Aircraft Fuel Valve Position Compensation for Accurate Flow Control

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Solution Overview

Problem

Existing fuel flow measurement systems in jet engines suffer from inaccuracies due to errors in FMV position calculations, which affect engine operability and require costly high-precision sensors and uniform LVDT error distribution across channels, increasing costs and weight.

Innovation Solution

Utilizing calibration resistors with position sensors to derive delta curves that compensate for measurement discrepancies, allowing for accurate fuel flow calculation without the need for high-precision LVDT sensors and uniform LVDT error distribution, thereby reducing operational margins and costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If high-precision LVDT sensors are used to measure FMV position, then measurement precision is improved, but device complexity and cost increase

Engineering Contradiction:
ImproveFMV position measurement accuracyVSAvoidsensor requirements
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent uses a copy of the measurement system with two independent measurement channels instead of relying on a single high-precision sensor. Each channel has its own LVDT sensor with potentially different error characteristics, and the system processes both measurements to achieve accurate fuel flow calculation without requiring either individual sensor to be highly precise.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent transforms the problem from measuring absolute FMV position accurately to measuring the difference between two FMV position measurements. By changing the measurement parameter from absolute position to differential position, the system can tolerate larger individual measurement errors while maintaining accurate fuel flow calculation.

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If uniform LVDT error distribution is required across channels, then measurement precision is improved, but manufacturing precision requirements increase

Engineering Contradiction:
Improvefuel flow measurement accuracyVSAvoidLVDT error distribution uniformity
Core Design Contradiction:
Measurement precisionVSManufacturing precision

Solution Approach 1:

The patent explicitly accepts and utilizes the asymmetric nature of LVDT errors across different channels rather than requiring uniform error distribution. The system is designed to handle channels with different error characteristics, transforming a manufacturing constraint into a design feature that simplifies production while maintaining measurement accuracy through differential measurement.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

By implementing two independent measurement channels with potentially different error profiles, the system creates redundancy that allows accurate fuel flow calculation without requiring uniform manufacturing precision across all sensors. The differential approach cancels out individual channel errors.

Inventive Principle:
Principle #26Copying

3Measurement precision

If additional high-precision sensors are added to compensate for measurement errors, then measurement precision is improved, but weight increases

Engineering Contradiction:
Improvefuel flow calculation accuracyVSAvoidsensor weight
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The patent uses existing LVDT sensors in a differential configuration rather than adding new high-precision sensors. By copying the measurement function across two channels and processing the difference, the system achieves accurate fuel flow measurement without the weight penalty of additional high-precision sensing hardware.

Inventive Principle:
Principle #26Copying

4Reliability

If operational margins are increased to account for measurement errors, then reliability is improved, but productivity decreases

Engineering Contradiction:
Improveengine operabilityVSAvoidfuel flow calculation efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent uses dual-channel measurement to directly calculate accurate fuel flow without requiring large operational margins. The differential measurement approach provides inherent error compensation, allowing the system to maintain both high reliability and high productivity by eliminating the need for conservative margin-based corrections.

Inventive Principle:
Principle #26Copying

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enhances fuel flow calculation accuracy and reduces operational margins by compensating for measurement errors, providing a low-cost solution that maintains engine performance without the need for additional sensors, thus optimizing engine efficiency and reducing weight.

Implementation Method 1

This measurement is affected by a certain error

Methodology Applied
Scientific EffectInductance: Electromagnetic Induction

Implementation Method 2

a variable capacitor for providing a feedback signal

Methodology Applied
Scientific EffectCapacitance: Capacitance

Data Source

PatentEP4242441B1Method and apparatus for controlling fuel flow into an aircraft engine
Publication Date: 2025.07.16 GE AVIO SRL
  • EP4242441B1 patent drawingFigure 1
  • EP4242441B1 patent drawingFigure 2
  • EP4242441B1 patent drawingFigure 3

AI summary

Based upon measured resistances, a first delta curve and second delta curve are selected. A first fuel valve position (FVP) is received from a first position sensor (102), and the first FVP is applied to the first delta curve to obtain a first offset. A second FVP is received from a second position sensor (104), and the second FVP is applied to second delta curve to obtain a second offset. The first offset is applied to the first measured FVP to obtain the first compensated FVP and the second offset is applied to the second measured FVP to obtain the second compensated FVP. The first compensated FVP and the second compensated FVP are correlated to obtain a final compensated FVP, which is applied to a desired fuel valve position to obtain a final fuel valve position.