发明申请
US20090324397A1 Gas Turbine Engine With Insulated Cooling Circuit 有权
带绝缘冷却回路的燃气轮机

Gas Turbine Engine With Insulated Cooling Circuit
摘要:
A gas turbine engine is provided comprising a compressor with an insulated cooling circuit. The compressor comprises a compressor casing having a compression chamber and at least one stator and at least one rotor disposed in the compression chamber, the at least one stator comprising a stator body having a plurality of tubes for transporting cooling air through passages in the stator body into the compression chamber. The plurality of tubes are surrounded by an air gap for insulating the tubes from the stator body.
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