发明名称 |
SYSTEM FOR PREMIXING AIR AND FUEL IN A FUEL NOZZLE |
摘要 |
According to various embodiments, a system includes a turbine fuel nozzle. The turbine fuel nozzle includes a first fuel passage extending to a downstream mixing region, a first air passage extending from an exterior of the turbine fuel nozzle to the downstream mixing region, and a second fuel passage extending into the first air passage upstream of the downstream mixing region.
|
申请公布号 |
US2012192565(A1) |
申请公布日期 |
2012.08.02 |
申请号 |
US201113195799 |
申请日期 |
2011.08.01 |
申请人 |
TRETYAKOV DMITRY VLADLENOVICH;SLOBODYANSKIY ILYA ALEXANDROVICH;KOSHEVETS SERGEY VICTOROVICH;GENERAL ELECTRIC COMPANY |
发明人 |
TRETYAKOV DMITRY VLADLENOVICH;SLOBODYANSKIY ILYA ALEXANDROVICH;KOSHEVETS SERGEY VICTOROVICH |
分类号 |
F02C7/22;B05B7/04 |
主分类号 |
F02C7/22 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|