Title :
A very high speed switched-reluctance starter-generator for aircraft engine applications
Author :
MacMinn, Stephen R. ; Jones, William D.
Author_Institution :
General Electric Co., Schenectady, NY, USA
Abstract :
An electric direct-drive gearless starter-generator has been designed and built for an aircraft engine application. The system is based on a switched-reluctance motor, which was chosen for its simplicity, robustness, high-speed capability, and efficiency. The overall system configuration and the design of the switched-reluctance motor and its solid-state power converter are described. When operating as engine starter, the motor produces torque to spin the engine up to its light-off speed. Following light-off, the motor continues to produce torque to assist the engine in accelerating to idle speed. When the engine is running, the machine generates electrical power to supply engine and vehicle loads up to a peak operating speed of 50000 r/min. Key issues in the machine design are reliability, high speed, power density, and cost. Test results have verified that the system can meet the torque and generated-power requirements over its entire operating range
Keywords :
aircraft instrumentation; electric generators; reluctance motors; aircraft engine applications; cost; direct-drive gearless starter-generator; efficiency; engine starter; generated-power requirements; high speed switched-reluctance starter-generator; high-speed capability; idle speed; jet engine starter; light-off speed; machine design; operating range; power density; reliability; robustness; simplicity; solid-state power converter; switched-reluctance motor; system configuration; torque; Acceleration; Aircraft propulsion; Automotive components; Engines; Power generation; Power supplies; Robustness; Solid state circuits; Switching converters; Torque;
Conference_Titel :
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location :
Dayton, OH
DOI :
10.1109/NAECON.1989.40453
