| 发明名称 |
FULL RING SLIDING NACELLE WITH THRUST REVERSER |
| 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. The gas turbine engine also includes a rail coupled to the fore pylon and extending in the aft direction from the first annular portion. The gas turbine engine also includes a second annular portion, arranged aft of the first portion and coupled to the rail. The second annular portion is movable along an engine core centerline between a closed position and at least one open position. The second annular portion is configured to engage the first annular portion in the closed position, thereby providing access to the engine core. The gas turbine engine further comprises a thrust reverser arranged in the second annular portion. |
| 申请公布号 |
US2015121895(A1) |
申请公布日期 |
2015.05.07 |
| 申请号 |
US201414187027 |
申请日期 |
2014.02.21 |
| 申请人 |
United Technologies Corporation |
发明人 |
Suciu Gabriel L.;Chandler Jesse M.;Bomzer T. David |
| 分类号 |
F02K1/32;F02C3/04;F02C7/20 |
主分类号 |
F02K1/32 |
| 代理机构 |
|
代理人 |
|
| 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 and extending in the aft direction from the first annular portion; 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 at least one open position, wherein the second annular portion is configured to engage the first annular portion in the closed position, thereby providing access to the engine core; and a thrust reverser arranged in the second annular portion. |
| 地址 |
Hartford CT US |
