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根据目前已有的机载设备和相关仪器,通过飞机滑油的目标温度和实际温度的差异控制设置电液伺服活门、作动器和连杆机构,从而形成闭环式的自动散热系统,达到温度自动调节的目标。本文首先分析了飞机滑油温度调节控制的传统方法 ,在此基础上以飞机发动机温度调节控制入手,对飞机滑油温度自动调节技术进行了研究,给出了一些自己的看法和建议。
According to the existing airborne equipment and related instruments, the electro-hydraulic servo valve, actuator and connecting rod mechanism are controlled by the difference between the target temperature and the actual temperature of the aircraft oil to form a closed-loop automatic cooling system, and the temperature Automatic adjustment of the target. This paper first analyzes the traditional method of aircraft oil temperature regulation and control. Based on this, the control of aircraft engine temperature is started. The technology of automatic regulation of aircraft oil temperature is studied. Some opinions and suggestions are given.