| 发明名称 |
OFFSET CORES FOR GAS TURBINE ENGINES |
| 摘要 |
A gas turbine engine includes a propulsor with a power turbine, a power turbine shaft extending forward therefrom defining a centerline axis, and a fan driven by the power turbine shaft. The fan is aligned with the centerline axis forward of the power turbine and is operatively connected to be driven by the power turbine through the power turbine shaft. A gas generator operatively connected to the propulsor is included downstream from the fan and forward of the power turbine, wherein the gas generator defines a generator axis offset from the centerline axis. The gas generator is operatively connected to the power turbine to supply combustion products for driving the power turbine. |
| 申请公布号 |
US2016115866(A1) |
申请公布日期 |
2016.04.28 |
| 申请号 |
US201514921575 |
申请日期 |
2015.10.23 |
| 申请人 |
United Technologies Corporation |
发明人 |
Suciu Gabriel L.;Hill James D. |
| 分类号 |
F02C3/14;F01D25/30;F01D25/24;F02C3/04;F02K3/00 |
主分类号 |
F02C3/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a propulsor including a power turbine, a power turbine shaft extending forward therefrom defining a centerline axis, and a fan driven by the power turbine shaft, wherein the fan is aligned with the centerline axis and is defined forward of the power turbine; and a gas generator operatively connected to the propulsor downstream from the fan and forward of the power turbine, wherein the gas generator defines a generator axis offset from the centerline axis. |
| 地址 |
Farmington CT US |
