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航空发动机测量装置用于测量发动机某特定部位的温度、压力等参数。基于ANSYS分析软件对某型航空发动机测量装置在发动机工作时的高温条件下进行数据采集时的温度场进行了模拟,分析了测量装置的温度场变化规律,提取了测量装置上特征点的温度变化曲线,为测量装置结构优化提供了依据。
Aero-engine measuring device is used to measure the temperature, pressure and other parameters of a specific part of the engine. Based on the ANSYS analysis software, the temperature field of a certain type of aero-engine measuring device during data acquisition under high temperature during engine operation was simulated. The variation law of the temperature field of the measuring device was analyzed. The temperature change of the characteristic points of the measuring device Curves provide the basis for the optimization of the measuring device structure.