发明名称 TURBINE BUCKET ASSEMBLY AND TURBINE SYSTEM
摘要 A turbine bucket assembly and turbine system are disclosed. The assembly includes a single-lobe joint having an integral platform, the joint having a first axial length; a non-segmented airfoil extending radially outward from the integral platform and having a tip end with a second axial length, the second axial length being less than the first axial length; and a turbine wheel having a receptacle with a geometry corresponding to the single-lobe joint and being coupled to the single-lobe joint. The joint and the non-segmented airfoil include a turbine bucket material, and the turbine wheel includes a turbine wheel material, the turbine wheel material having a lower heat resistance and a higher thermal expansion than the turbine bucket material.
申请公布号 US2015345310(A1) 申请公布日期 2015.12.03
申请号 US201414290352 申请日期 2014.05.29
申请人 GENERAL ELECTRIC COMPANY 发明人 DAVIDSON Dwight Eric;BALSONE Stephen Joseph;POTTER Brian Denver
分类号 F01D5/28;F01D5/30 主分类号 F01D5/28
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 non-segmented airfoil extending radially outward from the integral platform and having a tip end with a second axial length, the second axial length being less than the first axial length; and a turbine wheel having a receptacle with a geometry corresponding to the single- lobe joint and being coupled to the single-lobe joint; wherein the non-segmented airfoil includes a turbine bucket material, and the turbine wheel includes a turbine wheel material, the turbine wheel material having a lower heat resistance and a higher thermal expansion than the turbine bucket material.
地址 Schenectady NY US