A METHOD FOR CLEANING A STATIONARY GAS TURBINE UNIT DURING OPERATION

A cleaning fluid is sprayed into the air inlet channel at a point where the air velocity is at least 40 % of the velocity at the compressor inlet. The gas turbine unit comprises a turbine and a compressor driven by the latter. The air inlet channel for the unit is located upstream from the air inlet...

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Bibliographic Details
Main Authors ASPLUND, PETER, HJERPE, CARL-JOHAN
Format Patent
LanguageEnglish
French
German
Published 07.09.2005
Edition7
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:A cleaning fluid is sprayed into the air inlet channel at a point where the air velocity is at least 40 % of the velocity at the compressor inlet. The gas turbine unit comprises a turbine and a compressor driven by the latter. The air inlet channel for the unit is located upstream from the air inlet channel for the compressor and has a section which is tapered in the direction of the compressor air inlet.
Bibliography:Application Number: EP20030759149