An unmanned aerial vehicle (UAV) according to various embodiments may comprise: a housing; a motor arranged in the inner space of the housing; a rotor which is rotated by the motor, and which comprises at least one cam structure; and at least one landing member which serves as at least a part of the housing, and which selectively protrudes from the housing depending on interference of the cam structure. An unmanned aerial vehicle (UAV) according to various embodiments comprises: a housing; at least one rotor blade arranged in the inner space of the housing; and at least one landing member, wherein the at least one landing member serves as a part of the housing in a closed position and protrudes from the housing in an open position such that the load of the unmanned aerial vehicle can be supported during landing. Other embodiments are also possible.

    L'invention concerne un véhicule aérien sans pilote (UAV) qui, selon divers modes de réalisation, peut comprendre : un boîtier ; un moteur agencé dans l'espace intérieur du boîtier ; un rotor qui est entraîné en rotation par le moteur et qui comprend au moins une structure de came ; et au moins un élément d'atterrissage qui constitue au moins une partie du boîtier et qui fait saillie de manière sélective à partir du boîtier en fonction de l'interférence de la structure de came. Un véhicule aérien sans pilote (UAV), selon divers modes de réalisation, comprend : un boîtier ; au moins une pale de rotor disposée dans l'espace intérieur du boîtier ; et au moins un élément d'atterrissage, l'au moins un élément d'atterrissage constituant une partie du boîtier dans une position fermée et faisant saillie depuis le boîtier dans une position ouverte, de sorte que la charge du véhicule aérien sans pilote puisse être supportée pendant l'atterrissage. D'autres modes de réalisation sont également possibles.

    다양한 실시예에 따르는 무인 비행체(unmanned aerial vehicle; UAV)에 있어서, 하우징; 상기 하우징의 내부 공간에 배치되는 모터; 상기 모터에 의해 회전되며, 적어도 하나의 캠 구조를 포함하는 회전체; 및 상기 하우징의 적어도 일부로 기여되며, 상기 캠 구조의 간섭에 따라 상기 하우징에서 선택적으로 돌출되는 적어도 하나의 랜딩 부재(landing member)를 포함할 수 있다. 다양한 실시예에 따르는 무인 비행체(unmanned aerial vehicle; UAV)에 있어서, 하우징; 상기 하우징의 내부 공간에 배치되는 적어도 하나의 회전 날개(rotor blade); 및 적어도 하나의 랜딩 부재(landing member)를 포함하되, 상기 적어도 하나의 랜딩 부재는, 닫힌 상태(closed position)에서, 상기 하우징의 일부로써 기여되고, 개방 상태(open position)에서, 상기 하우징에서 돌출되어 랜딩 시, 무인 비행체의 하중을 지지할 수 있다. 이 밖의 다른 실시예가 가능하다.


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    Title :

    UNMANNED AERIAL VEHICLE AND METHOD FOR OPERATING SAME


    Additional title:

    VÉHICULE AÉRIEN SANS PILOTE ET SON PROCÉDÉ DE FONCTIONNEMENT
    무인 비행체 및 그의 동작 방법


    Contributors:
    PARK SANG-IL (author) / KIM EUNYOUNG (author)

    Publication date :

    2018-04-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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