Aircraft Vent Tank Flame Barrier Design

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Solution Overview

Problem

Aircraft fuel tank systems face issues with high-pressure surges of liquid fuel during filling, which can damage the system, especially when fuel is cold and viscous, and vent tanks are often space-inefficiently located, requiring effective pressure equalization and venting solutions.

Innovation Solution

The system incorporates a vent tank with a minimal ullage design, a vent pipe for direct fluid flow, and flame barrier means within the vent pipe to prevent flame ingress and facilitate liquid fuel egress, along with ice screen means to prevent ice buildup, ensuring efficient venting and space optimization.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If vent tanks are designed with larger liquid fuel capacity to handle surges, then fuel surge capacity is improved, but space efficiency deteriorates

Engineering Contradiction:
Improveliquid fuel surge capacityVSAvoidvent tank volume
Core Design Contradiction:
Quantity of substanceVSVolume of moving object

Solution Approach 1:

The patent positions the vent tank in the wing tip area, utilizing the lateral/directional space rather than increasing vertical depth. This dimensional approach allows the vent tank to handle fuel surges without compromising the space efficiency of the main fuel storage areas, resolving the contradiction between surge capacity and space efficiency.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Volume of moving object

If vent tank is positioned in space-restricted areas like wing tips, then space efficiency is improved, but pressure equalization capability deteriorates

Engineering Contradiction:
Improvespace efficiencyVSAvoidpressure equalization capability
Core Design Contradiction:
Volume of moving objectVSReliability

Solution Approach 1:

The venting system is segmented into multiple components: the vent tank positioned in the wing tip, vent pipes with flame barrier means, and ice screen means. This segmentation allows the vent tank to occupy restricted space while the specialized venting components handle pressure equalization functions, resolving the contradiction between space efficiency and pressure equalization capability.

Inventive Principle:
Principle #1Segmentation

3Device complexity

If conventional venting systems are used, then simplicity is maintained, but protection against flame ingress and ice buildup deteriorates

Engineering Contradiction:
Improveventing system complexityVSAvoidflame ingress and ice buildup
Core Design Contradiction:
Device complexityVSObject-affected harmful factors

Solution Approach 1:

The flame barrier means and ice screen means act as intermediary protective elements within the vent pipe system. These intermediaries block harmful factors (flames and ice) without requiring complete system redesign, thus providing enhanced protection while maintaining relatively simple system architecture.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 configuration effectively manages pressure surges, prevents damage from high-pressure fuel, and optimizes space usage by ensuring efficient venting and flame protection, even in restricted areas like wing tips, while maintaining flow efficiency and safety.

Implementation Method 1

flame barrier means arranged within the vent pipe so as to provide a barrier to ingress to the vent tank of a flame front external to the vent tank

Methodology Applied
Scientific EffectFlame barrier:

Implementation Method 2

a vent pipe having a first open end in fluid communication with the ullage vent means and a second open end positioned within the minimal ullage of the vent tank, the vent pipe being arranged to provide a substantially direct nominally vertical fluid flow path

Methodology Applied
Scientific EffectGravity: Gravitation

Implementation Method 3

Vent tanks are arranged to allow air to flow from atmosphere into the fuel tanks as they are drained and to allow air, fuel vapour or inerting gasses or a mixture of these to flow out of the tanks to atmosphere as the tanks are filled

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Data Source

PatentUS9440728B2Aircraft fuel tank system
Publication Date: 2016.09.13 AIRBUS OPERATIONS LTD
  • US9440728B2 patent drawing
  • US9440728B2 patent drawing
  • US9440728B2 patent drawing

AI summary

An aircraft fuel tank system is disclosed in which a vent tank is provided with a compact vent pipe comprising one or more built-in flame barrier elements providing high liquid fuel outflow rate.