| 发明名称 |
TURBINE ENGINE FUEL INJECTION SYSTEM AND METHODS OF ASSEMBLING THE SAME |
| 摘要 |
A fuel injection system for use in a combustor of a turbine assembly includes a substantially annular fuel injection housing at least partially defining an annular cavity. The fuel injection system also includes a fuel manifold and an air manifold. The fuel manifold includes a plurality of fuel injection ports extending through the fuel injection housing. The air manifold includes a first plurality of air injection ports and a second plurality of air injection ports that each extends through the fuel injection housing. |
| 申请公布号 |
US2017122211(A1) |
申请公布日期 |
2017.05.04 |
| 申请号 |
US201514927578 |
申请日期 |
2015.10.30 |
| 申请人 |
General Electric Company |
发明人 |
Zhang Yuxin;Chatakonda Obulesu;Gudiyella Soumya;Joshi Narendra Digamber;Tangirala Venkat Eswarlu;Masquelet Matthieu Marc;Yellapantula Shashank |
| 分类号 |
F02C7/22;F23R3/28;F02C7/04 |
主分类号 |
F02C7/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuel injection system for use in a combustor of a turbine assembly, said fuel injection system comprising:
a substantially annular fuel injection housing at least partially defining an annular cavity; a fuel manifold defining a plurality of fuel injection ports extending through said substantially annular fuel injection housing; and an air manifold defining a first plurality of air injection ports and a second plurality of air injection ports, said first plurality of air injection ports and said second plurality of air injection ports extend through said substantially annular fuel injection housing. |
| 地址 |
Schenectady NY US |
