发明名称 Method of heating gas turbine inlet
摘要 <p>METHOD OF HEATING GAS TURBINE INLET An air inlet system delivers a flow of air. The system included a temperature controlling section configured to alter temperature of the air flow. The temperature controlling section imparts a temperature variation distribution across different portions of the air flow. The system also includes a transition section, one or more flow diverters, one or more screens and/or a flow splitter to cause mixing of the different, temperature variant portions of the air flow and reduce the temperature variation distribution. Fig. 2</p>
申请公布号 AU2012232951(A1) 申请公布日期 2013.05.02
申请号 AU20120232951 申请日期 2012.09.28
申请人 GENERAL ELECTRIC COMPANY 发明人 RAJESH, PRABHAKARAN SARASWATHI;CHILLAR, RAHUL JAIKARAN;KIPPEL, BRADLEY AARON;CONRAD, RICKY DARYL
分类号 F02C7/04;F02C7/042 主分类号 F02C7/04
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