L'avion plus électrique est un concept qui a le vent en poupe chez les principaux constructeurs du domaine de l'aéronautique. Dans ce domaine, comme dans d'autres, les besoins en énergie électrique sont croissants et nécessitent de mettre en place des systèmes de conversion d'énergie fiables, performants et modulaires. Ces systèmes de conversion sont souvent couplés avec des systèmes de stockage d'énergie (type batterie) permettant dans certaines situations de rendre l'avion énergétiquement autonome grâce à une source de puissance indépendante des principaux organes de production d'énergie. Cette interconnexion batterie - réseau de bord présente un rapport de tension élevé ce qui, ajouté aux fortes valeurs de courant de la basse tension, en fait un objet particulièrement complexe à réaliser.L'objectif de cette thèse est de concevoir de manière optimale un convertisseur de puissance isolé permettant l'interconnexion d'un bus basse tension 28 V (typiquement des batteries) à un bus haute tension 540 V (réseau de bord de l'avion) avec une puissance échangeable d'environ 12 kW. Elle se déroule dans le cadre d'un projet ANR (quatre partenaires universitaires, associés à l'entreprise AIRBUS) dont l'une des tâches est le développement d'outils de conception pour l'électronique de puissance. Le travail correspondant comprend une contribution à cette tâche sous forme de la construction de modèles des principaux composants intervenant dans un convertisseur, modèles destinés à être intégrés dans les routines d'optimisation. Pour cette raison, ils seront analytiques (physique, empiriques, mélange des deux).Ces modèles seront ensuite insérés dans un outil global développé dans une autre thèse du projet, à l'aide duquel différentes architectures de convertisseurs seront comparées afin d'en déduire la meilleure solution pour le cahier des charges énoncé précédemment. Un prototype du convertisseur retenu sera finalement réalisé en utilisant des technologies avancées, pour conduire une validation expérimentale. / The electric aircraft tends to become widespread at all the main manufacturers of the domain of the aeronautics. Needs do not stop growing and require setting up reliable, efficiency and modular systems of conversion of energy. These systems of conversion are often coupled with systems of storage of energy (battery) allowing in certain situations to make the punctually autonomous aircraft energetically thanks to a source of power independent from main organs of power production. This interconnection battery - network of edge presents a very high report of rise of tension what, added to the high current value of the battery bus, in fact a particularly complex object to be realized.The objective of this thesis is to design in an optimal way a converter of power isolated allowing the interconnection of a low-voltage bus 28V (typically batteries) in a high-voltage bus 540V (network of edge of the aircraft) with an exchangeable power about 12 kW. It takes place within the framework of an ANR project (four university partners + AIRBUS) the development of tools of conception of which one of the tasks is for the ENP. The corresponding work includes a contribution to this task in the form of the construction of models of the main components occurring in a converter, model intended to be integrated into the routines of optimization. For that reason, they will be analytical (physical, empirical or mix both).These models will then be inserted into a global tool developed in another thesis of the project, by means of which various architectures of converters will be compared to deduct the best solution from it for the previous specifications. A prototype of the reserved converter will be finally realized by using advanced technologies, to lead an experimental validation.

abstract: This thesis investigates different unidirectional topologies for the on-board charger in an electric vehicle and proposes soft-switching solutions in both the AC/DC and DC/DC stage of the converter with a power rating of 3.3 kW. With an overview on different charger topologies and their applicability with respect to the target specification a soft-switching technique to reduce the switching losses of a single phase boost-type PFC is proposed. This work is followed by a modification to the popular soft-switching topology, the dual active bridge (DAB) converter for application requiring unidirectional power flow. The topology named as the semi-dual active bridge (S-DAB) is obtained by replacing the fully active (four switches) bridge on the load side of a DAB by a semi-active (two switches and two diodes) bridge. The operating principles, waveforms in different intervals and expression for power transfer, which differ significantly from the basic DAB topology, are presented in detail. The zero-voltage switching (ZVS) characteristics and requirements are analyzed in detail and compared to those of DAB. A small-signal model of the new configuration is also derived. The analysis and performance of S-DAB are validated through extensive simulation and experimental results from a hardware prototype. Secondly, a low-loss auxiliary circuit for a power factor correction (PFC) circuit to achieve zero voltage transition is also proposed to improve the efficiency and operating frequency of the converter. The high dynamic energy generated in the switching node during turn-on is diverted by providing a parallel path through an auxiliary inductor and a transistor placed across the main inductor. The paper discusses the operating principles, design, and merits of the proposed scheme with hardware validation on a 3.3 kW/ 500 kHz PFC prototype. Modifications to the proposed zero voltage transition (ZVT) circuit is also investigated by implementing two topological variations. Firstly, an integrated magnetic structure is built combining the main inductor and auxiliary inductor in a single core reducing the total footprint of the circuit board. This improvement also reduces the size of the auxiliary capacitor required in the ZVT operation. The second modification redirects the ZVT energy from the input end to the DC link through additional half-bridge circuit and inductor. The half-bridge operating at constant 50% duty cycle simulates a switching leg of the following DC/DC stage of the converter. A hardware prototype of the above-mentioned PFC and DC/DC stage was developed and the operating principles were verified using the same. / Dissertation/Thesis / Doctoral Dissertation Electrical Engineering 2017