In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change , is hard to be simulated.
航空发动机控制系统半物理模拟试验中，涡轮出口气体温度高、变化快，难以模拟。
The aero-engine combustion outlet temperature makes a strong impact on the life of engine and the power of the engine output.
航空发动机燃烧室出口温度的高低及出口温度场的均匀程度，直接影响到发动机的工作寿命和输出功率的大小。
The principles and calibration method by using this sensor to measure "engine outlet A3 temperature" and "TPU exhaust temperature" are also presented.
并说明了用此传感器来测量“发动机A 3引气口温度”和“TPU排气温度”的原理及校准方法。
The principles and calibration method by using this sensor to measure "engine outlet A3 temperature" and "TPU exhaust temperature" are also presented.
并说明了用此传感器来测量“发动机A 3引气口温度”和“TPU排气温度”的原理及校准方法。
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