发明名称 AIRCRAFT FUEL MEASUREMENT
摘要 A method of estimating a quantity of a liquid fuel in a fuel tank of an aircraft is disclosed. A surface of the fuel is illuminated with light so that the light is reflected or scattered by the surface of the fuel onto an array of sensors. The light travels to and from the surface of the fuel via a measurement path containing a transmission medium. A measured time of flight is made at each sensor for the light which travels via the measurement path to that sensor. At least one of the sensors is illuminated with light via a reference path containing a transmission medium with substantially the same refractive index as the transmission medium in the measurement path, the reference path having a known reference distance which does not vary in accordance with the quantity of the fuel.
申请公布号 US2017003157(A1) 申请公布日期 2017.01.05
申请号 US201615189511 申请日期 2016.06.22
申请人 AIRBUS OPERATIONS LIMITED 发明人 CIPULLO Alessio;BURNELL Stephen;LAM Joseph K-W
分类号 G01F23/292;G01S17/10;B64D37/00 主分类号 G01F23/292
代理机构 代理人
主权项 1. An aircraft fuel tank system comprising: a fuel tank; an array of sensors; a light source arranged to illuminate a surface of a liquid fuel in the fuel tank with light so that the light is reflected or scattered by the surface of the fuel onto the array of sensors, the light travelling to and from the surface of the fuel via a measurement path containing a transmission medium, wherein the light source is also arranged to illuminate at least one sensor of the array of sensors with light via a reference path containing a transmission medium with substantially the same refractive index as the transmission medium in the measurement path, the reference path having a known reference distance which does not vary in accordance with the quantity of the fuel; and a processing system arranged to determine a measured time of flight of the light which travels via the measurement path to each sensor of the array of sensors, measure a reference time of flight of the light which travels via the reference path to said at least one sensor, and estimate the quantity of the fuel in the fuel tank in accordance with the measured times of flight, the reference time of flight and the known reference distance.
地址 Bristol GB
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