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本文根据燃气轮机各部件的基本工作原理,从已有部件的试验特性推导出具有不同设计参数的新设计部件的特性。将这种方法与燃气轮机数学模型相结合,构成设计参数可以变化的燃气轮机“弹性”数学模型。
In this paper, according to the basic working principle of gas turbine components, the characteristics of new design components with different design parameters are deduced from the experimental characteristics of existing components. Combining this method with the mathematical model of a gas turbine constitutes a “flexible” mathematic model of a gas turbine that can vary in design parameters.