Compressor system and methods for reducing cooling airflow

Details Compressor system and methods for reducing cooling airflow Compressor system and methods for reducing cooling airflow

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/143 (2006.01) F01D 9/06 (2006.01) F02C 3/13 (2006.01) F02C 7/18 (2006.01)

Patent

CA 2299148

A cooling airflow compressor system and methods for reducing a cooling airflow is described. The cooling airflow compressor system utilizes a primary high pressure compressor in combination with a secondary high pressure compressor to further compress a primary airflow. The secondary high pressure compressor includes a rotor driven by a high pressure turbine connected by a high pressure turbine shaft to the primary high pressure compressor. A heat exchanger is connected to the secondary high pressure compressor to further cool the cooling airflow. The cooling airflow is utilized to cool the turbine and a high pressure turbine vane.

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