A double-blade tandem helicopter comprising a fuselage (10), a power system, a control system, and two rotor assemblies (30, 50). The rotor assemblies are longitudinally disposed relative to the fuselage. Each rotor assembly comprises a rotor shaft (31, 51), a rotor head (33, 53), and two blades (35, 37, 55, 57). The rotor shaft is connected to the power system, the rotor head is fixed to the rotor shaft, and the blades are attached to the rotor head. The double-blade tandem helicopter has a larger rotor disk area than that of a single-rotor helicopter while has a fuselage weight approaching that of the single-rotor helicopter, and thus has a take off weight approximately twice or more times of the single-rotor helicopter, and meanwhile has characteristics such as small volume, simple structure and high aerodynamic efficiency.


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    Titel :

    DOUBLE-BLADE TANDEM HELICOPTER


    Beteiligte:
    YANG FAN (Autor:in)

    Erscheinungsdatum :

    2022-04-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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