The aircraft (10) includes: at least one electric motor (135); at least one stand-alone electrical power supply (110, 120) supplying power to the electric motor; propulsion elements (130) referred to as “auxiliary propulsion elements”, included in the group including: a stand-alone electrical power supply (130) supplying power to the electric motor, a power supply converting thermal energy into electrical energy and supplying power to the electric motor, and an internal combustion engine; and a structure (100) configured to integrate each electric motor, each stand-alone electrical power supply and the auxiliary propulsion elements, the parameters of the structure being substantially identical regardless of the auxiliary propulsion elements. A method of fitting out such an aircraft is also described.
Aéronef et procédé d'aménagement d'un tel aéronef
Aircraft and method for arranging such an aircraft
Luftfahrzeug und Verfahren zur Ausstattung eines solchen Luftfahrzeugs
2019-09-04
Patent
Electronic Resource
French
PROCÉDÉ ET DISPOSITIF D'AMÉNAGEMENT D'UNE SOUTE AVIONIQUE EN POINTE-AVANT D'UN AÉRONEF
European Patent Office | 2017
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