Aircraft

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/20 (2006.01) B64C 29/00 (2006.01) B64C 39/02 (2006.01) B66F 19/00 (2006.01)

Patent

CA 2476749

The present invention concerns an aircraft having a plurality of lifting and thrust rotors, with an electric motor and an inverter for each motor. In order to provide an aircraft having a greater payload, connecting bars are provided between the motors. In that respect the invention is based on the realisation that, if such connecting bars are arranged in the manner of a latticework, they can provide a light but nonetheless stable structure for the aircraft, and that structure can carry correspondingly greater loads.

L'invention concerne un aéronef comportant une pluralité de rotors de sustentation et de poussée, chaque rotor ayant un moteur électrique pourvu d'un onduleur. L'invention vise à mettre en oeuvre un aéronef offrant une plus grande charge utile. A cet effet, des tiges de connexion sont prévues entre les moteurs. La disposition desdites tiges de connexion sous forme de treillis permet d'obtenir une construction légère et solide de l'aéronef, capable de supporter des charges élevées.

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