일 실시예에 따른, 다중 동력원 전기추진시스템을 구비한 비행체는, 동체, 상기 동체 내에 수용되고, 동력축을 구비하는, 동력터빈, 상기 동체 내에 수용되고, 상기 동력축의 일 단에 연결되는, 발전기, 상기 동력축의 타 단에 연결되고, 전진 비행을 위한 전진 프로펠러, 및 상기 발전기로부터 전력을 공급받고, 수직 이착륙을 위한 리프트 프로펠러를 포함할 수 있다.

    Provided is an aircraft with a multi-power source electric propulsion system. The aircraft includes a fuselage, a power turbine accommodated in the fuselage and having a power shaft, a generator accommodated in the fuselage and connected to one end of the power shaft, a forward propeller for a forward flight and connected to another end of the power shaft, and a lift propeller for vertical take-off and landing (VTOL) and configured to receive power from the generator.


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    Titel :

    AIRCRAFT WITH MULTI-POWER SOURCE ELECTRIC PROPULSION SYSTEMS


    Weitere Titelangaben:

    다중 동력원 전기추진시스템을 구비한 비행체


    Erscheinungsdatum :

    09.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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