It is disclosed a distributed electric propulsion fixed-wing aircraft comprising a plurality of propulsive units, wherein propulsive units are arranged symmetrically with respect to the longitudinal plane, wherein of propulsive units comprises first propulsive units at a first side of the longitudinal plane and second propulsive units at a second side of the longitudinal plane, wherein the distributed propulsion aircraft further comprises a control unit configured to provide a yawing moment so that a sideslip angle is generated, so that the distributed electric propulsion aircraft flies as a fixed-wing aircraft equipped with a single propeller.
DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT SIMULATING A SINGLE PROPELLER AIRCRAFT
FLUGZEUG MIT VERTEILTEM ELEKTRISCHEN ANTRIEB, DAS EIN FLUGZEUG MIT EINEM EINZIGEN PROPELLER SIMULIERT
AVION À PROPULSION ÉLECTRIQUE DISTRIBUÉE SIMULANT UN AVION À HÉLICE UNIQUE
2024-12-11
Patent
Electronic Resource
English
DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT SIMULATING A SINGLE PROPELLER AIRCRAFT
European Patent Office | 2021
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