Invention Grant
US08683811B2 Jet engine with compressor air circulation and method for operating the jet engine 有权
具有压缩机空气循环的喷气发动机和用于操作喷气发动机的方法

Jet engine with compressor air circulation and method for operating the jet engine
Abstract:
In a jet engine with compressor air circulation provided for stabilizing the flow conditions, the compressed hot compressor air tapped from the flow path of the compressor (1) is first cooled in the bypass duct (3) and then resupplied to the upstream compressor via line (12). This reduces the thermal load of the blades and improves efficiency.
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