisting of Al, Si, Ti and Zr is applied to the corrosion part which is heated to about 1800-2000 deg. F in a non-reactive environment to generate the reaction between the combustion product and the reactive metal. Thereby, the combustion product of the corrosion part on the surface if decomposed to occur a by-product, which is cooled thereafter. The by-product can be removed optionally from the surface of parts.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record>
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subjects BLASTING
CHEMICAL SURFACE TREATMENT
CHEMISTRY
CLEANING OR DEGREASING OF METALLIC MATERIAL BY CHEMICALMETHODS OTHER THAN ELECTROLYSIS
COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATIONOR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY IONIMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
COATING MATERIAL WITH METALLIC MATERIAL
COATING METALLIC MATERIAL
DIFFUSION TREATMENT OF METALLIC MATERIAL
ENGINE PLANTS IN GENERAL
HEATING
INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METALLURGY
MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLICMATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASSC23 AND AT LEAST ONEPROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION
WEAPONS
title METHOD FOR LOCALLY REMOVING OXIDIZED CORROSION PRODUCT FROM SURFACE OF PARTS OF TURBINE ENGINE
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