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
2020-08-12
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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