发明名称 GAS TURBINE INLET FLOW STRAIGHTENER
摘要 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.
申请公布号 US2005204743(A1) 申请公布日期 2005.09.22
申请号 US20040802828 申请日期 2004.03.18
申请人 LEBLANC ANDRE 发明人 LEBLANC ANDRE
分类号 F02C1/00;F02C3/13;F02C7/04;F02C7/042;F02C7/055;F02C9/18;F15D1/00;(IPC1-7):F02C7/04 主分类号 F02C1/00
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