Invention Grant
US09322333B2 System and method for determining a cooling flow parameter downstream from a gas turbine combustor
有权
用于确定燃气轮机燃烧器下游的冷却流动参数的系统和方法
- Patent Title: System and method for determining a cooling flow parameter downstream from a gas turbine combustor
- Patent Title (中): 用于确定燃气轮机燃烧器下游的冷却流动参数的系统和方法
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Application No.: US13345278Application Date: 2012-01-06
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Publication No.: US09322333B2Publication Date: 2016-04-26
- Inventor: Rex Allen Morgan
- Applicant: Rex Allen Morgan
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, PA
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F02C9/18 ; F02C9/16

Abstract:
A method for determining a cooling flow parameter of a cooling medium supplied through a gas turbine is disclosed. The method may generally include receiving a signal associated with a first value of a combustion product parameter at a location within a combustion zone of the gas turbine, receiving a signal associated with a second value of a combustion product parameter at a location downstream of the combustion zone, comparing the first and second values of the combustion product parameter and determining a cooling flow parameter of the cooling medium based on the comparison of the first and second values.
Public/Granted literature
- US20130174564A1 SYSTEM AND METHOD FOR OPERATING A GAS TURBINE Public/Granted day:2013-07-11
Information query
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