NOZZLE AND METHOD FOR WASHING GAS TURBINE COMPRESSORS
A method for cleaning a gas turbine unit. The invention further relates to a nozzle for use in washing the gas turbine unit. The nozzle is arranged to atomize a wash liquid in the air stream in an air intake of the gas turbine unit and comprises a nozzle body comprising an intake end for intake of s...
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Main Authors | , |
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Format | Patent |
Language | English Slovenian |
Published |
31.10.2009
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Subjects | |
Online Access | Get full text |
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Abstract | A method for cleaning a gas turbine unit. The invention further relates to a nozzle for use in washing the gas turbine unit. The nozzle is arranged to atomize a wash liquid in the air stream in an air intake of the gas turbine unit and comprises a nozzle body comprising an intake end for intake of said wash liquid and outlet end for exit of said wash liquid. The nozzle further comprises a number of orifices that are connected to the outlet end and respective orifice is arranged at a suitable distance from a center axis of said nozzle body, whereby the local density of the injected wash liquid in a desired area can be increased with preserved droplet size and thereby the efficiency of the cleaning process can be significantly improved at the same time as the risk for damaging the components in the gas turbine unit is significantly reduced. |
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AbstractList | A method for cleaning a gas turbine unit. The invention further relates to a nozzle for use in washing the gas turbine unit. The nozzle is arranged to atomize a wash liquid in the air stream in an air intake of the gas turbine unit and comprises a nozzle body comprising an intake end for intake of said wash liquid and outlet end for exit of said wash liquid. The nozzle further comprises a number of orifices that are connected to the outlet end and respective orifice is arranged at a suitable distance from a center axis of said nozzle body, whereby the local density of the injected wash liquid in a desired area can be increased with preserved droplet size and thereby the efficiency of the cleaning process can be significantly improved at the same time as the risk for damaging the components in the gas turbine unit is significantly reduced. |
Author | HJERPE CARL-JOHAN ASPLUND PETER |
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Discipline | Medicine Chemistry Sciences |
DocumentTitleAlternate | Ĺ oba in postopek pranja plinsko turbinskega kompresorja |
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Notes | Application Number: SI20040031193T |
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PublicationDate_xml | – month: 10 year: 2009 text: 20091031 day: 31 |
PublicationDecade | 2000 |
PublicationYear | 2009 |
RelatedCompanies | GAS TURBINE EFFICIENCY AB |
RelatedCompanies_xml | – name: GAS TURBINE EFFICIENCY AB |
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Snippet | A method for cleaning a gas turbine unit. The invention further relates to a nozzle for use in washing the gas turbine unit. The nozzle is arranged to atomize... |
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SubjectTerms | APPLYING LIQUIDS OR OTHER FLUENT MATERIALS TO SURFACES, IN GENERAL ATOMISING APPARATUS BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NOZZLES PERFORMING OPERATIONS SPRAYING APPARATUS SPRAYING OR ATOMISING IN GENERAL STEAM ENGINES TRANSPORTING WEAPONS |
Title | NOZZLE AND METHOD FOR WASHING GAS TURBINE COMPRESSORS |
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