A system, apparatus, and/or method for an aircraft that provides a novel independent-speed variable-frequency generator for aviation power generation. The generator architecture utilizes a 2-stage generator architecture with a wound rotor PM exciter (PME) that provides excitation to the rotor of a generator. A rotating bi-directional AC/DC/AC electric power converter connects the rotor windings of the exciter and the generator.
Architecture for an electric power generator for aviation
2025-06-17
Patent
Electronic Resource
English
ARCHITECTURE FOR AN ELECTRIC POWER GENERATOR FOR AVIATION
European Patent Office | 2023
|The Aviation Weather Products Generator
British Library Conference Proceedings | 1993
|Nuclear power aviation electric propulsion system for long-endurance aircraft and aviation aircraft
European Patent Office | 2024
|