| 发明名称 |
TURBINE ENGINE AND METHOD OF ASSEMBLING THEREOF |
| 摘要 |
A turbine engine is provided. The turbine engine includes a compressor configured to discharge a flow of air at a first flow angle and a combustor coupled downstream from the compressor. The combustor is configured to combust the flow of air with fuel to form a flow of combustion gas discharged from the combustor at a second flow angle. The turbine engine also includes a turbine coupled downstream from the combustor. The turbine includes an inlet configured to receive the flow of combustion gas having a flow angle within a predetermined range, wherein the combustor is oriented such that the second flow angle is within the predetermined range. |
| 申请公布号 |
US2015323185(A1) |
申请公布日期 |
2015.11.12 |
| 申请号 |
US201414570838 |
申请日期 |
2014.12.15 |
| 申请人 |
General Electric Compamy |
发明人 |
Silkowski Peter Daniel |
| 分类号 |
F23R3/14;F04D29/54;B23P15/04;F02C3/04 |
主分类号 |
F23R3/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine comprising:
a compressor configured to discharge a flow of air at a first flow angle; a combustor coupled downstream from said compressor, said combustor configured to combust the flow of air with fuel to form a flow of combustion gas discharged from said combustor at a second flow angle; and a turbine coupled downstream from said combustor, said turbine comprising an inlet configured to receive the flow of combustion gas having a flow angle within a predetermined range,
wherein said combustor is oriented such that the second flow angle is within the predetermined range. |
| 地址 |
Schenectady NY US |
