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Some aspects of COTS ultrasonic fuel level measurement

机译:COTS超声波燃油液位测量的某些方面

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The paper focuses on utilization of modern level sensors for measuring fuel volume in aviation. Ultrasonic principles of fuel quantity measurement have been introduced onboard aircraft to replace float level and capacitance level sensors. The principle of ultrasonic measurement of the fuel level is based on the reflection of sound waves at an interface of fuel and air. The fuel quantity can be calculated from fuel level if the shape of the tank is known. Specific electronic circuits were designed to employ ultrasonic transceivers operating at higher frequencies. Presented experiments compare characteristics of different ultrasonic sensors for installation in the aircraft fuel quantity measuring system. Tested operating conditions of several COTS ultrasonic sensors are focused on simulation of aircraft attitude changes.
机译:本文着重于利用现代液位传感器测量航空燃油量。飞机上已引入了燃油量测量的超声波原理,以取代浮球液位和电容液位传感器。超声波测量燃油油位的原理是基于声波在燃油和空气界面处的反射。如果油箱的形状已知,则可以根据油位计算出燃油量。特定的电子电路被设计为采用在更高频率下工作的超声波收发器。提出的实验比较了安装在飞机燃油量测量系统中的不同超声波传感器的特性。几个COTS超声传感器的经测试运行条件集中于模拟飞机姿态变化。

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