A vertical take-off and landing aircraft using a hybrid electric propulsion system is disclosed. A hybrid vertical take-off and landing aircraft according to one embodiment comprises: an engine; a generator which generates electric power by using power supplied from the engine; a battery which stores the electric power generated by the generator; a motor which is supplied with at least one of the electric power stored in the battery and the electric power which is generated by the generator but is not stored in the battery, and supplies power to at least one propulsion generation device; and a control unit which supplies only the electric power stored in the battery to the motor, selects a silence mode of controlling the lifetime by adjusting the output of the motor or a normal mode of supplying, to the motor, the electric power which is not stored in the battery, and determines the amount of the electric power stored in the battery and the amount of the electric power which is not stored in the battery, in the electric power supplied to the motor, on the basis of the selected mode.

    L'invention concerne un aéronef à décollage et atterrissage verticaux utilisant un système de propulsion électrique hybride. Un mode de réalisation de la présente invention concerne un aéronef à décollage et atterrissage verticaux comprenant: un moteur; un générateur qui génère de l'énergie électrique au moyen de l'énergie fournie par le moteur; une batterie qui stocke l'énergie électrique générée par le générateur; un moteur électrique qui est alimenté par l'énergie électrique stockée dans la batterie et/ou l'énergie électrique qui est générée par le générateur mais n'est pas stockée dans la batterie, et fournit de l'énergie à au moins un dispositif de génération de propulsion; et une unité de commande qui fournit uniquement l'énergie électrique stockée dans la batterie au moteur, sélectionne un mode silence de commande de la durée de vie par réglage de la sortie du moteur ou un mode normal de fourniture, au moteur, de l'énergie électrique qui n'est pas stockée dans la batterie, et détermine la quantité d'énergie électrique stockée dans la batterie et la quantité d'énergie électrique qui n'est pas stockée dans la batterie, dans l'énergie électrique fournie au moteur électrique, sur la base du mode sélectionné.

    하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기가 개시된다. 일 실시예에 따른 하이브리드 수직이착륙 항공기는 엔진, 상기 엔진에서 공급되는 동력을 이용하여 전력을 생산하는 발전기, 상기 발전기에서 생산된 전력을 저장하는 배터리, 상기 배터리에 저장된 전력 및 상기 발전기에서 생산되되 상기 배터리에 저장되지 않은 전력 중 적어도 하나를 공급받으며, 적어도 하나의 추력 발생 장치에 동력을 제공하는 모터 및 상기 배터리에 저장된 전력만을 상기 모터에 공급하고, 상기 모터의 출력을 조절하여 지속 가능 시간을 제어하는 사일런스(silence) 모드 또는 상기 배터리에 저장되지 않은 전력을 상기 모터에 공급하는 노멀(normal) 모드를 선택하고, 상기 선택된 모드에 기초하여, 상기 모터에 공급되는 전력에서, 상기 배터리에 저장된 전력의 양 및 상기 배터리에 저장되지 않은 전력의 양을 결정하는 제어부를 포함할 수 있다.


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    Title :

    VERTICAL TAKE-OFF AND LANDING AIRCRAFT USING HYBRID ELECTRIC PROPULSION SYSTEM


    Additional title:

    AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX UTILISANT UN SYSTÈME DE PROPULSION ÉLECTRIQUE HYBRIDE
    하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기


    Contributors:
    BAK JEONG-GYU (author) / CHO JINSOO (author) / KIM BOSEONG (author) / YUN SENGHYUN (author) / WON SUNGHONG (author) / JEONG TAE-CHUL (author) / CHO SOOYOUNG (author) / LEE GEUNHO (author) / PARK KYUSUNG (author) / HA JUHYUNG (author) ... [more]

    Publication date :

    2017-01-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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