首页> 外国专利> Aircraft lift and propulsion device, has upper and lower propellers, whose blades operate in concomitant manner in horizontal planes and tapered planes that are secant to horizontal planes for allowing air lift and propulsion of device

Aircraft lift and propulsion device, has upper and lower propellers, whose blades operate in concomitant manner in horizontal planes and tapered planes that are secant to horizontal planes for allowing air lift and propulsion of device

机译:飞机提升和推进装置,具有上下螺旋桨,其螺旋桨在水平面和与水平面相交的锥形平面中同时工作,以允许空气提升和推进装置

摘要

The device has upper and lower propellers (1, 2), whose blades operate in a concomitant manner in horizontal planes and tapered planes that are secant to the horizontal planes for allowing air lift and propulsion of the device. The propeller (2) has variable pitch blades that act on vertical position of an aircraft. The propellers are integrated to a fairing (3) by end of the blades. The propellers are integrated to the device by using a peripheral fairing (4). The fairing (4) has a large and deep recess (5) that is provided along an entire outer periphery.
机译:该装置具有上部和下部螺旋桨(1、2),其叶片在水平面和与水平面相交的锥形平面中以相应的方式工作,以允许空气升起和推进该装置。螺旋桨(2)具有可变螺距叶片,作用于飞机的垂直位置。螺旋桨通过叶片末端与整流罩(3)集成在一起。螺旋桨通过使用外围整流罩(4)集成到设备中。整流罩(4)具有沿整个外周设置的大而深的凹部(5)。

著录项

  • 公开/公告号FR2903657A1

    专利类型

  • 公开/公告日2008-01-18

    原文格式PDF

  • 申请/专利权人 LE BRETON YANN;

    申请/专利号FR20060006312

  • 发明设计人 LE BRETON YANN;

    申请日2006-07-11

  • 分类号B64C11/46;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:14

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