The present invention relates to a technology capable of safe take-off and landing of an aircraft by adding a thrust device capable of generating auxiliary thrust in addition to a main thrust device. According to the present invention, provided is a thrust device for air transportation means which comprises: wings fixed on the left and right sides of a fuselage; a rotor installed on the wing to generate propulsive force; a main thrust device providing a driving force to the rotor using a motor supplied with power from an engine and a battery; and an auxiliary thrust device installed on the fuselage to generate auxiliary thrust and having a center of gravity coincide with the center of gravity of the fuselage.

    본 발명은 메인추력장치 외에 보조적인 추진력을 생성 가능한 추력장치를 추가하여 비행체의 안전한 이착륙이 가능한 기술에 관한 것으로, 본 발명에서는, 동체의 좌우에 고정된 날개; 상기 날개에 설치되어 추진력을 생성하는 로터; 엔진과 배터리에서 동력을 공급받는 모터를 이용하여 상기 로터에 구동력을 제공하는 메인추력장치; 및 상기 동체에 설치되어 보조적인 추진력을 생성하고, 무게중심이 기체의 무게중심과 일치하도록 설치된 보조추력장치;를 포함하여 구성되는 항공운송수단용 추력장치가 소개된다.


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    Title :

    Device for generating thrust for air transport


    Additional title:

    항공운송수단용 추력장치


    Contributors:

    Publication date :

    2022-05-04


    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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