The present invention relates to a rotary wing aircraft 100 that extends along a roll axis R between a nose region 101 and an aft region 102, comprising: at least one first single-blade rotor 120 and at least one second single-blade rotor 130 which are spaced apart from each other along the roll axis; at least one first electric machine and at least one second electric machine which are at least configured to drive in motor mode the at least one first single-blade rotor 120 and the at least one second single-blade rotor 130 for generating lift in hover condition of the rotary wing aircraft; at least one propulsion device 140 that is at least configured to generate forward thrust in forward flight condition of the rotary wing aircraft; and a fixed-wing arrangement 150 that is at least configured to provide lift in the forward flight condition.
A ROTARY WING AIRCRAFT WITH AT LEAST TWO ROTORS AND A PROPULSION UNIT
EIN DREHFLÜGELFLUGZEUG MIT WENIGSTENS ZWEI ROTOREN UND EINER ANTRIEBSEINHEIT
UN AÉRONEF À VOILURE TOURNANTE AVEC AU MOINS DEUX ROTORS ET UNE UNITÉ DE PROPULSION
2024-07-10
Patent
Electronic Resource
English
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