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    • 8. 发明申请
    • Method for measuring the nozzle flow area between gas turbine engine vanes
    • 用于测量燃气涡轮发动机叶片之间的喷嘴流动面积的方法
    • US20070050156A1
    • 2007-03-01
    • US11216793
    • 2005-08-31
    • Janakiraman Vaidyanathan
    • Janakiraman Vaidyanathan
    • G01F1/00
    • G01B11/285F01D5/005F01D9/041G01B21/28
    • Provided are methods for accurately measuring nozzle 50 flow areas of new or refurbished gas turbine engine vanes 14. A first vane 114 is suitably fixtured in a laser scanning system 60 comprising a laser spot projector 82 a laser spot sensor 84, a multi-axis controller 68 and a computer 78. According to a nozzle flow area measurement method, a convex surface 38 and a concave surface 40 of a first vane 114 are scanned and stored as point clouds 196, 296 with the system. The point clouds 196, 296 are combined into a point cloud 396 and translated to a reference coordinate system 98. A point cloud 496 representing a nominally sized, second vane 214 is positioned adjacent to one surface of the combined point cloud 396. An inlet profile 56 is extracted from the intersection of an inlet plane 58, perpendicular to a combustion gas flow vector 18 direction, and each point cloud 396, 496. A nozzle 50 flow area is then accurately calculated using integration techniques from the inlet profile 56. The process is repeated for the second surface of the first vane 114. In another method, a combined point cloud 396 of a second vane 214, which is also scanned using the scanning system, replaces the nominal point cloud 496. The nozzle 50 flow area between the first 114 and second 214 vanes is then measured using the earlier described method steps.
    • 提供了用于精确测量新的或翻新的燃气涡轮发动机叶片14的喷嘴50流动区域的方法。 第一叶片114适当地固定在激光扫描系统60中,激光扫描系统60包括激光点投影仪82,激光点传感器84,多轴控制器68和计算机78。 根据喷嘴流动面积测量方法,第一叶片114的凸表面38和凹面40被扫描并作为点云196,296与系统一起存储。 点云196,296被组合成点云396并转换为参考坐标系98。 表示标称尺寸的第二叶片214的点云496定位成与组合点云396的一个表面相邻。 入口轮廓56从垂直于燃烧气体流向量18方向的入口平面58和每个点云396,496的交点提取。 然后使用来自入口轮廓56的积分技术精确地计算喷嘴50的流动面积。 对于第一叶片114的第二表面重复该过程。 在另一种方法中,也使用扫描系统扫描的第二叶片214的组合点云396代替标称点云496。 然后使用先前描述的方法步骤测量第一114和第二214叶片之间的喷嘴50流动面积。