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为了防止刹车温度过高,现代大型民航飞机采用刹车温度监控系统监控机轮温度。该系统由温度传感器、数据处理组件和显示组件组成。基本工作原理为:温度传感器感感受到机轮温度并传递给数据处理组件,数据处理组件将接收到的数据进行比较处理后,传给显示组件。早期飞机上,整个数据的传递和显示是以模拟信号进行的,而现在先进的飞机则通过数据处理组件将模拟信号转换为数字信号,以更直观的方式显示。温度探测与数据的形成传输温度传感器是一个热敏感型电阻元件,位于每个机轮刹车毅的扭力杆内。它根据轮子刹车时产生的不同温
In order to prevent the brake temperature is too high, the modern large civil aviation aircraft brake temperature monitoring system to monitor the wheel temperature. The system consists of temperature sensors, data processing components and display components. The basic working principle is as follows: the temperature sensor senses the temperature of the wheel and transmits it to the data processing component, and the data processing component compares the received data to the display component. Early aircraft, the entire data transmission and display is based on analog signals, and today’s advanced aircraft through the data processing components will convert analog signals into digital signals, a more intuitive way to display. Temperature detection and data transmission Temperature sensor is a heat-sensitive resistance element, located in each wheel brake Yi torque rod. It is based on the different temperatures generated when the wheels brake