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Drag reduction systems having fractal geometry/geometrics

机译:具有分形几何/几何学的减阻系统

摘要

Airfoil and hydrofoil systems include structures having a surface texture defined by fractal geometries. Raised portions or fractal bumps can be included on the surfaces, forming a surface texture. The surface textures can be defined by two-dimensional fractal shapes, partial two-dimensional fractal shapes, non-contiguous fractal shapes, three-dimensional fractal objects, and partial three-dimensional fractal objects. The surfaces can include indents having fractal geometries. The indents can have varying depths and can be bordered by other indents, or bumps, or smooth portions of the airfoil or hydrofoil structure. The fractal surface textures can reduce vortices inherent from airfoil and hydrofoil structures. The roughness and distribution of the fractal surface textures reduce the vortices, improving laminar flow characteristics and at the same time reducing drag. The systems are passive and do not require applied power.
机译:机翼和水翼系统包括具有由分形几何形状限定的表面纹理的结构。可在表面上包括凸起部分或分形凸起,从而形成表面纹理。表面纹理可以由二维分形形状,部分二维分形形状,不连续的分形形状,三维分形对象和局部三维分形对象定义。所述表面可包括具有分形几何形状的凹痕。凹痕可以具有变化的深度,并且可以与其他凹痕或隆起或机翼或水翼结构的光滑部分接壤。分形表面纹理可以减少机翼和水翼结构固有的旋涡。分形表面纹理的粗糙度和分布减少了涡流,改善了层流特性,同时减少了阻力。该系统是无源的,不需要施加功率。

著录项

  • 公开/公告号US10001015B2

    专利类型

  • 公开/公告日2018-06-19

    原文格式PDF

  • 申请/专利权人 ALEXANDER J. SHELMAN-COHEN;

    申请/专利号US201414247958

  • 发明设计人 ALEXANDER J. SHELMAN-COHEN;

    申请日2014-04-08

  • 分类号B64C21;F01D5/14;B63B1/34;B64C21/10;F03D1/06;

  • 国家 US

  • 入库时间 2022-08-21 13:06:10

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