The present invention provides an energy-saving platform for a vertical takeoff and landing aircraft that uses an auxiliary aircraft that supports takeoff and landing of a vertical takeoff and landing aircraft between the flight point and the takeoff and landing point by strapping the vertical takeoff and landing aircraft, or uses an auxiliary energy storage device that is separated when the vertical takeoff and landing aircraft completes takeoff, so that it can reduce the energy required during vertical takeoff and landing of the vertical takeoff and landing aircraft.

    본 발명은 수직 이착륙 비행체를 결박하여 비행 지점과 이착륙 지점간의 수직 이착륙 비행체의 이착륙을 지원하는 보조 비행체를 이용하거나, 수직이착륙 비행체가 이륙을 완료하면 분리되는 보조 에너지 저장 장치를 이용하여, 수직 이착륙 비행체의 수직 이착륙시에 필요한 에너지를 절감시킬 수 있는 수직 이착륙 비행체의 에너지 절감 플랫폼을 제공한다.


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    Title :

    ENERGY SAVING PLATFORM FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT


    Additional title:

    수직 이착륙 비행체의 에너지 절감 플랫폼


    Contributors:
    CHO MOON SOO (author) / CHO YUN HO (author) / LEE HYUN WOO (author)

    Publication date :

    2023-04-20


    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