A turboelectric distributed propulsion based on brushless doubly-fed machines (BDFMs) is provided, which minimizes power conversion, enhances mechanical reliability, and strengthens fault-tolerance capability of a DC-based propulsion system. A turboelectric distributed propulsion (TeDP) architecture using BDFMs for aviation applications, and a designed BDFM, inverter, and controller are provided. Simulations and systems are also provided.
INDEPENDENT SPEED VARIABLE FREQUENCY GENERATOR FOR MORE ELECTRIC AIRCRAFT USING BRUSHLESS DOUBLY-FED MACHINES (BDFM)
2021-12-09
Patent
Electronic Resource
English
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