To provide a multicopter of which weight can be reduced.SOLUTION: A multicopter includes: a body part 3; and a rotor 2 rotated by a motor 20 and generating lift force, where multiple rotors 2 are fitted to the body part 3. The body part 3 has an annular support frame part 10. The rotors 2 are directly or indirectly fitted to the support frame part 10.SELECTED DRAWING: Figure 1


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    Title :

    マルチコプター


    Publication date :

    2021-04-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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