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    • 144. 发明专利
    • Turbine exhaust diffuser
    • 涡轮排气歧管
    • JP2014013037A
    • 2014-01-23
    • JP2013120421
    • 2013-06-07
    • General Electric Co ゼネラル・エレクトリック・カンパニイ
    • MOORTHI SUBRAMANIYAN
    • F01D25/30F02C7/00
    • F01D5/145F01D25/30
    • PROBLEM TO BE SOLVED: To provide turbine exhaust diffuser components for boundary layer flow control.SOLUTION: A turbine exhaust diffuser 26 includes a diffuser component disposed within the turbine exhaust diffuser and having an outer surface. The turbine exhaust diffuser also includes a suction path extending between the outer surface and an interior compartment of the diffuser component, the suction path configured to ingest a fluid. The turbine exhaust diffuser further includes an actuating path extending between the outer surface and the interior compartment of the diffuser component, the actuating path configured to expel the fluid. The turbine exhaust diffuser further includes a flow manipulating device disposed within the interior compartment of the diffuser component.
    • 要解决的问题:提供用于边界层流量控制的涡轮机排气扩散器部件。解决方案:涡轮机排气扩散器26包括设置在涡轮机排气扩散器内并具有外表面的扩散器部件。 涡轮排气扩散器还包括在扩散器部件的外表面和内部隔室之间延伸的吸入路径,该吸入路径被配置为摄取流体。 涡轮排气扩散器还包括在扩散器部件的外表面和内部隔间之间延伸的致动路径,致动路径被配置成排出流体。 涡轮排气扩散器还包括设置在扩散器部件的内部隔室内的流动操纵装置。