| 摘要 |
PROBLEM TO BE SOLVED: To provide a system, a method, and an apparatus for controlling gas leakage in a turbine. SOLUTION: A plurality of seals (214) are provided where each of the plurality of seals (214) may be operable to reduce gas backflow pressure from the inlet (212) of a turbine component (202). Further, one or more channels (216) may be operable to direct at least a portion of the gas backflow from respective points within the plurality of seals (214) to corresponding points within a gas flow path of the turbine. COPYRIGHT: (C)2010,JPO&INPIT |
