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Non-contact aircraft fuel quantity measuring method and system

A non-contact, measurement method technology, applied in the field of non-contact aircraft fuel quantity measurement methods and systems, can solve the problems of low accuracy of detection results and achieve the effect of accurate volume

Active Publication Date: 2019-03-12
ZHENGZHOU UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The present invention provides a non-contact method and system for measuring the amount of fuel oil in an aircraft, which is used to solve the problem of low accuracy of detection results in the prior art when detecting the amount of fuel oil in an aircraft fuel tank

Method used

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  • Non-contact aircraft fuel quantity measuring method and system
  • Non-contact aircraft fuel quantity measuring method and system
  • Non-contact aircraft fuel quantity measuring method and system

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Embodiment Construction

[0056] The technical solutions of the present invention will be further described below in conjunction with specific embodiments.

[0057] System embodiment:

[0058] The non-contact aircraft fuel measuring system provided by this embodiment has a structure such as figure 1 As shown, a laser 2, a camera 3, a roll angle sensor 4 and a pitch angle sensor 5 are arranged on the top of the aircraft fuel tank 1, and the controller is connected to the control end of the laser 2, and connected to the camera 3, the roll angle sensor 4, and the pitch angle sensor 5 signal output terminals; the controller is also connected with a memory, and the memory is stored with a computer program for execution on the controller. When the controller executes the computer program, according to the camera 3, the roll angle sensor 4 and the pitch sensor 5 collected Data, realize the non-contact method of measuring the amount of fuel in the aircraft fuel tank, and calculate the amount of fuel in the ai...

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Abstract

The invention provides a non-contact aircraft fuel quantity measuring method and system. The measuring method includes the steps that a laser device is controlled to emit cross detection light into afuel tank; an image of a fuel surface in the fuel tank is acquired to obtain the coordinates of a cross light intersection in the image of the fuel surface in the fuel tank in an aircraft fuselage coordinate system; the coordinates of the cross light intersection in the image of the fuel surface in the fuel tank in the aircraft fuselage coordinate system are corrected according to the flight attitude of an aircraft to obtain the coordinates of the cross light intersection in the image of the fuel surface in the fuel tank in a reference coordinate system; the volume of fuel in the fuel tank isobtained according to a corresponding relationship between the coordinates of the cross light intersection in the image of the fuel surface in the fuel tank in the reference coordinate system and thequantity of fuel in the fuel tank. By means of the technical scheme, the problem that in the prior art, when the quantity of fuel in the fuel tank of the aircraft is detected, the accuracy of the detection result is low is solved.

Description

technical field [0001] The invention belongs to the technical field of aircraft fuel oil quantity measurement, and in particular relates to a non-contact aircraft fuel oil quantity measurement method and system. technical background [0002] The remaining fuel volume of the aircraft fuel tank is an important parameter for flight. According to it, the continuous flight time of the aircraft can be calculated. Therefore, real-time and accurate measurement and display of the remaining fuel volume of the aircraft fuel tank is very important to complete the flight mission. [0003] In terms of aircraft fuel measurement, capacitive fuel level sensors are mainly used at present. This kind of sensor has been soaked in oil for a long time and has a short service life. Because it uses mechanical methods to change the resistance value, the detection accuracy is not high, and there are also lead wires. The potential danger of explosion caused by discharge; the magnetic float level gauge ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01F22/00
CPCG01F22/00
Inventor 薛均晓徐明亮于海玉潘俊郭毅博
Owner ZHENGZHOU UNIV