Aircraft Hydrogen Pipe Connector Jacket for Leak Containment

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Solution Overview

Problem

Existing systems for transporting gaseous hydrogen in aircrafts face challenges in optimizing adaptability and reducing leakage probability in complex aircraft structures, particularly at pipe connections.

Innovation Solution

A system comprising a first and second pipe connected by a connector, surrounded by a protective jacket made of flexible material like nitrile rubber, with an orienting device and a sensor for detecting leaks, to enhance reliability and minimize hydrogen leakage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If pipe sections are connected one to another using connectors, then adaptability to different aircraft structures is improved, but leakage probability increases at connection zones

Engineering Contradiction:
Improveadaptability to different aircraft structuresVSAvoidleakage probability at connection zones
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

A flexible protective jacket made of elastomeric material (such as nitrile rubber) is disposed around the connecting zone of pipe sections. The jacket acts as a flexible barrier that contains potential hydrogen leaks at connection points while maintaining adaptability to different aircraft structures through modular pipe section design.

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The protective jacket serves as an intermediary element between the pipe connection and the external environment. It mediates by containing any potential hydrogen leakage within the jacket, preventing direct release into the aircraft environment while allowing the connection to function normally.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If a protective jacket is added around the connecting zone, then leakage probability is reduced, but device complexity increases

Engineering Contradiction:
Improveleakage probability reductionVSAvoidsystem component quantity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The protective jacket is implemented as a simple flexible sleeve rather than a complex mechanical containment system. This single-component approach reduces overall system complexity compared to rigid containment structures while effectively addressing leakage concerns.

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The protective jacket is designed as a simple, replaceable component that can be easily installed and removed. If degradation or damage occurs, the entire jacket can be replaced as a single unit without affecting the pipe connection itself, simplifying maintenance procedures.

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

3Stability of the object's composition

If the protective jacket is made of flexible material like rubber, then it can accommodate movement and vibration, but manufacturing precision requirements increase

Engineering Contradiction:
Improveaccommodation of movement and vibrationVSAvoidjacket fitting precision
Core Design Contradiction:
Stability of the object's compositionVSManufacturing precision

Solution Approach 1:

The protective jacket is made of flexible elastomeric material that can deform and conform to the pipe connection geometry. This flexibility compensates for manufacturing tolerances and allows the jacket to accommodate thermal expansion, vibration, and movement without requiring extremely tight manufacturing precision.

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The elastomeric material properties (such as durometer hardness and elasticity) are selected to provide optimal balance between flexibility for movement accommodation and sufficient structural integrity for leak containment. The material parameters are chosen to ensure proper fit without requiring ultra-precise manufacturing.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentEP4671588A1System for transporting gaseous hydrogen in an aircraft
Publication Date: 2025.12.31 AIRBUS OPERATIONS (SAS)
  • EP4671588A1 patent drawingFigure 1
  • EP4671588A1 patent drawingFigure 2~3
  • EP4671588A1 patent drawingFigure 4

AI summary

A system (1) for transporting a gaseous fluid, like dihydrogen, comprising a first pipe for transporting said fluid, called first pipe (2), a second pipe for transporting said fluid, called second pipe (3), and a connector (4) arranged to connect an end, called first connecting end (6), of the first pipe (2) to an end, called second connecting end (7), of the second pipe (3), a zone (Z) comprising the first connecting end (6) of the first pipe (2), the second connecting end (7) of the second pipe (3) and the connector (4) being called connecting zone (Z), the system (1) comprising a protective jacket (5) around the connecting zone (Z) against said first and second connecting ends (6, 7) and said connector (4).