| 摘要 |
The invention relates to numerical gas turbine models. The object of the present invention is to propose a gas turbine model and a method for the modeling of a gas turbine, which permits transient modeling with high precision and at the same time numerically efficient means for modeling a gas turbine. The present invention is based on a gas turbine model, which consists of a plurality of sub models. These sub models are either purely dynamic or static, which allows significant simplifications in the numerical solution of the overall model. System parts, which simulate the effects of volumes, metal masses, of actuators, and of measuring systems are regarded as dynamic. The remaining system parts are regarded as static over a time characteristic. |
