The invention provides a portable and foldable double-rotor aircraft which is foldable, convenient to carry and suitable for flying in a small zone. The portable and foldable double-rotor aircraft comprises a machine body, two propellers, two control planes and two foot stools symmetrically arranged below the machine body. The two propellers are symmetrically and linearly arranged on the two sides of the machine body through supporting arms respectively. The two control planes are also symmetrically and linearly arranged on the two sides of the machine body though supporting rods respectively. The centers of rotating faces of the two propellers and the two control planes are located on the same vertical plane. The supporting arms can be folded to the machine body through first foldable bases. Two machine arm clamping mechanisms for clamping the supporting arms after the supporting arms are folded are further arranged on the machine body. The supporting rods can also be folded towards the machine body through second foldable bases. Two supporting rod fixing bases for clamping the supporting rods after the supporting rods are folded are further arranged on the second foldable bases.


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    Titel :

    Portable and foldable double-rotor aircraft


    Beteiligte:
    LIAO QILING (Autor:in) / ZUO HAO (Autor:in) / GAO HEYUAN (Autor:in)

    Erscheinungsdatum :

    21.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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