The present invention relates to a vertical take-off and landing type hybrid drone comprising: a pair of front rotary rotors, which are formed on a fixed blade, perform a vertical rotation operation so that vertical taking-off and landing are performed, and respectively perform independent control in order to control the rockshaft of the drone; a rear rotary rotor which is formed on a tail wing and which provides propulsion during flight of the drone; a dual receiver for receiving a plurality of flight control signals; and a rotor control unit for analyzing the plurality of flight control signals transmitted from the dual receiver, and controlling the driving of the front and rear rotary rotors by selecting the flight control signal having a small error.

    La présente invention concerne un drone hybride du type à décollage et atterrissage verticaux comprenant : une paire de rotors rotatifs avant, qui sont formés sur une lame fixe, effectuent une opération de rotation verticale de telle sorte que des décollages et atterrissages verticaux sont effectués, et effectuent respectivement une commande indépendante afin de commander l'axe du drone ; un rotor rotatif arrière qui est formé sur une aile arrière et qui fournit une propulsion pendant le vol du drone ; un double récepteur pour recevoir une pluralité de signaux de commande de vol ; et une unité de commande de rotor pour analyser la pluralité de signaux de commande de vol transmis par le double récepteur, et commander l'entraînement des rotors rotatifs avant et arrière en sélectionnant le signal de commande de vol ayant une petite erreur.

    본 발명은 수직 이착륙형 하이브리드 드론에 관한 것으로, 고정익에 구성되고, 수직 이착륙이 이루어지도록 상,하 회전 작동을 하며, 드론의 요축 제어를 위해 각각 독립적인 제어가 이루어지는 한 쌍의 전방 회전로터; 꼬리날개에 구성되며, 상기 드론의 비행시 추진력을 제공하는 후방 회전로터; 복수의 비행 제어 신호를 수신받는 듀얼 수신기; 상기 듀얼 수신기로부터 전송되는 상기 복수의 비행 제어 신호를 분석하고, 에러가 적은 비행 제어 신호를 선별하여 상기 전방 및 후방 회전로터의 구동을 제어하는 로터 제어부;를 포함하는 것을 특징으로 한다.


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    Titel :

    VERTICAL TAKEOFF AND LANDING TYPE HYBRID DRONE


    Weitere Titelangaben:

    DRONE HYBRIDE DU TYPE À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
    수직 이착륙형 하이브리드 드론


    Beteiligte:
    KIM MU SEON (Autor:in)

    Erscheinungsdatum :

    2020-06-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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



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