The present invention relates to a deceleration device for an aircraft, comprising: a separation unit connected to one side of an aircraft; a parachute connected to the separation unit by a plurality of cables; a power generation unit that is provided on the parachute to generate electricity; and a wire that transmits the power produced by the power generation unit to the separation unit, wherein the separation unit is configured to be separated from the aircraft by electric power transmitted from the wire.

    본 발명은 비행체의 감속장치에 관한 것으로, 비행체의 일측에 연결되는 분리부; 다수의 케이블에 의해 분리부와 연결되는 낙하산; 낙하산에 구비되어 전력을 생산하는 발전부; 및 발전부에서 생산된 전력을 분리부로 전달하는 전선;을 포함하되, 분리부는, 전선에서 전달되는 전력에 의해 비행체와 분리되도록 구성된다.


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    Title :

    Apparatus for decelerating of aircraft


    Additional title:

    비행체의 감속장치


    Contributors:

    Publication date :

    2021-06-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B26F Perforieren , PERFORATING / F03D Windkraftmaschinen , WIND MOTORS



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