Analyzed the reasons for the rising of primary exit temperature of twin screw compressor, put forward corresponding solutions, which were proven to be effective by equipment repair and commissioning.

针对双螺杆压缩机一级出口温度逐渐升高的原因进行分析，提出相应的解决措施，并通过设备检修试车进行了进一步论证。

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This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.

本文研究利用不同飞行状态下测量的发动机变量估计涡轮进口温度和压气机出口压力。

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