A gas turbine combustion chamber modeling by physical model

被引：1
|
作者：
Glavan, Ivica [1 ]
Poljak, Igor [1 ]
Kosor, Mate [1 ]
机构：
[1] Univ Zadar, Maritime Dept, M Pavlinovica 1, Zadar 23000, Croatia
来源：
POMORSTVO-SCIENTIFIC JOURNAL OF MARITIME RESEARCH | 2021年 / 35卷 / 01期
关键词：
Gas turbine; Combustion chamber; Combustion temperature; Modelica; SimulationX; PROPULSION; SYSTEM;
D O I：
10.31217/p.35.1.4
中图分类号：
U [交通运输];
学科分类号：
08 ; 0823 ;
摘要：
The validity of the gas turbine unit model largely depends on the accuracy of the flue gas temperature value calculation at the gas turbine inlet (TIT). This temperature is determined by the maximum combustion temperature. In variable running mode, the temperature value is regulated by changing the ratio of air and fuel at the inlet to the combustion chamber. The paper presents a model of a gas turbine combustion chamber using Modelica, an object-oriented language for modeling complex physical systems with the aim of determining the temperature of combustion flue gases, specific heat capacity, enthalpy, and flue gas composition at different gas turbine loads.
引用
收藏
页码：30 / 35
页数：6
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