本文给出一种模型燃气轮机燃烧室中三维气相反应流流场的数值计算结果。
This paper describes the numerical calculations of gaseous reacting flows in a model of gas turbine combustors.
由于火焰筒轴线平行于发动机轴线，燃气轮机燃烧室的联焰管与火焰筒正交。
The axis of a flame tube being parallel to that of an engine, the flame crossover tube of a turbine combustor is usually orthogonal with respect to the flame tube.
本文通过中压全尺寸燃气轮机燃烧室空气加湿燃烧实验，研究了加湿度对燃烧特性的影响。
In this paper, an air humidified combustion experiment was carried out using mid-pressure full-dimension gas turbine combustor to determine the effects of humidity on combustion characteristics.
应用计算流体动力学软件FLUENT，对QD128航改燃气轮机燃烧室进行了三维数值模拟计算分析。
The 3D numerical simulation of the QD128 aero-derivative gas turbine combustor was performed by using computational fluid dynamics(CFD) software FLUENT.
研究还发现柔和燃烧具有较高的燃料适应性和变负荷性能，验证了柔和燃烧应用于燃气轮机燃烧室的可行性。
It is found that mild combustion is of wide fuel flexibility and load flexibility, which reflects the feasibility of mild combustion of gas turbine combustor application.
采用数值模拟方法对燃用天然气的某型航改燃气轮机环形燃烧室进行三维流场分析。
The three-dimensional flow field of annular combustor for aero-derivative gas turbine burning gas fuel was numerically simulated.
复合热障涂层是有用的燃气轮机部件，如密封环段，叶片部分罩，转换和燃烧室。
The composite thermal barrier coating is useful on combustion turbine components such as ring seal segments, vane segment shrouds, transitions and combustors.
本文在注蒸汽联合循环和余热锅炉型联合循环的基础上提出了采用烟气再循环和燃烧室回注水的燃气轮机循环，并对其进行了分析和优化。
Ultrafine pulverized-coal contained in the tertiary air was used as the reburning fuel and the oxygen level of the tertiary air was reduced with the use of flue gas recirculation(FGR).
本文在注蒸汽联合循环和余热锅炉型联合循环的基础上提出了采用烟气再循环和燃烧室回注水的燃气轮机循环，并对其进行了分析和优化。
Ultrafine pulverized-coal contained in the tertiary air was used as the reburning fuel and the oxygen level of the tertiary air was reduced with the use of flue gas recirculation(FGR).
应用推荐