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

System and method for determining a cooling flow parameter downstream from a gas turbine combustor
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
Information query
Patent Agency Ranking
0/0