一种航空永磁发电机功率控制系统及方法
By combining inner-loop and outer-loop control strategies with a PI controller, the problems of high load requirements and complex operation in the constant power output control of aircraft permanent magnet generators are solved, achieving efficient and simplified power control and improving the system's dynamic response and power-to-weight ratio.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- SHAANXI AVIATION ELECTRICAL
- Filing Date
- 2025-09-24
- Publication Date
- 2026-07-17
AI Technical Summary
Existing constant power output control methods for aircraft permanent magnet generators have high load requirements, are complex to operate, and are limited by the rated speed of the motor, resulting in reduced efficiency and high maintenance costs.
By employing inner-loop and outer-loop control strategies, combined with a PI controller, Clarke and Park converters, and an SVPWM module, the target power control of the aircraft permanent magnet generator is achieved through phase current detection and motor electrical angle calculation. The magnetic field strength is optimized using a modulation ratio field weakening module, and the sampling conditions are simplified to improve the system power-to-weight ratio.
It achieves efficient power control of aircraft permanent magnet generators under minimal sampling conditions, simplifies the operation process, reduces system complexity and maintenance costs, and improves the system's dynamic response capability.
Smart Images
Figure CN121077307B_ABST