ROTORCRAFT COMPONENT SIMULATION USING SCAN-BASED GEOMETRY

    公开(公告)号:EP3082055B1

    公开(公告)日:2018-07-18

    申请号:EP16164943.9

    申请日:2016-04-12

    CPC classification number: G06F17/5018 G06F17/5086

    Abstract: A method of performing structural analysis relating to a component (18) having CAD-based geometry (200), refined CAD-based geometry and CAD-based FEA data (60) associated therewith. The method includes scanning (72) the component to obtain scan-based point cloud geometry of the component, aligning the scan-based point cloud geometry with the CAD-based geometry (200) of the component (18), generating scan-based geometry of the component by refining the scan-based point cloud geometry, comparing the scan-based geometry with the refined CAD-based geometry of the component (18) to quantify geometric differences therebetween, generating scan-based FEA geometry (250) of the component (18) by meshing the scan-based geometry, performing finite element analysis on the scan-based FEA geometry (250) to obtain scan-based FEA data and comparing the scan-based FEA data with the CAD-based FEA data (170) of the component (18) to quantify the effect of geometric difference therebetween.

    ROTORCRAFT COMPONENT SIMULATION USING SCAN-BASED GEOMETRY
    2.
    发明公开
    ROTORCRAFT COMPONENT SIMULATION USING SCAN-BASED GEOMETRY 有权
    飞行员扫描基准测量

    公开(公告)号:EP3082055A1

    公开(公告)日:2016-10-19

    申请号:EP16164943.9

    申请日:2016-04-12

    CPC classification number: G06F17/5018 G06F17/5086 Y02T10/82

    Abstract: A method of performing structural analysis relating to a component (18) having CAD-based geometry (200), refined CAD-based geometry and CAD-based FEA data (60) associated therewith. The method includes scanning (72) the component to obtain scan-based point cloud geometry of the component, aligning the scan-based point cloud geometry with the CAD-based geometry (200) of the component (18), generating scan-based geometry of the component by refining the scan-based point cloud geometry, comparing the scan-based geometry with the refined CAD-based geometry of the component (18) to quantify geometric differences therebetween, generating scan-based FEA geometry (250) of the component (18) by meshing the scan-based geometry, performing finite element analysis on the scan-based FEA geometry (250) to obtain scan-based FEA data and comparing the scan-based FEA data with the CAD-based FEA data (170) of the component (18) to quantify the effect of geometric difference therebetween.

    Abstract translation: 执行与具有基于CAD的几何(200),与CAD相关联的基于CAD的几何和基于CAD的FEA数据(60)的组件(18)相关的结构分析的方法。 该方法包括扫描(72)该组件以获得该组件的基于扫描的点云几何,将基于扫描的点云几何与该组件(18)的基于CAD的几何(200)对准,生成基于扫描的几何 通过精简基于扫描的点云几何,将基于扫描的几何与组件(18)的精细的基于CAD的几何形状进行比较,以量化其间的几何差异,生成组件的基于扫描的FEA几何(250) (18),通过对基于扫描的几何进行啮合,对基于扫描的FEA几何进行有限元分析(250)以获得基于扫描的FEA数据,并将基于扫描的FEA数据与基于CAD的FEA数据进行比较(170) 以量化其间的几何差异的影响。

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