Thèses et travaux de recherche du projet

Thèse 1: S. Touhami, “Analytical Sizing Models to Assess the Performances of High Specific Power Electric Motors for Hybrid Aircraft,” PhD Thesis, Institut National Polytechnique de Toulouse (Toulouse INP), 2020.

Thèse 2: N. Erroui, “Chaine de conversion forte puissance pour la propulsion aéronautique hybride,” PhD Thesis, Insititut National Polytechnique de Toulouse (Toulouse INP), 2019.

Thèse 3: A. Zeaiter, “Thermal modeling and cooling of electric motors application to the propulsion of hybrid aircraft,” PhD Thesis, Ecole Nationale Supérieure de Mécanique et d’Aérotechnique (ENSMA), 2020.

Thèse 4: F. Accorinti, “Two-phase power electronics cooling solution design in air context answer to the objectives of the hybrid aircraft 2035.,” PhD Thesis, Ecole Nationale Supérieure de Mécanique et d’Aérotechnique (ENSMA), 2020.

Thèse 5: P. Collin “Design, taking into account the partial discharges phenomena, of the electrical insulation system (eis) of high power electrical motors for hybrid electric propulsion of future regional aircrafts,” PhD Thesis, Institut National Polytechnique de Toulouse (Toulouse INP), 2020.

Thèse 6: M. Pettes Duler, “Integrated optimal design of a hybrid-electric aircraft powertrain,” PhD Thesis, Institut National Polytechnique de Toulouse (Toulouse INP), 2021.

Post Doc 1: M. Tognan, Battery & Fuel Cell state of the art & metamodels; ‘HASTECS Technical report, 2019.

Post Doc 2: M E Banda, D Malec and JP Cambronne, “Partial discharge (DP) prevention within power converter busbars dedicated to hybrid aircraft propulsion, Hastecs technical report, 2018.