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 |
US9359951(B2) |
申请公布日期 |
2016.06.07 |
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;F02C7/04;F02C7/047;F02C7/045 |
主分类号 |
F02C7/08 |
代理机构 |
Nixon & Vanderhye P.C. |
代理人 |
Nixon & Vanderhye P.C. |
主权项 |
1. An inlet system for a gas turbine, the inlet system comprising:
an inlet air duct; a silencer disposed in the inlet air duct, the silencer including panels with spaces between the panels; and a conduit with orifices disposed to inject inlet bleed heat into each of the spaces, wherein each of the orifices is disposed along the conduit at a midpoint between two of the panels, and the midpoint includes deviations from ideal or nominal values that are within manufacturing and/or inspection tolerances. |
地址 |
Schenectady NY US |