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。
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