Aircraft Fuel Filter Bypass Valve with Dual Pressure Sensors

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Solution Overview

Problem

Existing aircraft fuel supply systems with filter bypass mechanisms are complex, costly, and heavy, lacking a simple architecture for effectively managing fuel filter clogs and maintaining fuel flow without significant weight and packaging burdens.

Innovation Solution

A fuel supply system incorporating a fuel supply line, a fuel filter, a filter bypass line, and a filter bypass valve with two differential pressure sensors, where the valve moves between positions to selectively bypass the filter based on pressure thresholds, allowing continuous and selective pressure sensing to manage clogs and alert personnel.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a filter bypass mechanism is implemented to handle fuel filter clogs, then fuel flow reliability is improved, but system complexity and weight increase

Engineering Contradiction:
Improvefuel flow reliabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The fuel filter system performs self-diagnosis and self-bypass activation through differential pressure sensors that automatically detect filter clogging conditions and trigger the bypass valve without requiring external intervention or complex control systems

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The bypass functionality is extracted as a separate, independently controllable valve mechanism that can be activated only when needed, rather than being integrated into the main filter assembly, reducing overall system complexity while maintaining reliability

Inventive Principle:
Principle #2Taking out (Extraction)

2Reliability

If a filter bypass mechanism is implemented to handle fuel filter clogs, then fuel flow reliability is improved, but system weight increases

Engineering Contradiction:
Improvefuel flow reliabilityVSAvoidsystem weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The system uses self-activating bypass valve controlled by differential pressure sensors, eliminating the need for heavy external control systems, actuators, and power supply components while maintaining reliable filter bypass functionality

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The bypass valve is designed as a simple, lightweight component that can be easily replaced or serviced, using basic mechanical elements rather than complex, heavy-duty components

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

3Measurement precision

If continuous pressure sensing is used to detect filter clogs, then detection accuracy is improved, but device complexity increases

Engineering Contradiction:
Improvedetection accuracyVSAvoiddevice complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

A differential pressure sensor serves as an intermediary device that indirectly measures filter clogging by detecting pressure difference across the filter, providing accurate detection without requiring direct measurement of filter blockage or complex sensor arrays

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The differential pressure sensor automatically provides continuous monitoring and triggers bypass activation when clogging is detected, eliminating the need for manual inspection or complex diagnostic systems

Inventive Principle:
Principle #25Self-service

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

This solution provides a simpler, lighter, and more cost-effective fuel supply system architecture that ensures uninterrupted fuel flow while alerting personnel to filter clogs and bypass conditions, offering significant weight and packaging benefits over existing systems.

Implementation Method 1

The first differential pressure sensor is configured to continuously sense differential pressure across the fuel filter

Methodology Applied
Scientific EffectDifferential pressure sensing: Pressure Drop

Implementation Method 2

the second differential pressure sensor is configured to selectively sense differential pressure across the fuel filter

Methodology Applied
Scientific EffectDifferential pressure sensing: Pressure Drop

Implementation Method 3

The filter bypass valve is coupled to the filter bypass line and is movable between a first position, in which only the first differential pressure sensor senses differential pressure across the fuel filter, and a second position, in which the first differential pressure sensor and the second differential pressure sensor both sense differential pressure across the fuel filter

Methodology Applied
Scientific EffectPressure differential flow control: Pressure Drop

Data Source

PatentUS9441598B2Aircraft fuel filter impending and actual bypass indication system
Publication Date: 2016.09.13 HONEYWELL INTERNATIONAL INC
  • US9441598B2 patent drawing
  • US9441598B2 patent drawing
  • US9441598B2 patent drawing

AI summary

A fuel supply system includes a fuel supply line, a fuel filter, a filter bypass line, a first differential pressure sensor, a second differential pressure sensor, and a filter bypass valve. The fuel filter is disposed in series in the fuel supply line to remove particulate from the fuel. The filter bypass line has a fuel inlet upstream of the fuel filter, and an outlet that is downstream of the fuel filter. The first differential pressure sensor continuously senses differential pressure across the fuel filter, and the second differential pressure sensor selectively senses differential pressure across the fuel filter. The filter bypass valve is movable between a first non-bypassing position and a second bypassing position and controls whether only the first differential pressure sensor or both the first and second differential pressure sensors sense the differential pressure across the fuel filter.