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Inspection of virtual turbomachinery blade contact gaps

机译:检验虚拟涡轮机械刀片触点差距

摘要

PROBLEM TO BE SOLVED: To provide a computer system and computerized method for virtually inspecting contact gaps of a blade stage of a turbomachine.SOLUTION: The system may include a digitizing device 130 for obtaining a three-dimensional model 132 of a shroud 134 of each blade of the blade stage. A computer system may include at least one module configured to perform the following steps: extracting a geometric location data of a hard face plane of each shroud from the three-dimensional model; generating a three-dimensional virtual rendering of the shrouds of the blade stage on the basis of the geometric location data and known dimensions of the blade stage, the three-dimensional virtual rendering including a rendering of contact gaps between adjacent shrouds; and inspecting the blade stage using the three-dimensional virtual rendering.SELECTED DRAWING: Figure 1
机译:要解决的问题:提供一种计算机系统和计算机化方法,用于几乎检查了涡轮机的叶片阶段的叶片阶段的接触间隙。果实:系统可以包括数字化设备130,用于获得每个的护罩134的三维模型132刀片阶段的叶片。计算机系统可以包括至少一个模块,该模块被配置为执行以下步骤:从三维模型中提取每个护罩的硬面平面的几何位置数据;基于几何位置数据和叶片级的已知尺寸,三维虚拟渲染产生三维虚拟渲染的三维虚拟渲染,包括相邻护罩之间的接触间隙的渲染;使用三维虚拟渲染检查刀片阶段。选择绘图:图1

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