发明名称 TURBINE BUCKET ASSEMBLY AND TURBINE SYSTEM
摘要 A turbine bucket assembly and turbine system are disclosed. The turbine bucket assembly includes a single-lobe joint having an integral platform, the joint having a first axial length; a segmented airfoil having a root segment extending radially outward from the platform and a tip segment coupled to the root segment, the tip segment having a second axial length, which is less than the first axial length; and a turbine wheel defining a receptacle with a geometry corresponding to the single-lobe joint and being coupled to the single-lobe joint. The tip segment includes a tip segment material, the root segment includes a root segment material, and the turbine wheel includes a turbine wheel material, the root segment material and the turbine wheel material having a lower heat resistance and a higher thermal expansion than the tip segment material.
申请公布号 US2015345296(A1) 申请公布日期 2015.12.03
申请号 US201414290076 申请日期 2014.05.29
申请人 GENERAL ELECTRIC COMPANY 发明人 DAVIDSON Dwight Eric;McDUFFORD Michael David;POTTER Brian Denver;BALSONE Stephen Joseph;WASSYNGER Stephen Paul
分类号 F01D5/14 主分类号 F01D5/14
代理机构 代理人
主权项 1. A turbine bucket assembly comprising: a single-lobe joint having an integral platform, the joint having a first axial length; a segmented airfoil having a root segment extending radially outward from the integral platform and a tip segment coupled to the root segment, the tip segment having a second axial length, the second axial length being less than the first axial length; and a turbine wheel defining a receptacle with a geometry corresponding to the single-lobe joint and being coupled to the single-lobe joint; wherein the tip segment includes a tip segment material, the root segment includes a root segment material, and the turbine wheel includes a turbine wheel material, the root segment material and the turbine wheel material having a lower heat resistance and a higher thermal expansion than the tip segment material.
地址 Schenectady NY US