| 发明名称 |
INLET BLEED HEAT SYSTEM AND RELATED METHOD FOR A COMPACT GAS TURBINE INLET |
| 摘要 |
An inlet system for a gas turbine includes an inlet air duct; a silencer disposed in the inlet air duct, the silencer including a plurality of panels with spaces between the panels; and a conduit with orifices disposed to inject inlet bleed heat into each of the spaces. A method of conditioning inlet air for a gas turbine includes flowing air through spaces between panels of a silencer in an inlet air duct of the gas turbine, and injecting inlet bleed heat through orifices and into each of the spaces. |
| 申请公布号 |
US2015068217(A1) |
申请公布日期 |
2015.03.12 |
| 申请号 |
US201314019791 |
申请日期 |
2013.09.06 |
| 申请人 |
General Electric Company |
发明人 |
MERCHANT Laxmikant;AVISHETTI Srinivas;PONYAVIN Valery Ivanovich;BYRD Doug |
| 分类号 |
F02C7/08;F02C7/045 |
主分类号 |
F02C7/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An inlet system for a gas turbine, the system comprising:
an inlet air duct; a silencer disposed in the inlet air duct, the silencer including a plurality of panels with spaces between the panels; and a conduit with orifices disposed to inject inlet bleed heat into each of the spaces. |
| 地址 |
Schenectady NY US |
