Aircraft Fuel Management System Dynamic Reserve Optimization

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Solution Overview

Problem

Aircraft fuel management systems face challenges in reducing fuel reserves while maintaining flight safety, as existing methods do not effectively account for unforeseen flight conditions, leading to increased fuel consumption and weight.

Innovation Solution

A fuel management system that compares theoretical and actual fuel consumption values during flight, initiating measures such as reducing flight speed or adjusting on-board energy consumption to optimize fuel use, allowing for a reduction in reserve fuel without compromising safety.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If the quantity of reserve fuel carried on board is reduced to lower the aircraft weight, then fuel consumption and operating costs are reduced, but flight safety may be compromised due to insufficient fuel reserves for unforeseen events

Engineering Contradiction:
Improveaircraft weightVSAvoidflight safety
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The fuel management system continuously monitors actual fuel consumption and compares it with planned consumption, providing feedback to the flight crew when deviations exceed thresholds. This real-time feedback enables dynamic adjustment of fuel reserves based on actual flight conditions rather than static pre-flight calculations, allowing reduced reserve fuel while maintaining safety through active monitoring and intervention capabilities

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system transitions from static fuel reserve calculations to dynamic fuel management by continuously adapting fuel consumption assessments to actual flight conditions. The fuel reserve requirement changes dynamically based on real-time monitoring of consumption patterns, enabling the system to optimize the balance between weight reduction and safety margins throughout the flight

Inventive Principle:
Principle #15Dynamics

2Device complexity

If traditional fuel management methods are used without real-time monitoring, then system complexity is reduced, but fuel consumption increases due to inability to detect and respond to deviations from planned consumption

Engineering Contradiction:
Improvefuel management system complexityVSAvoidfuel consumption
Core Design Contradiction:
Device complexityVSUse of energy by moving object

Solution Approach 1:

The system implements continuous feedback loops that monitor actual fuel consumption against planned consumption, automatically detecting deviations and triggering alerts or automated responses. This feedback mechanism enables the system to respond dynamically to changing flight conditions, optimizing fuel usage without requiring overly complex manual intervention procedures

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The fuel management system performs self-monitoring and self-assessment of fuel consumption patterns, automatically comparing actual consumption with planned consumption and initiating appropriate responses without requiring constant pilot intervention. This self-service capability reduces the operational burden on the flight crew while maintaining effective fuel management

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS8888046B2Fuel management system
Publication Date: 2014.11.18 AIRBUS OPERATIONS GMBH
  • US8888046B2 patent drawing
  • US8888046B2 patent drawing
  • US8888046B2 patent drawing

AI summary

A computer implemented fuel management method and system for monitoring and minimizing a fuel consumption of an aircraft. The fuel management system and method determines, on the basis of model assumptions, a theoretical value relating to the quantity of fuel that is necessary for travelling along at least one sector of a flight route. Furthermore, the fuel management system and method determine a practical value relating to a quantity of fuel that is necessary for travelling along the same sector of the flight route, taking into account actual measured values. Moreover, the system and method compare the theoretical value with the practical value and to provide at least one measure in order to save fuel during a flight when the practical value differs from the theoretical value by a predeterminable amount.