| 摘要 |
A turbomachine 100 includes a compressor 110 configured to compress air received at an intake portion 202 to form a compressed airflow that exits into an outlet portion 204. The compressor has a plurality of rotor blades 112 and a plurality of stator vanes 113, and a compressor casing 111 forming an outer shell of the compressor. A combustor 120 is operably connected with the compressor, and the combustor receives the compressed airflow. A turbine 130 is operably connected with the combustor, and the turbine receives combustion gas flow from the combustor. The turbine has a turbine casing. A cooling system is operatively connected to the compressor casing. The cooling system includes a plurality of heat pipes 250 located in at least a portion of the plurality of stator vanes 113. The heat pipes 250 are configured to be in thermal communication with the compressor casing 111. The heat absorbed by the plurality of heat pipes 250 is transferred to the compressor casing 111. |
