These results can provide some reference for maintain and design for gas turbine combustor.
本文研究结果可为发动机火焰筒的维修和改进设计提供参考。
The 3D numerical simulation of the QD128 aero-derivative gas turbine combustor was performed by using computational fluid dynamics(CFD) software FLUENT.
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。
A gas turbine combustor includes a pilot burner, and a plurality of main burners disposed around the periphery of the pilot burner on the radially outer side.
一种燃气轮机燃烧装置，包括：引燃燃烧器；以及在引燃燃烧器周围的半径方向外侧设置的多个主燃烧器。
The effect of combustor pressure on soot concentration and flame radiation was investigated in a small model gas turbine combustor with an air-blast atomizer.
在一个小型高压燃烧试验台上研究了燃烧室采用空气雾化喷嘴后，燃烧室压力对燃烧室内烟粒浓度和火焰辐射的影响。
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.
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。
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.
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。
The three-dimensional flow field of annular combustor for aero-derivative gas turbine burning gas fuel was numerically simulated.
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 formation mechanism of bulging and cracking of combustor inner liner and his influence on gas turbine exhaust temperature dispersity was analyzed.
分析了火焰筒鼓包和破裂的形成机制对燃气轮机排气温度分散度的影响，提出了相应措施，以防止因燃烧恶化对热通道部件的伤害。
The formation mechanism of bulging and cracking of combustor inner liner and his influence on gas turbine exhaust temperature dispersity was analyzed.
分析了火焰筒鼓包和破裂的形成机制对燃气轮机排气温度分散度的影响，提出了相应措施，以防止因燃烧恶化对热通道部件的伤害。
应用推荐