基于b样条曲面的螺旋桨几何建模

R. Fernández, F. Pérez-Arribas
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引用次数: 0

摘要

这项工作提出了一种新的设计方法,用于使用b样条曲面对船舶螺旋桨叶片进行建模,b样条曲面是CAD和船舶建筑软件产品中的标准工具。船舶的螺旋桨叶片是自由曲面的一个很好的例子,它的设计特别考虑了控制其性能的几个参数。CAD中用于表面设计的传统工具,如控制点操作,不适合叶片设计,设计师更喜欢使用最终代表其表面的螺旋桨参数集合,并具有明确的流体动力学意义。该方法使用螺旋桨几何形状的通用设计参数,并生成叶片几何形状的最终b样条曲面,该曲面可用于螺旋桨的可视化、计算和构造。该方法首先根据在几个径向位置的一系列横截面的二维定义,定义形成螺旋桨叶片的三维点网格。这些三维点考虑了叶片的倾角和扭转是由前倾角和俯仰角给出的,这在设计过程中很常见,也考虑了不同的螺旋桨参数,如倾斜和叶片厚度分布。螺旋桨叶片是非常薄的物体,曲率变化很大,如果使用标准b样条技术,除非使用大量控制点,否则无法在公差下很好地建模,从而产生非常复杂的表面。该方法强调对螺旋桨性能影响较大的叶片前缘的拟合,在几何上与其他叶片相比曲率半径较小。前缘很难用标准技术复制。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
PROPELLERS GEOMETRY MODELING THROUGH B-SPLINES SURFACES
This work presents a new design methodology for modelling the blades of ship propellers using B-spline surfaces that are a standard tool in CAD and Naval Architecture software products. Propeller blades of a ship are good examples of free form surfaces, designed specifically considering several parameters that control their performance. Traditional tools for surface design in CAD such as control point manipulation, are not appropriated for blade design, and the designers prefer to work with a collection of propeller parameters that ultimately represent its surface and that possess a clear hydrodynamic meaning. This method uses common design parameters for the geometry of propellers and produces a final B-spline surface for the geometry of the blades that can be used for the visualization, calculations, and construction of the propeller. The method starts with the definition of a 3D grid of points that form the propeller blades based on the 2D definition of a series of cross-sectional profiles at several radial locations. These 3D points consider the inclination and twist of the blades are given by rake and pitch angles, quite common in the design procedures, and also different propellers parameters such as skew and blade thickness distribution. Propeller blades are very thin objects with great changes of curvature, and if standard B-spline techniques are used, they cannot be modelled well under a tolerance unless a large number of control points is used, producing very complex surfaces. The method stresses the fitting of the blade's leading edge which has great effect on the propeller behavior and geometrically has a small curvature radius in comparison with the rest of the blades. The leading edge is difficult to reproduce with standard techniques.
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