发明名称 Trailing edge thickness measurement method and apparatus
摘要 Apparatus for measuring the trailing edge thickness of an airfoil in a turbine includes a plurality of tools; each tool having a main body portion and a forward end; an opening along a side edge and in proximity to a forward edge of the forward end, the opening including a slot of predetermined width adapted to engage the trailing edge of the airfoil; wherein each of the tools has a different predetermined slot width. A method for determining the trailing edge thickness of an airfoil in a turbine includes the steps of: a) providing a tool having an opening including a slot having a predetermined width, the opening adapted to receive the trailing edge of the airfoil; b) aligning the tool to receive the trailing edge of the airfoil in the opening; c) determining if a match exists between the trailing edge and the slot width; d) if no match, repeating steps a) through c) with a tool having a different predetermined slot width until a match is found; and e) recording the size of the tool, as identified by the predetermined slot width, as the actual trailing edge thickness of the airfoil.
申请公布号 US2002092190(A1) 申请公布日期 2002.07.18
申请号 US20010760293 申请日期 2001.01.16
申请人 HOFER DOUGLAS CARL;MOLLO NICHOLAS JOSEPH;MADDAUS ALAN DONN;SHAPIRO DAVID ELLIOTT;FOURNIER MAURICE D. 发明人 HOFER DOUGLAS CARL;MOLLO NICHOLAS JOSEPH;MADDAUS ALAN DONN;SHAPIRO DAVID ELLIOTT;FOURNIER MAURICE D.
分类号 G01B3/34;F01D25/00;F02C7/00;G01B3/30;G01B5/06;G01B5/20;(IPC1-7):G01B3/42 主分类号 G01B3/34
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