首页> 外国专利> Deflection device e.g. for aerodynamic body, has edge which exhibits surface and surface is set for local direction of flow and deflector attachable at end of body with deflector shaped as missile

Deflection device e.g. for aerodynamic body, has edge which exhibits surface and surface is set for local direction of flow and deflector attachable at end of body with deflector shaped as missile

机译:偏转装置对于空气动力学车身,其边缘具有表面,表面设置为局部流动方向,并且可以在车身末端安装导流板,导流板的形状为导弹

摘要

The deflector has an edge which exhibits a surface (4). The surface (4) is bet for local direction of flow (13). The deflector is attachable (2) at an end of the body (8). The deflector is shaped as a missile (8). The missile has a blunt form, where a dragging probe (20) is attachable. In direction of flow behind the body a turbulence is developed. A first section of the dragging probe has an arranged deflector having a first length (28). A second length (24) of a second section of the dragging probe (20) is provided which is in turbulence range, and longer than the first length.
机译:偏转器的边缘具有表面(4)。该表面(4)用于局部流动方向(13)。偏转器可附接在主体(8)的端部(2)。偏转器的形状像导弹(8)。导弹为钝头形式,可安装拖曳探针(20)。在身体后方的流动方向上产生了湍流。拖曳探针的第一部分具有布置的偏转器,该偏转器具有第一长度(28)。设置了拖曳探针(20)的第二部分的第二长度(24),该第二长度在湍流范围内并且比第一长度长。

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