Aircraft powered by hybrid power

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/24 (2006.01)

Patent

CA 2725769

The invention relates to an aircraft powered by hybrid power that comprises: an outer structure (12 to 20); electric equipment (34); internal combustion propulsion means (40); and a means for supplying power to the propulsion means; characterised in that the aircraft further comprises: a plurality of converters for directly converting light energy into electric power (24), arranged on at least a portion of the outer surface of the outer structure; a means (32) for comparing the electric power generated by said converters with the instantaneous consumption of said electric equipment (34); a means (36) for recovering excess electric power if there is any; and a means (38) for supplying said propulsion means (40) with additional power from said excess electric power if there is any.

Aéronef à alimentation en énergie hybride comprenant : - une structure externe (12 à 20), - des équipements électriques (34), - des moyens de propulsion (40) à combustion interne; et - des moyens d'alimentation en énergie des moyens de propulsion, caractérisé en ce qu'il comprend en outre : - une pluralité de convertisseurs directs d'énergie lumineuse en énergie électrique (24), disposés sur au moins une partie de la surface externe de la structure externe; - des moyens (32) pour comparer l'énergie électrique produite par lesdits convertisseurs à la consommation instantanée desdits équipements électriques (34); - des moyens (36) pour récupérer l'énergie électrique excédentaire s'il y en a, et; - des moyens (38) pour fournir auxdits moyens de propulsion (40) un complément d'énergie à partir de ladite énergie électrique excédentaire si elle existe.

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