发明名称 TRAILING EDGE THICKNESS MEASUREMENT METHOD AND APPARATUS
摘要 PURPOSE: A method and an apparatus for measuring a trailing edge thickness are provided to measure the trailing edge thickness of a bucket and a nozzle in an assembled stage quickly and effectively. CONSTITUTION: An 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(14), an opening along a side edge(20) and in proximity to a forward edge(22) of the forward end(14), the opening including a slot(26) of predetermined width adapted to engage the trailing edge of the airfoil wherein each of the tools has a different predetermined slot width. A tool having an opening including a slot having a predetermined width is provided. The tool is aligned to receive the trailing edge in the opening. A match exists between the trailing edge and the slot width is decided. If no match, the providing step and the deciding step are repeated with a tool having a different predetermined slot width until a match is found. The size of the tool is recorded as the trailing edge thickness.
申请公布号 KR20020061166(A) 申请公布日期 2002.07.23
申请号 KR20020002188 申请日期 2002.01.15
申请人 GENERAL ELECTRIC COMPANY 发明人 FOURNIER MAURICE D.;HOFER DOUGLAS CARL;MADDAUS ALAN DONN;MOLLO NICHOLAS JOSEPH;SHAPIRO DAVID ELLIOTT
分类号 G01B3/34;F01D25/00;F02C7/00;G01B3/30;G01B5/06;G01B5/20;(IPC1-7):G01B5/06 主分类号 G01B3/34
代理机构 代理人
主权项
地址