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Turbine engine and method for flowing air in a turbine engine
Turbine engine and method for flowing air in a turbine engine
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机译:涡轮发动机和使空气在涡轮发动机中流动的方法
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摘要
According to one aspect of the invention, a gas turbine engine includes a combustor, a fuel nozzle placed in an end of the combustor, and a passage configured to receive an air flow from a compressor discharge casing, wherein the passage directs the air flow into a chamber downstream of the nozzle, wherein a chamber pressure is lower than a compressor discharge casing pressure. The gas turbine engine also includes a flow control device configured to control the air flow from the compressor discharge casing into the passage.
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