With the help of a quasi nonlinear method set up was the mathematical model of a three shaft gas turbine.
本文作者采用准非线性方法建立了三轴式燃气轮机数学模型。
A simple mathematical model with high accuracy is essential to the control of a single shaft gas turbine.
建立单轴燃气轮机简单但又具有足够精度的数学模型，对其控制是十分重要的。
The results of simulation agree quite well with actual physical processes. Hence, the proposed model can be employed for the study of a single shaft gas turbine and its control system.
模拟结果与实际物理过程相吻合，因此，此模型可以用于单轴燃气轮机及其控制系统的研究。
Applying the method of combining the mechanism analysis modeling and gray box modeling, the mathematic model of the single-shaft gas turbine generating units and the control system was established.
应用机理分析建模和灰箱建模相结合的方法，建立了单轴燃气轮机发电机组及其控制系统的数学模型。
Its medium is blast furnace gas which is inflammable, explosive and toxicant. Therefore, the shaft end sealing system of a turbine expander must be safe and reliable, and has economic running.
由于其介质为高炉煤气，属于易燃、易爆、有毒气体，所以要求透平膨胀机的轴端密封系统必须安全可靠，且运行经济。
The latest stage in this development process is a single-shaft arrangement with the generator located between the gas and steam turbine.
这一过程的最新阶段是设计出一种将发电机置于燃气轮机和汽轮机之间的单轴布置方案。
For large gas-turbine generator or single-shaft units which is started with synchronized motors 2 sets of SFC devices with mutual stand-by should be provided for 2 or 3 generators.
对于以同步马达运行方式启动的大型燃气轮发电机或单轴机组的发电机，每2台或3台发电机装设2套互为备用的SFC装置。
The main shaft between the air compressor and the gas turbine in a jet aircraft engine is hollow to permit an internal speed reduction shaft with the minimum requirement of space and weight.
在喷气式飞机发动机内位于空气压缩和燃气涡轮之间的主轴是空心的，允许有一个需要最小空间和重量的内部减速轴。
The main shaft between the air compressor and the gas turbine in a jet aircraft engine is hollow to permit an internal speed reduction shaft with the minimum requirement of space and weight.
在喷气式飞机发动机内位于空气压缩和燃气涡轮之间的主轴是空心的，允许有一个需要最小空间和重量的内部减速轴。
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