4-MW Class High-Power-Density Generator for Future Hybrid-Electric Aircraft
This article describes the underpinning research, development, construction, and testing of a 4-MW multithree phase generator designed for a hybrid-electric aircraft propulsion system demonstrator. The aim of the work is to demonstrate gravimetric power densities around 20 kW/kg, as required for multi-MW aircraft propulsion systems. The key design choices, development procedures, and tradeoffs, together with the experimental testing of this electrical machine connected to an active rectifier, are presented. A time-efficient analytical approach to the downselection of various machine configurations, geometrical variables, different active and passive materials, and different thermal management options is first presented. A detailed design approach based on the 3-D finite element analysis (FEA) is then presented for the final design. Reduced power tests are carried out on a full-scale 4-MW machine prototype, validating the proposed design. The experimental results are in good agreement with simulation and show significant progress in the field of high-power-density electrical machines at the targeted power rating.
|Título según WOS:||ID WOS:000703376000076 Not found in local WOS DB|
|Título de la Revista:||IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION|
|Editorial:||IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC|
|Fecha de publicación:||2021|
|Página de inicio:||2952|