| 发明名称 | Integrated nozzle and plug | ||
| 摘要 | A gas turbine engine includes a first annular portion that is stationary and adapted for partially surrounding an engine core. The first annular portion includes a fore pylon connecting portion. A rail is coupled to the fore pylon portion and extends in the aft direction from the stationary portion. A second annular portion is positioned aft of the first portion and coupled to the rail, the second portion being movable along an engine core centerline between a closed position and an open position, wherein the second annular portion is configured to engage with the first annular portion in the closed position to provide access to an engine core. The second annular portion includes a nozzle plug. | ||
| 申请公布号 | US9573695(B2) | 申请公布日期 | 2017.02.21 |
| 申请号 | US201414187032 | 申请日期 | 2014.02.21 |
| 申请人 | United Technologies Corporation | 发明人 | Suciu Gabriel L.;Chandler Jesse M. |
| 分类号 | F01D25/28;B64D29/06;F01D9/02;F01D25/24 | 主分类号 | F01D25/28 |
| 代理机构 | Kinney & Lange, P.A. | 代理人 | Kinney & Lange, P.A. |
| 主权项 | 1. A gas turbine engine comprising: a first annular portion that is stationary and adapted for partially surrounding an engine core, the first annular portion including a fore pylon connecting portion; a rail coupled to the fore pylon portion and extending in the aft direction from the stationary portion; and a second annular portion, aft of the first portion and coupled to the rail, the second portion being movable along an engine core centerline between a closed position and a fully open position, wherein the second annular portion is configured to engage with the first annular portion in the closed position, and to provide access to the engine core in a partially open position, the second annular portion including a nozzle plug. | ||
| 地址 | Farmington CT US | ||