Invention Grant
US09359951B2 Inlet bleed heat system and related method for a compact gas turbine inlet
有权
入口放气加热系统及其紧凑型燃气轮机入口的相关方法
- Patent Title: Inlet bleed heat system and related method for a compact gas turbine inlet
- Patent Title (中): 入口放气加热系统及其紧凑型燃气轮机入口的相关方法
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Application No.: US14019791Application Date: 2013-09-06
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Publication No.: US09359951B2Publication Date: 2016-06-07
- Inventor: Laxmikant Merchant , Srinivas Avishetti , Valery Ivanovich Ponyavin , Doug Byrd
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye P.C.
- Main IPC: F02C7/08
- IPC: F02C7/08 ; F02C7/04 ; F02C7/047 ; F02C7/045
Abstract:
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.
Public/Granted literature
- US20150068217A1 INLET BLEED HEAT SYSTEM AND RELATED METHOD FOR A COMPACT GAS TURBINE INLET Public/Granted day:2015-03-12
Information query
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