首页> 外国专利> Vertically-starting delta wing aircraft, has vertically rotatable front motor fastened to body and designed in upwardly-pivoting manner, and rear motor fastened to body and designed in vertically downwardly pivoting manner

Vertically-starting delta wing aircraft, has vertically rotatable front motor fastened to body and designed in upwardly-pivoting manner, and rear motor fastened to body and designed in vertically downwardly pivoting manner

机译:垂直启动的三角翼飞机,具有可垂直旋转的固定在机身上并以向上旋转的方式设计的后电动机,以及具有固定在机身上且垂直向下枢转方式而设计的后电动机。

摘要

The aircraft has a vertically rotatable front motor fastened to a body and designed in an upwardly-pivoting manner. A rear motor is fastened to the body and designed in a vertically downwardly pivoting manner, where impact pressure is produced below trapezoidal main wings. Wheels and a buoyancy chamber are fastened to ends of the main wings. An upper side of the body forms a linear slope that runs at an angle of 3 degree to a chord of the main wings, and a lower side of the body is formed parallel to the upper side and designed in a boat hull-shape.
机译:该飞机有一个可垂直旋转的前电动机,该电动机固定在机身上,并以向上旋转的方式设计。后部电动机固定在车身上并以垂直向下枢转的方式设计,在该处,在梯形主翼下方产生冲击压力。车轮和浮力室固定在主翼的末端。主体的上侧形成与主翼的弦线成3度角的线性斜率,主体的下侧与上侧平行且形成为船体形状。

著录项

  • 公开/公告号DE102010056546A1

    专利类型

  • 公开/公告日2012-07-05

    原文格式PDF

  • 申请/专利权人 RICHTER HELMUT;

    申请/专利号DE20101056546

  • 发明设计人 RICHTER HELMUT;

    申请日2010-12-29

  • 分类号B64C29;

  • 国家 DE

  • 入库时间 2022-08-21 17:05:13

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