| 发明名称 |
CROSS-FLOW TURBINE ENGINE |
| 摘要 |
An embodiment of the present invention is a gas turbine engine including a compressor, a turbine, an annular combustor, an exhaust duct, a first engine shaft bearing, and a second engine shaft bearing. The turbine has an axial flow direction toward the compressor. The combustor has an axial flow direction away from the compressor. The exhaust duct is disposed between the compressor and the combustor. The first engine shaft bearing is disposed on an axial side of the compressor opposite the turbine. The second engine shaft bearing is disposed on an axial side of the turbine opposite the compressor. |
| 申请公布号 |
US2014165582(A1) |
申请公布日期 |
2014.06.19 |
| 申请号 |
US201213716247 |
申请日期 |
2012.12.17 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Pascu Victor;Shah Nipulkumar G. |
| 分类号 |
F02C7/18;F02C9/16 |
主分类号 |
F02C7/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a compressor; a turbine connected to the compressor by an engine shaft, the turbine having an axial flow direction toward the compressor; an annular combustor having an axial flow direction away from the compressor; an exhaust duct disposed between the compressor and the combustor; a first engine shaft bearing supporting the engine shaft on an axial side of the compressor opposite the turbine; and a second engine shaft bearing supporting the engine shaft on an axial side of the turbine opposite the compressor.
|
| 地址 |
Hartford CT US |
