Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel

被引:8
|
作者
Serbin, Serhiy [1 ]
Burunsuz, Kateryna [1 ]
机构
[1] Admiral Makarov Natl Univ Shipbldg, Dept Turbines, Mech Engn Inst, UA-54025 Mikolayiv, Ukraine
关键词
gas turbine engine; nitrogen oxide emission; numerical simulation; IMPROVEMENT;
D O I
10.1515/tjj-2020-0029
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Investigations of the working process in a gas turbine combustion chamber with ecological and energy steam injection operating on liquid fuel are conducted. The mathematical model of the aerodynamic processes and liquid fuel combustion in similar burning devices based on the numerical solution of the system of conservation and transport equations for a multi-component chemically reactive turbulent system is developed. The influence of the relative steam mass flow rate (the ratio of the sum of the mass flow rates of ecological and energy steam to the fuel consumption) on the combustion chamber's emission characteristics is determined. The obtained results can be used for parameter selection and optimization of promising high-temperature gas turbine combustion chambers with steam injection operating on liquid fuels.
引用
收藏
页码:71 / 80
页数:10
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