| 发明名称 | Turbine servicing device | ||
| 摘要 | A turbine servicing device includes a base member mountable proximate an inlet of a section of a turbine system. Also included is a retaining component operatively coupled to the base member. Further included is a rod having a first end and a second end, the rod in a slidable and pivotable relationship with the retaining component. Yet further included is a machining device operatively coupled to the rod proximate the second end and configured to polish a portion of a turbine component. | ||
| 申请公布号 | US9085060(B2) | 申请公布日期 | 2015.07.21 |
| 申请号 | US201213723603 | 申请日期 | 2012.12.21 |
| 申请人 | GENERAL ELECTRIC COMPANY | 发明人 | Clark Jason Matthew |
| 分类号 | B23P6/00;B24B19/14;B24B23/02;B24B23/08;F01D25/28 | 主分类号 | B23P6/00 |
| 代理机构 | Cantor Colburn LLP | 代理人 | Cantor Colburn LLP |
| 主权项 | 1. A turbine servicing device comprising: a base member mountable proximate an inlet of a compressor section of a turbine system; a retaining component comprising a spherical bearing joint operatively coupled to the base member; a rod having a first end and a second end, the rod in a slidable relationship with the retaining component and in a pivotable relationship with the base member; a machining device operatively coupled to the rod proximate the second end and configured to polish a portion of a turbine component; and a user interface consisting of a single handle operatively coupled to the first end of the rod, wherein an entire length of the rod and the user interface is extendable into the compressor section through a plurality of inlet guide vanes. | ||
| 地址 | Schenectady NY US | ||