The present invention relates to an operation facility of a rotary wing type unmanned aerial vehicle. the operation facility of a rotary wing type unmanned aerial vehicle comprises: a passage space (30) formed to extend in a vertical direction z and allowing the unmanned aerial vehicle to ascend or descend; and an air pressure control system (40) controlling air pressure in the passage space (30). the air pressure control system (40) controls the air pressure such that the air pressure above the unmanned aerial vehicle is lower than the air pressure below the unmanned aerial vehicle.

    회전날개식 무인항공기의 운용 설비로서, 상하 방향 Z로 연장되도록 형성되고, 무인항공기가 상승 또는 하강을 행하는 통로 공간(30)과, 통로 공간(30) 내의 기압을 제어하는 기압 제어 시스템(40)을 구비하고, 기압 제어 시스템(40)은, 무인항공기보다 상측의 기압이 무인항공기보다 하측의 기압보다 낮아지도록 제어한다.


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    Title :

    OPERATION FACILITY FOR UNMANNED AERIAL VEHICLE


    Additional title:

    무인항공기의 운용 설비


    Contributors:

    Publication date :

    2024-03-14


    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 / B64U / B65G TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS , Transport- oder Lagervorrichtungen, z.B. Förderer zum Laden oder Abladen / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




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