发明名称 TURBINE BLADE HAVING MATERIAL BLOCK AND RELATED METHOD
摘要 A turbine blade including a root section at an end of the turbine blade, a first airfoil section adjacent to the root section, and a tip section adjacent to the airfoil section and including a material block that is incongruous with the airfoil section. A midspan section may also include a material block. Each material block can be selectively machined to customize the length of the turbine blade and the position of a tip shroud connection or midspan connection. The turbine blade can be sized for retrofitting last stage blades of older turbines. A radial position of the root mounts for the turbine blade may also be adjusted to provide further customization.
申请公布号 US2010199496(A1) 申请公布日期 2010.08.12
申请号 US20090366688 申请日期 2009.02.06
申请人 GENERAL ELECTRIC COMPANY 发明人 DEMANIA ALAN RICHARD;MADDAUS ALAN DONN;POCK STEVEN RUSSELL
分类号 B21K25/00;B23P15/02 主分类号 B21K25/00
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