首页> 外国专利> Flying object for vertical starting and landing for marsh-and hover flight, has driving mechanism designed as centrifugal compressor, where object is provided with horizontal-lamellae that extends into two groups parallel to rolling axis

Flying object for vertical starting and landing for marsh-and hover flight, has driving mechanism designed as centrifugal compressor, where object is provided with horizontal-lamellae that extends into two groups parallel to rolling axis

机译:用于垂直启动和降落的飞行物体,用于沼泽和悬停飞行,具有设计为离心压缩机的驱动机构,其中物体配备有水平薄片,该薄片平行于滚动轴分为两组

摘要

The object has a driving mechanism (4) whose rotating axis is aligned parallel to a rolling axis. The driving mechanism is designed as a centrifugal compressor, where ambient air is sucked and compressed towards the rolling axis and is discharged towards a pitch axis. The object is provided with a set of horizontal-lamellae (9) that forms gaps, where the horizontal-lamellae extends into two groups parallel to the rolling axis laterally along the object.
机译:该物体具有驱动机构(4),该驱动机构的旋转轴平行于滚动轴对齐。驱动机构设计为离心式压缩机,在该压缩机中,周围的空气被吸入并压缩到滚动轴上,然后被排放到俯仰轴上。该物体设有一组形成间隙的水平薄片(9),其中该水平薄片沿物体横向延伸成平行于滚动轴线的两组。

著录项

  • 公开/公告号DE202006019947U1

    专利类型

  • 公开/公告日2007-08-23

    原文格式PDF

  • 申请/专利权人 OECAL ISKENDER;

    申请/专利号DE202006019947U1

  • 发明设计人

    申请日2006-12-19

  • 分类号B64C29;B64C39;

  • 国家 DE

  • 入库时间 2022-08-21 20:28:56

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