Filtration system for gas turbines

FILTRATION SYSTEM FOR GAS TURBINES A system (10) for use with an inlet of a gas turbine through which an airflow toward the gas turbine proceeds is provided and includes a first self-cleaning stage 5 (50) to remove dust, snow and ice from the airflow, a second water tight stage (60), disposed downst...

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Bibliographic Details
Main Authors KIPPEL, BRADLY AARON, CLOAREC, SEBASTIEN, CLEMENTS, JACK THOMAS, MALIVERNAY, MARC, AMMANN, LISA KAMDAR, HINER, STEPHEN DAVID, GANDIA, LIBERTO, CHILLAR, RAHUL JANKARAN, WALTERS, MARCUS CARR
Format Patent
LanguageEnglish
Published 26.03.2015
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
SEPARATION
TRANSPORTING
WEAPONS
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Summary:FILTRATION SYSTEM FOR GAS TURBINES A system (10) for use with an inlet of a gas turbine through which an airflow toward the gas turbine proceeds is provided and includes a first self-cleaning stage 5 (50) to remove dust, snow and ice from the airflow, a second water tight stage (60), disposed downstream from the first stage (50), to prevent aerosol droplets and aqueous solutions of deliquesced particulates, which include at least portions of the dust not removed by the first stage (50) and which are re-released into the airflow from the first stage (50), from proceeding along the airflow and to remove solid 10 particulates not removed by the first stage (50) from the airflow, and a third water removal stage, disposed downstream from the second stage, to remove from the airflow aerosol droplets leaking from the second stage. K~i~ 81 WI 21 11-1D1E
Bibliography:Application Number: AU20090208093