The present invention discloses a multi-rotor aircraft with a multi-axis misalignment layout, which comprises a frame (10), a plurality of upper power sources (20), a plurality of lower power sources (30), a plurality of upper propellers (40), and a plurality of lower propellers (50). The plurality of upper propellers (40) are provided at intervals and are connected to the upper part of the frame (10) through the plurality of upper power sources (20). The plurality of lower propellers (50) are provided at intervals and are connected to the lower part of the frame (10) through the plurality of lower power sources (30). In the vertical projection direction of the frame (10), the plurality of upper propellers (40) and the plurality of lower propellers (50) are staggered. The upper propellers (40) and the lower propellers (50) are staggered so that the pitch between the upper propellers (40) and the lower propellers (50) is large. The central axis of the upper power sources (20) and the central axis of the lower power sources (30) are not collinear or overlapped. In the vertical projection direction of the frame (10), the overlapping area between the upper propellers (40) and the lower propellers (50) is less. Compared with the multi-rotor aircraft in the prior art, the multi-rotor aircraft with the multi-axis misalignment layout can significantly reduce flight resistance and volume, and improve propeller efficiency at the same load capacity.


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    Titel :

    MULTI-ROTOR AIRCRAFT WITH MULTI-AXIS MISALIGNMENT LAYOUT


    Weitere Titelangaben:

    MEHRROTORFLUGZEUG MIT MEHRACHSIGER AUSRICHTUNGSANORDNUNG
    AÉRONEF À ROTORS MULTIPLES À CONFIGURATION D'ALIGNEMENT MULTI-AXES


    Beteiligte:
    TIAN YU (Autor:in)

    Erscheinungsdatum :

    29.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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