
Título
Analysis of Interleaved Input-Parallel Output-Parallel Dual-Active-Bridge Converter for More Electric AircraftAutor-a
Fecha de publicación
2021Grupo de investigación
Accionamientos aplicados a la tracción y a la generación de energía eléctricaOtras instituciones
IkerlanVersión
PostprintTipo de documento
Contribución a congresoContribución a congresoIdioma
engDerechos
© 2021 IEEEAcceso
Acceso embargadoFin de la fecha de embargo
2024-02-29Versión de la editorial
https://doi.org/10.1109/VPPC53923.2021.9699172Publicado en
IEEE Vehicle Power and Propulsion Conference (VPPC) 25-28 October, 2021Editorial
IEEEPalabras clave
Analytical models
Power system measurementS
Density measurement
Atmospheric modeling ... [+]
Power system measurementS
Density measurement
Atmospheric modeling ... [+]
Analytical models
Power system measurementS
Density measurement
Atmospheric modeling
Capacitors
Modulation
Voltage [-]
Power system measurementS
Density measurement
Atmospheric modeling
Capacitors
Modulation
Voltage [-]
Resumen
Dual-Active-Bridge (DAB) converter is one of the most proposed topologies when considering DC/DC bidirectional isolated power conversion. In these applications, the power density of the converter is o ... [+]
Dual-Active-Bridge (DAB) converter is one of the most proposed topologies when considering DC/DC bidirectional isolated power conversion. In these applications, the power density of the converter is one of the main optimization goals. To improve power density, interleaved Input-Parallel Output-Parallel (IPOP) DAB configurations are analyzed in this paper. This configuration helps to reduce voltage and current ripple in input and output capacitors, whose contribution in the converter volume and weight is critical in aircraft applications. To this aim, an analytical model to determine the voltage and current waveforms in these components is proposed in this work. These equations are validated through a simulation model developed in PLECS. Finally, a comparison is presented to find the optimal IPOP configuration in a More Electric Aircraft case study. [-]
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