| 发明名称 |
COMBUSTOR |
| 摘要 |
A burner includes a pilot burner, a combustion chamber, and a swirler located radially outwardly of the combustion chamber and being adapted to impose a swirling motion on a fuel/air mixture about an axial centerline of the combustion chamber. The pilot burner has a pilot burner face located radially inwardly of the swirler and forms an axially upstream wall of the combustion chamber, the pilot burner face incorporating a pilot fuel injector and an ignitor, both being positioned radially offset from the axial centerline. A recess is positioned radially offset from the axial centerline within the pilot burner face. |
| 申请公布号 |
US2017009994(A1) |
申请公布日期 |
2017.01.12 |
| 申请号 |
US201515113429 |
申请日期 |
2015.01.06 |
| 申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
Buchanan Eoghan;Sadasivuni Suresh |
| 分类号 |
F23R3/28;F02C7/264;F23R3/14 |
主分类号 |
F23R3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A burner comprising:
a pilot burner, a combustion chamber, and a swirler located radially outwardly of the combustion chamber and being adapted to impose a swirling motion on a fuel/air mixture about an axial centerline of the combustion chamber, wherein the pilot burner comprises a pilot burner face located radially inwardly of the swirler and forming an axially upstream wall of the combustion chamber, the pilot burner face incorporating a pilot fuel injector and an ignitor, both being positioned radially offset from the axial centerline, and a recess being positioned radially offset from the axial centerline within the pilot burner face. |
| 地址 |
München DE |
