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发明授权
US09284890B2 Method of determining a combustor exit temperature and method of controlling a gas turbine 有权
确定燃烧器出口温度的方法和控制燃气轮机的方法

Method of determining a combustor exit temperature and method of controlling a gas turbine
摘要：
A method of determining an exit temperature of a gas exiting a combustor of a gas turbine includes determining a mass flow and a temperature of fuel being delivered to the combustor; determining a mass flow and a temperature of air being delivered to the combustor, determining a temperature dependence of the specific heat capacity of a burnt mixture of the fuel and the air being delivered to the combustor; and determining an exit temperature of the burnt mixture exiting the combustor. The exit temperature is determined based on the determined mass flow and temperature of the fuel, the determined mass flow and temperature of the air, and the determined temperature dependence of the specific heat capacity of the burnt mixture.
摘要（中）：

确定离开燃气轮机的燃烧器的气体的出口温度的方法包括确定输送到燃烧器的燃料的质量流量和温度; 确定输送到燃烧器的空气的质量流量和温度，确定被输送到燃烧器的燃料和空气的燃烧混合物的比热容的温度依赖性; 以及确定离开燃烧器的燃烧的混合物的出口温度。 出口温度根据确定的燃料质量流量和温度，确定的空气质量流量和温度以及确定的燃烧混合物的比热容量的温度依赖性来确定。

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