Method and system for automated repair design of damaged blades of a compressor or turbine
    1.
    发明授权
    Method and system for automated repair design of damaged blades of a compressor or turbine 有权
    压缩机或涡轮机损坏叶片的自动修复设计方法和系统

    公开(公告)号:US06915236B2

    公开(公告)日:2005-07-05

    申请号:US10301723

    申请日:2002-11-22

    CPC classification number: B23P6/002 F01D5/005 Y10T29/4973

    Abstract: A method is disclosed for evaluating a damaged blade in a compressor or turbine using a computer system accessing a database of blade repair information, where the method includes: selecting a blade damage geometry category corresponding to the damage of the blade from a plurality of blade damage geometry categories; measuring the blade damage, and generating a repair geometry for the blade based on the blade damage measurements and the selected blade damage geometry category.

    Abstract translation: 公开了一种用于使用访问刀片修复信息的数据库的计算机系统来评估压缩机或涡轮机中的损坏的刀片的方法,其中所述方法包括:从多个刀片损伤中选择对应于刀片损坏的刀片损伤几何类别 几何类别; 测量刀片损伤,并根据刀片损伤测量和所选择的刀片损伤几何类别为刀片生成修复几何。

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