发明名称 GAS TURBINE INLET FLOW STRAIGHTENER
摘要 <p>A radial inlet assembly comprising a radial inlet adapted to be in fluid communication with a compressor, and a restricting member covering the radial inlet and receiving a circumferentially asymmetric airflow, the restricting member partially blocking the airflow around the radial inlet, the restricting member blocking a greater portion of the airflow where the airflow is greater to circumferentially redistribute the airflow in a more symmetric manner in the radial inlet.</p>
申请公布号 CA2498459(C) 申请公布日期 2013.07.23
申请号 CA20052498459 申请日期 2005.02.25
申请人 PRATT & WHITNEY CANADA CORP. 发明人 LEBLANC, ANDRE
分类号 F02C7/04;F02C1/00;F02C3/13;F02C7/042;F02C7/055;F02C9/18;F15D1/00 主分类号 F02C7/04
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