论文部分内容阅读
文中给出了在S1A - 0 2燃机上进行压气机级间喷水的实验方案 ,并给出按等功率及等涡轮出口温度运行条件下 ,发动机各主要性能参数在不同工况下随喷水量的变化规律。依据实验 ,总结出压气机级间喷水对燃机性能影响的结论。
In this paper, the experimental scheme of the compressor sprayed on the S1A - 0 2 gas turbine is given. Under the operating conditions of equal power and turbine outlet temperature, the main performance parameters of the engine under different operating conditions The amount of change. Based on the experiment, the conclusion is drawn that the influence of the jet water between compressor stages on the performance of the gas turbine.