Fast hybrid helicopter with large range

The helicopter (1) has a lift rotor provided with blades (11) arranged at top of a central fuselage (2), and a support lift surface (20) provided with half wings (21, 22). A mechanical interconnection system mechanically interconnects the rotor and propellers (31, 32) of the wings. The surface (20)...

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Bibliographische Detailangaben
1. Verfasser: FERRIER, JEAN-JACQUES
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:The helicopter (1) has a lift rotor provided with blades (11) arranged at top of a central fuselage (2), and a support lift surface (20) provided with half wings (21, 22). A mechanical interconnection system mechanically interconnects the rotor and propellers (31, 32) of the wings. The surface (20) is arranged at rear of the helicopter between a turning rotor strut and a rear end (4) of the fuselage, where the helicopter is equipped with a self-leveling surface (50) arranged at a level of a front end (3) of the fuselage.