Invention Grant
US08220275B2 Inlet bleed heat system thermal lag mitigation using compressor interstage bleeds
有权
入口放热系统热滞后缓解使用压缩机级间流出
- Patent Title: Inlet bleed heat system thermal lag mitigation using compressor interstage bleeds
- Patent Title (中): 入口放热系统热滞后缓解使用压缩机级间流出
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Application No.: US12353543Application Date: 2009-01-14
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Publication No.: US08220275B2Publication Date: 2012-07-17
- Inventor: Steven William Tillery
- Applicant: Steven William Tillery
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Cantor Colburn LLP
- Main IPC: F02C7/26
- IPC: F02C7/26

Abstract:
A system to mitigate thermal lag of start-up operations of a gas turbine is provided and includes a housing which is disposed upstream from and which is fluidly coupled to a compressor of the gas turbine, a first system coupled to an aft portion of the compressor and to the housing which, when activated, receives a first air supply from the compressor and delivers the first air supply to the housing, and a second system, coupled to the first system, which removes a second air supply from an intermediate portion of the compressor and delivers the second air supply to the first system prior to the activation of the first system.
Public/Granted literature
- US20100175388A1 INLET BLEED HEAT SYSTEM THERMAL LAG MITIGATION USING COMPRESSOR INTERSTAGE BLEEDS Public/Granted day:2010-07-15
Information query
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