Gas turbine inlet flow straightener

Details Gas turbine inlet flow straightener Gas turbine inlet flow straightener

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/04 (2006.01) F02C 1/00 (2006.01) F02C 3/13 (2006.01) F02C 7/042 (2006.01) F02C 9/18 (2006.01) F15D 1/00 (2006.01)

Patent

CA 2498459

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.

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