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 US2012014803(A1) 申请公布日期 2012.01.19
申请号 US201113246000 申请日期 2011.09.27
申请人 DEMANIA ALAN RICHARD;MADDAUS ALAN DONN;POCK STEVEN RUSSELL;GENERAL ELECTRIC COMPANY 发明人 DEMANIA ALAN RICHARD;MADDAUS ALAN DONN;POCK STEVEN RUSSELL
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
主权项
地址