| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine system having a plasma actuator flow control structure.SOLUTION: In a gas turbine system having a plasma actuator flow control structure including a compressor section for compressing an airstream, the compressor section includes at least one inlet guide vane for controlling the airstream near an inlet portion of the compressor section. In addition, the compressor section also includes a turbine inlet assembly for ingesting the airstream to be routed to the compressor section. Furthermore, the compressor section includes a plasma actuator disposed within at least one of the inlet portion of the compressor section and the turbine inlet assembly for controllably producing an electric field to manipulate a portion of the airstream. |
