A rotorcraft comprising a fuselage, a single main rotor, and a first propeller and a second propeller. The rotorcraft has an adjustment system configured, at least during a stage of hovering flight, to position the first propeller in a first low speed configuration in order to exert a first thrust including a first horizontal component and a first vertical component, the adjustment system being configured, at least during the stage of hovering flight, to position the second propeller in a second low speed configuration so as to exert a second thrust comprising a second horizontal component and a second vertical component.
GIRAVION MUNI D'UNE VOILURE TOURNANTE ET D'AU MOINS DEUX HELICES, ET PROCEDE APPLIQUE PAR CE GIRAVION
ROTORCRAFT PROVIDED WITH A ROTARY WING AND AT LEAST TWO PROPELLERS, AND METHOD APPLIED BY SAID ROTORCRAFT
DREHFLÜGELFLUGZEUG, DAS MIT DREHFLÜGELN UND MINDESTENS ZWEI PROPELLERN AUSGESTATTET IST, UND VON DIESEM DREHFLÜGELFLUGZEUG ANGEWANDTES VERFAHREN
12.08.2020
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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