发明名称 FILTRATION SYSTEM FOR GAS TURBINES
摘要 A system for use with an inlet of a gas turbine through which airflow toward the gas turbine proceeds is provided and includes a first stage to remove primary aerosol droplets from the airflow by coalescing the primary aerosol droplets into secondary aerosol droplets, which are larger than the primary aerosol droplets, and to remove solid particulates from the airflow, a second water tight stage, disposed downstream from the first stage, to prevent the secondary aerosol droplets and aqueous solutions of deliquesced particulates, which are not removed by the first stage and which are re-released into the airflow from the first stage, from proceeding along the airflow and to remove solid particulates not removed by the first stage from the airflow, and a third water removal stage, disposed downstream from the second stage, to remove from the airflow the remaining secondary aerosol droplets leaking from the first and second stages.
申请公布号 CA2675904(C) 申请公布日期 2013.08.13
申请号 CA20092675904 申请日期 2009.08.20
申请人 GENERAL ELECTRIC COMPANY 发明人 HINER, STEPHEN DAVID;CHILLAR, RAHUL JAIKARAN;KIPPEL, BRADLY AARON;AMMANN, LISA KAMDAR;CLEMENTS, JACK THOMAS;WALTERS, MARCUS CARR;CLOAREC, SEBASTIEN;MALIVERNAY, MARC;GANDIA, LIBERTO
分类号 F02C7/05 主分类号 F02C7/05
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