The present invention relates to a twin engine type fixed wing flight vehicle in which an aileron is not mounted, wherein a fixed wing flight vehicle in which an aileron is not mounted in a main wing is formed to be a twin engine type in which a motor having excellent control ability is mounted. Moreover, each motor formed for a rotating direction to be different is controlled to precisely control an angle and a speed when turning and flying. According to the present invention, the twin engine type fixed wing flight vehicle in which an aileron is not mounted comprises a motor member in each of main wings provided on both sides of a fuselage. In the twin engine type fixed wing flight vehicle, an aileron is not mounted in each of the main wings of the twin engine type fixed wing flight vehicle, and the rotating directions of the motor members are formed to be different from each other.

    본 발명은 주 날개에 에일러론이 미장착된 고정익 비행체를 제어성이 우수한 모터가 장착되는 쌍발기 형태로 구성하되, 회전 방향이 다르게 구성되는 각각의 모터를 제어하여 선회 비행시의 각도 및 속도를 정밀하게 제어하는 에일러론이 미장착되는 쌍발형 고정익 비행체에 관한 것이다. 본 발명에 의한 에일러론이 미장착되는 쌍발형 고정익 비행체는 동체의 양측으로 구비되는 주 날개부 각각에 모터 부재가 구비되는 쌍발형 고정익 비행체에 있어서, 쌍발형 고정익 비행체의 주 날개부 각각에는 에일러론이 미장착되고, 각각의 모터 부재는 상호 간에 회전 방향이 다르게 구성되는 것을 특징으로 한다.


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    Title :

    Fixed wing flight vehicle unequipped aileron


    Additional title:

    에일러론이 미장착되는 쌍발형 고정익 비행체


    Contributors:

    Publication date :

    2017-11-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

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



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