首页> 外国专利> Powered aircraft including inflatable and rotatable bodies exhibiting a circular cross-section perpendicular to its rotation axis and in order to generate a lift force

Powered aircraft including inflatable and rotatable bodies exhibiting a circular cross-section perpendicular to its rotation axis and in order to generate a lift force

机译:动力飞行器,包括可充气和可旋转的物体,其横截面垂直于其旋转轴并呈圆形,以产生升力

摘要

A lift force generating aircraft having an engine and a thrust force producing device. A pair of elongated and rotating bodies, an axial centerline through the bodies extending in a direction substantially perpendicular to a fore to aft axis extending between the engine and thrust-producing device and at a location above a center of gravity associated with the engine and thrust-producing device. The rotating bodies being constructed of a material inflatable to a desired pressure. A rotary output associated with the engine rotating the bodies, causing them to deflect to angles lesser than the perpendicular with the fore to aft axis, and in response to air stream forces acting upon the bodies in order to reduce drag forces experienced on a rear side of the rotating bodies.
机译:具有发动机和推力产生装置的产生升力的飞行器。一对细长且旋转的主体,穿过主体的轴向中心线沿基本垂直于前后轴线的方向延伸,该轴线在发动机和推力产生装置之间延伸,并且位于与发动机和推力相关的重心上方的位置生产设备。旋转体由可膨胀至期望压力的材料构成。与发动机相关的旋转输出使车身旋转,使其偏转到小于与前后轴线垂直的角度,并响应于作用在车身上的气流力,以减小后侧承受的阻力的旋转体。

著录项

  • 公开/公告号US7427047B2

    专利类型

  • 公开/公告日2008-09-23

    原文格式PDF

  • 申请/专利权人 OMID SAEED TEHRANI;

    申请/专利号US20050138130

  • 发明设计人 OMID SAEED TEHRANI;

    申请日2005-05-26

  • 分类号B64C39;B64C27;

  • 国家 US

  • 入库时间 2022-08-21 20:11:12

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