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Method and electronic device for providing an optimal quantity of aircraft fuel

A technology for electronic equipment and aircraft, applied in instruments, data processing applications, forecasting, etc., can solve problems such as increasing aircraft weight and total fuel flight cost

Pending Publication Date: 2018-09-25
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although loading extra fuel reduces the risk that an aircraft may need to be redirected due to low fuel, loading extra fuel increases aircraft weight, total fuel burned, and overall flight cost

Method used

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  • Method and electronic device for providing an optimal quantity of aircraft fuel
  • Method and electronic device for providing an optimal quantity of aircraft fuel
  • Method and electronic device for providing an optimal quantity of aircraft fuel

Examples

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Embodiment Construction

[0034] The present disclosure relates to methods and electronics for providing and loading an optimum amount of aircraft fuel. figure 1 An exemplary flowchart representing method 100 is shown. Empirical flight data 102 from past flight records of the aircraft is collected to determine 104 aircraft specific performance correction parameters for each flight phase (typically, each of climb, cruise, and landing flight phases). exist figure 1 In an embodiment of the present invention, aircraft specific performance correction parameters 106 include drag and fuel factors for each of climb, cruise, and landing phases of flight Aircraft specific performance correction parameters 106 may be calculated, for example, by an aircraft performance monitoring (APM) tool.

[0035] At step 110 , the total fuel required 114 for a given flight plan 108 is determined using aircraft specific performance correction parameters 106 (eg, via a flight planning tool). Optionally, additional data 112 -...

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PUM

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Abstract

A method and electronic device for providing an optimal quantity of aircraft fuel. The method comprises collecting recorded flight data (102) from past flights of an aircraft; determining (104) aircraft specific performance correction parameters (106) per flight phase, using the recorded flight data (102); collecting a flight plan (108) of the aircraft; determining (110) the total fuel required (114) for the given flight plan (108), using the aircraft specific performance correction parameters (106); determining (116) a single synthetic drag factor ([epsilon]D<FMS>) and a single synthetic fuelfactor ([epsilon]FF<FMS>) that, when used by the aircraft FMS, yield the said total fuel required (114) for the given flight plan (108); receiving an estimated total fuel required (122) determined bythe aircraft FMS based on the flight plan (108), the single synthetic drag factor ([epsilon]D<FMS>) and the single synthetic fuel factor ([epsilon]FF<FMS>). The method allows reducing the fuel weightand total flight cost, and is particularly advantageous for FMS which only admit one single drag factor and one single fuel factor.

Description

technical field [0001] The present disclosure is within the field of avionics and relates to methods and systems for improving aircraft performance. More specifically, it is an object of the present disclosure to estimate more accurate fuel consumption for a determined flight plan and to reduce the amount of fuel loaded onto an aircraft prior to execution of a given flight plan. Background technique [0002] Fuel estimates are typically used to determine fuel requirements for a given flight plan. The fuel estimate can then be used to determine how much fuel to load for a particular flight. Therefore, the accuracy of fuel estimates may be important for flight planning. If the estimate is lower than the calculated probable fuel requirement, then not enough fuel may not have been loaded for the flight. Alternatively, if the estimated value exceeds the calculated required amount of fuel, then more fuel may be loaded than required, which may add unnecessary weight to the fligh...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/04G06Q50/30
CPCG06Q10/04G06Q50/40G08G5/0034G08G5/0091G08G5/0039G06Q10/047G07C5/085G07C5/12
Inventor D·加里-洛佩兹M·C·沃斯J·德普林斯A·J·G·T·斯库泰斯
Owner THE BOEING CO
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