| 发明名称 |
COMBUSTOR FOR GAS TURBINE ENGINE |
| 摘要 |
A gas turbine engine comprises a combustor. The combustor comprises an annular combustor chamber formed between an inner liner and an outer liner spaced apart from the inner liner. An annular fuel manifold has fuel nozzles distributed circumferentially on the fuel manifold, the fuel manifold and fuel nozzles positioned entirely inside the combustion chamber. |
| 申请公布号 |
US2014260260(A1) |
申请公布日期 |
2014.09.18 |
| 申请号 |
US201313795058 |
申请日期 |
2013.03.12 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
Morenko Oleg |
| 分类号 |
F23R3/28 |
主分类号 |
F23R3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustor comprising:
an annular combustor chamber formed between an inner liner and an outer liner spaced apart from the inner liner; and an annular fuel manifold having fuel nozzles distributed circumferentially on the fuel manifold, the fuel manifold and fuel nozzles positioned entirely inside the combustion chamber. |
| 地址 |
Longueuil CA |
