AIRCRAFT
    2.
    发明申请
    AIRCRAFT 有权
    飞机

    公开(公告)号:US20170008622A1

    公开(公告)日:2017-01-12

    申请号:US14795406

    申请日:2015-07-09

    申请人: ADVISR AERO LLC

    IPC分类号: B64C27/22 B64C39/10 B64C3/38

    摘要: An aircraft is provided that is convertible in flight between a rotary wing configuration and a fixed wing configuration. In its fixed wing configuration the aircraft resembles a Blended Wing Body (BWB) having a swept wing angle β. Conversions from the fixed wing configuration to the rotary wing configuration, and vice versa, are accomplished by flipping an outboard portion of one wing through 180° to reorient the leading edge of the outboard portion by an angle of 2β to establish a reverse sweep. In its rotary configuration, the entire aircraft is rotated.

    摘要翻译: 提供一种飞行器,其可在旋翼结构和固定翼构型之间在飞行中可转换。 在其固定翼构型中,飞机类似于具有扫掠翼角β的混合翼体(BWB)。 通过将一个机翼的外侧部分翻转180°,将外侧部分的前缘重新定位2°的角度来建立反向扫描来实现从固定翼构型到旋转翼构型的转换,反之亦然。 在其旋转结构中,整个飞机旋转。