| 发明名称 |
INTEGRATED HEAT SHIELD |
| 摘要 |
A fuel injector for a gas turbine engine includes a nozzle tip assembly having a substantially monolithically formed nozzle body. The nozzle body has an annular outlet chamber for issuing a spray from the nozzle tip. A feed channel is in fluid communication with the outlet chamber through a feed passage. A heat shield void substantially surrounds the feed channel(s). |
| 申请公布号 |
US2015069148(A1) |
申请公布日期 |
2015.03.12 |
| 申请号 |
US201414190535 |
申请日期 |
2014.02.26 |
| 申请人 |
Delavan Inc |
发明人 |
Ryon Jason A.;Pfeffer Brett A.;Donovan Matthew R.;Buelow Philip E. |
| 分类号 |
F02C7/22;F02C7/24 |
主分类号 |
F02C7/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuel injector for a gas turbine engine comprising:
a nozzle tip assembly including a substantially monolithic nozzle body having:
an annular outlet chamber for issuing a spray from the nozzle tip;a feed channel in fluid communication with the outlet chamber through a feed passage; anda heat shield void substantially surrounding the feed channel. |
| 地址 |
West Des Moines IA US |
