Patent ID: 11913376
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  Y | IPC F

Claim 3:
4. The method according to claim 1, wherein the stator shroud assembly includes a plurality of pressurized stator vanes, each pressurized stator vane including a stator vane airflow passage therewithin and at least one pressurized airflow nozzle, among the plurality of pressurized airflow nozzles, in fluid communication with the stator vane airflow passage, and, in the directing, the pressurized airflow nozzles of the plurality of pressurized stator vanes direct the flow of pressurized air onto the plurality of rotor vanes of at least one of the plurality of compressor rotors so as to cause the compressor rotor shaft assembly to rotate.