Aircraft engine starter/generator and controller
An aircraft starting and generating system includes a starter/generator that includes a main machine, an exciter, and a permanent magnet generator. The system also includes an inverter/converter/controller that is connected to the starter/generator and that generates AC power to drive the starter/generator in a start mode for starting a prime mover of the aircraft, and that converts AC power, obtained from the starter/generator after the prime mover have been started, to DC power in a generate mode of the starter/generator. The exciter includes a stator and a rotor, and wherein the exciter rotor includes a three-phase AC winding.
1. An aircraft starting and generating system, comprising: a starter/generator that includes a main machine, an exciter, and a permanent magnet generator; and
an inverter/converter/controller (ICC) that is connected to the starter/generator and that generates AC power to drive the starter/generator in a start mode for starting a prime mover of the aircraft, and that converts AC power, obtained from the starter/generator after the prime mover have been started, to DC power in a generate mode of the starter/generator, the ICC including a contactor,
wherein the exciter includes a stator and a rotor, and wherein the exciter stator includes a winding that is configured to work conjunctionally with the contactor to function as an AC winding during the start mode, and that is configured to work conjunctionally with the contactor as a DC winding during the generate mode.
2. The aircraft starting and generating system according to claim 1 , wherein the inverter/converter/controller comprises:
a main insulated-gate bipolar transistor (IGBT) bridge that is connected to a main stator of the main machine; and
an exciter insulated-gate bipolar transistor (IGBT) Bridge that is connected to an exciter stator of the exciter.
3. The aircraft starting and generating system according to claim 1 , wherein the starter/generator further comprises:
a full wave or half-wave rectifier,
wherein the exciter includes an exciter rotor and an exciter stator, and
wherein the full wave or half wave rectifier is provided on a shaft of the exciter rotor, and rotates with rotation of the exciter shaft.
4. The aircraft starting and generating system according to claim 2 , wherein the contactor provides connection of the exciter insulated-gate bipolar transistor (IGBT) bridge with the exciter stator during the start mode.