| 摘要 |
PROBLEM TO BE SOLVED: To provide a reliable aircraft engine constant frequency starter/generator.SOLUTION: A constant frequency starter/generator 55 for a turbine engine includes a first inverter/converter 56, a second inverter/converter 60, a DC link 58 electrically connecting the first inverter/converter 56 to the second inverter/converter 60, and an electric machine having a synchronous main machine. The constant frequency starter/generator 55 is operable in a start mode and a run mode. |
