| 发明名称 | Turbine nozzle cooling assembly | ||
| 摘要 | The present application provides an inner nozzle platform. The inner nozzle platform may include a platform cavity, an impingement plenum positioned within the platform cavity, a retention plate positioned on a first side of the impingement plenum, and a compliant seal positioned on a second side of the impingement plenum. | ||
| 申请公布号 | US8944751(B2) | 申请公布日期 | 2015.02.03 |
| 申请号 | US201213345776 | 申请日期 | 2012.01.09 |
| 申请人 | General Electric Company | 发明人 | Winn Aaron Gregory;Coign Robert Walter;Phillips James Stewart;Tipton Thomas Robbins;Foster Gregory Thomas;Meenakshisundaram Ravichandran;Pai Niranjan Gokuldas |
| 分类号 | B05B9/00;F01D11/00;B05B1/00 | 主分类号 | B05B9/00 |
| 代理机构 | Sutherland Asbill & Brennan LLP | 代理人 | Sutherland Asbill & Brennan LLP |
| 主权项 | 1. A nozzle inner platform, comprising: a platform cavity comprising hooks on opposite sides of the platform cavity; an impingement plenum positioned within the platform cavity; a retention plate coupled within the platform cavity and positioned on a first side of the impingement plenum, the retention plate secured in the platform cavity by engaging the hooks on opposite sides of the platform cavity; and a compliant seal positioned on a second side of the impingement plenum. | ||
| 地址 | Schenectady NY US | ||