The present invention provides a launching apparatus for a drone, which launches a drone to a predetermined position or a predetermined altitude. The launching apparatus for a drone includes: a canister including a drone chamber and a gas chamber providing gas pressure of compressed gas, wherein the drone chamber is formed in a cylindrical shape with a predetermined length and mounted for the drone to be launched; a gas supply unit providing the gas pressure of the compressed gas by being mounted on the gas chamber of the canister; and a sealing unit installed in the canister and dividing the drone chamber and the gas chamber in a sealing state, wherein the sealing unit is formed of a flexible material. The sealing unit discharges the drone from the canister by transmitting the gas pressure provided by the gas supply unit while the sealing unit supports the drone.

    드론을 소정의 고도나 위치로 발사하는 드론 발사장치를 제시하며, 소정의 길이를 갖는 원통형으로 형성되어 상기 드론이 발사 가능하게 탑재되는 드론챔버와, 압축가스의 가스압력이 제공되는 가스챔버가 마련되는 캐니스터; 상기 캐니스터의 가스챔버에 장착되어 압축가스의 가스압력을 제공하는 가스공급부; 및 상기 캐니스터의 내부에 마련되어 상기 드론챔버와 상기 가스챔버를 밀봉상태로 구획하고, 유연성을 갖는 소재로 형성되어 상기 드론을 지지하면서 상기 가스공급부에서 제공되는 가스압력을 전달하여 상기 드론을 상기 캐니스터에서 배출시키는 씰링부를 포함한다.


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    Title :

    DRONE LAUNCH APPARATUS


    Additional title:

    드론 발사장치


    Contributors:

    Publication date :

    2023-11-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



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