Airborne fuel system fuel consumption estimation and health monitor method

A fuel system and health monitoring technology, which is applied in the direction of neural learning methods, instruments, biological neural network models, etc., can solve the problems of not considering engine performance attenuation, incomplete consideration of factors, and increased fuel consumption rate, so as to reduce maintenance positioning time , reduce fuel consumption costs and improve maintenance efficiency

Inactive Publication Date: 2019-04-09
CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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AI Technical Summary

Problems solved by technology

[0003] Most of the existing fuel consumption estimation methods are estimating the fuel consumption of the cruising section, and cannot predict the fuel consumption of the whole course of flight, and a large part of the fuel consumption of short-range flights depends on the stage of take-off, climbing and landing, so these methods are not suitable for practical engineering applications
These methods also seldom take into account the impact of weather, horizontal plane movement, acceleration and other factors on fuel consumption, and the factors considered are not comprehensive. Generally, the impact of weather (wind, temperature) on fuel is not considered, let alone the engine performance attenuation and the smoothness of the fuselage. Increased fuel consumption due to variation
In terms of monitoring and isolation of fuel system failures and abnormalities, the health monitoring method mainly relies on the self-test software of the fuel system to provide health information to the on-board maintenance system, and fails to make full use of aircraft flight data, and there is room for improvement

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  • Airborne fuel system fuel consumption estimation and health monitor method
  • Airborne fuel system fuel consumption estimation and health monitor method
  • Airborne fuel system fuel consumption estimation and health monitor method

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Embodiment Construction

[0029] The specific embodiments of the present invention will be further described below with reference to the accompanying drawings.

[0030] The technical scheme of the present invention is: an airborne fuel system fuel consumption estimation and health monitoring method, comprising the following steps:

[0031] Step 1: Data sample processing:

[0032] 1.1) Carry out packet loss, addition and deletion processing on the original flight data to form complete and usable original flight data, and then complete the marking of the original flight data according to the record data of fuel system failures and abnormal events;

[0033] The present invention adopts the complete QAR data of a certain flight of a certain type of BOEING (737-300) as the experimental database. QAR data records about 250 parameters, including important parameters such as engine parameters, airspeed, ground speed, pressure altitude, etc. There are analog quantities, digital signals, switch quantities, etc....

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Abstract

The invention relates to an airborne fuel system fuel consumption estimation and health monitor method. The method comprises the following steps of: processing a data sample; building and training a fuel consumption estimation model; integrating the whole leg by taking a fuel flow predicted value and flight time as marks, so as to obtain a predicted value of a fuel consumption gross of a flight inone flight; on the basis of an obtained fuel flow model, adding channels of flight faults and abnormal events for an output layer; inputting obtained training data sample into the fuel flow model improved in the fourth step as a training sample, and carrying out training to obtain fuel flow model which is capable of monitoring airplane faults and abnormities according to airplane data; and inputting data of unmarked faults and abnormities which only undergo packet loss and addition/deletion processing into the fuel flow model improved in the fifth step as test data, so as to monitor the dataof unknown faults and abnormities.

Description

technical field [0001] The invention belongs to the field of aviation fuel systems, and relates to a fuel consumption estimation and health monitoring method for an airborne fuel system. Background technique [0002] For civil aviation companies, aviation fuel cost control and fuel system operation safety are one of their most concerned contents. Airlines at home and abroad have carried out work and research on fuel systems around fuel saving. important issues for the company. The basic idea is to analyze and study the factors that affect aviation fuel consumption, and establish an aircraft fuel consumption estimation model, so as to improve the fuel estimation accuracy of the flight plan route and reduce the fuel consumption cost. At the same time, in terms of monitoring and isolating the failure and abnormality of the fuel system, the health monitoring method is mainly completed through the self-test software and hardware of the fuel system. [0003] Most of the existing...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G07C5/08G07C5/00G06N3/08
CPCG06N3/084G07C5/006G07C5/0808
Inventor 潘震张竞凯池程芝李铁颖
Owner CHINESE AERONAUTICAL RADIO ELECTRONICS RES INST
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