首页> 外国专利> Hybrid aircraft e.g. passenger aircraft, for transport of e.g. persons, has nose-side and rear-side annular wings, where chord of wings is arranged at constant or continuously changing radial distance about longitudinal axis of aircraft

Hybrid aircraft e.g. passenger aircraft, for transport of e.g. persons, has nose-side and rear-side annular wings, where chord of wings is arranged at constant or continuously changing radial distance about longitudinal axis of aircraft

机译:混合动力飞机客机,用于运输例如人,具有前侧和后侧环形翼,其中翼弦围绕飞机的纵轴以恒定或连续变化的径向距离布置

摘要

The aircraft has an aerostatic drive component operated by lifting gas cells (11), and an aerodynamic drive component generated by a carrier surface (20). The carrier surface has nose-side and rear-side annular wings (2) alignable in a flight direction, where a chord of the wings is arranged at a constant or continuously changing radial distance about a longitudinal axis (x) of the aircraft. The wings are divided into two radial segments, where one of the segments is formed as the carrier surface with an asymmetric wing profile.
机译:该飞机具有通过举升气室(11)操作的空气动力驱动部件,以及由运载器表面(20)产生的空气动力驱动部件。载体表面具有可在飞行方向上对准的前侧和后侧环形翼(2),其中翼的弦围绕飞机的纵轴(x)以恒定或连续变化的径向距离布置。机翼分为两个径向部分,其中一个部分形成为具有不对称机翼轮廓的承载面。

著录项

  • 公开/公告号DE102008038872A1

    专利类型

  • 公开/公告日2010-02-11

    原文格式PDF

  • 申请/专利权人 GRIMM FRIEDRICH;

    申请/专利号DE20081038872

  • 发明设计人 GRIMM FRIEDRICH;

    申请日2008-08-08

  • 分类号B64B1/20;B64C39;

  • 国家 DE

  • 入库时间 2022-08-21 18:28:50

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