하이브리드 수직이착륙 운송수단은 유체 정역학 부력을 제공하도록 구성된 기낭, 기낭에 부착되고 움직임을 통하여 동적 양력을 생성하기 위해 동체의 반대 측면들로부터 연장되는 적어도 한쌍의 날개들을 갖는 동체 및 각각의 날개상에 그리고 수직 이륙 또는 착륙 성능들을 제공하기 위해서 기낭의 종축에 횡방향에 있는 축에 대하여 각각의 날개와 함께 회전하도록 구성된 추력 생성 디바이스를 갖는다. 이상적으로는, 기낭은 저-속도 및 대지상에서의 안정성을 증강시키기 위해 음(negative)의 유체 정역학 양력을 제공한다.

    A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability. A vehicle comprising a first lift device capable of providing hydrostatic lift; a second lift device capable of providing dynamic lift through movement; and a system structured to generate thrust coupled to the second lift device, the second lift device and the thrust generation system capable of rotating together about an axis that is lateral to a longitudinal axis of the vehicle at angles at least in the range of 90 degrees to and including 180 degrees.


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    Title :

    HYBRID VTOL VEHICLE


    Additional title:

    하이브리드 수직이착륙 운송수단


    Contributors:
    EGAN JAMES C (author) / EGAN JOEL D (author)

    Publication date :

    2016-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft



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