An aircraft (100) includes a body (10) and an outer frame (1) rotatably coupled to the body (10). The body (10) includes a plurality of rotary blades (15a-15d) and a driver (14a-14d) configured to rotate the plurality of rotary blades (15a-15d). The outer frame (1) includes a rotary frame (la-lc) rotatable about a rotation axis intersecting the direction of gravity, and a center of gravity of the plurality of rotary blades (15a-15d) and the driver (14a-14d) is located lower than the rotation axis in the direction of gravity.

    Un aéronef (100) comprend un corps (10) et un cadre externe (1) couplé rotatif au corps (10). Le corps (10) comprend une pluralité de lames rotatives (15a-15d) et un dispositif d'entraînement (14a-14d) configuré pour faire tourner la pluralité de lames rotatives (15a-15d). Le cadre externe (1) comprend un cadre rotatif (la-lc) pouvant tourner autour d'un axe de rotation croisant la direction de la gravité, et un centre de gravité de la pluralité de lames rotatives (15a-15d) et le dispositif d'entraînement (14a-14d) est situé plus bas que l'axe de rotation dans la direction de la gravité.


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    Title :

    AIRCRAFT, FLIGHT SYSTEM, AND STRUCTURE INSPECTION SYSTEM


    Additional title:

    AÉRONEF, SYSTÈME DE VOL ET SYSTÈME D'INSPECTION DE STRUCTURE


    Contributors:

    Publication date :

    2019-08-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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