| 发明名称 |
DUAL FUEL NOZZLE SYSTEM AND APPARATUS |
| 摘要 |
In various embodiments, a dual fuel nozzle (200) for use in a gas 200 turbine engine is provided. The nozzle may be configured to supply and gas and a liquid. The dual fuel nozzle (200) may include an interior wall (217). The interior wall (217) may include a shoulder (219). The shoulder (219) may include one or more gas ports (216). Gas may be discharged through the gas ports (216) and penetrate a mixing zone. |
| 申请公布号 |
US2016201897(A1) |
申请公布日期 |
2016.07.14 |
| 申请号 |
US201414913056 |
申请日期 |
2014.08.19 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Snyder Timothy S;Dai Zhongtao;Smith Randolph J;Kopp-Vaughan Kristin |
| 分类号 |
F23C1/08;F23D14/48 |
主分类号 |
F23C1/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine fuel nozzle, comprising:
a housing, defining a mixing chamber including a transition zone, the housing comprising,
an interior wall comprising a shoulder and defining a fuel port in the shoulder,the fuel port configured to conduct a fuel into the mixing chamber, wherein the fuel propagates across a volume of the mixing chamber prior to reaching the transition zone. |
| 地址 |
Hartford CT US |
