Aircraft Cryogenic Tank Walls With Integrated Sensor Tracks

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Solution Overview

Problem

Current methods for monitoring cryogenic liquid tanks in aircraft, such as those using optical fibers or wireless sensor networks, face challenges in power supply and design complexity, with energy harvesting being non-viable in all cases and requiring tailored designs.

Innovation Solution

A cryogenic liquid tank with an electrically conductive track structure formed on the tank walls, integrating sensors directly onto the tank body, allowing for power and data transfer without cables, and utilizing sensors like capacitive, resistive, thermocouple, or radiofrequency sensors for distributed measurement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If optical fibers or wireless sensor networks are used for monitoring, then measurement capability is improved, but device complexity and power supply requirements worsen

Engineering Contradiction:
Improvedistributed measurement capabilityVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent combines the sensor network with the tank structure itself by integrating conductive tracks directly into the tank walls. This merging eliminates the need for separate cable systems and external power supplies, as the tank structure serves dual purposes: containing the cryogenic liquid and providing the electrical infrastructure for sensors.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The tank walls are designed to serve multiple functions simultaneously: structural containment, thermal insulation, and electrical conduction for sensors. The conductive tracks integrated into the tank walls provide both structural reinforcement and electrical pathways, eliminating the need for separate cable systems.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Ease of operation

If wireless sensor networks with energy harvesting are used, then cable requirements are reduced, but design complexity and applicability worsen

Engineering Contradiction:
Improvecable-free operationVSAvoiddesign complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The tank structure itself provides the electrical infrastructure needed by sensors through integrated conductive tracks. The system serves itself by using the tank walls as both containment structures and electrical conduits, eliminating the need for external power supplies and complex energy harvesting designs.

Inventive Principle:
Principle #25Self-service

3Reliability

If conventional cable systems are used for sensor power supply, then power delivery is reliable, but installation effort and time worsen

Engineering Contradiction:
Improvepower supply reliabilityVSAvoidinstallation efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent merges the power delivery infrastructure with the tank structure by integrating conductive tracks directly into the tank walls during manufacturing. This eliminates the need for separate cable installation processes, reducing installation time and effort while maintaining reliable electrical connections for sensors.

Inventive Principle:
Principle #5Merging (Combining)

4Ease of manufacture

If sensors are integrated directly onto tank walls, then cabling effort is reduced, but manufacturing complexity worsens

Engineering Contradiction:
Improvecabling effortVSAvoidmanufacturing complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The tank walls are designed to serve multiple functions simultaneously: structural containment, thermal insulation, and electrical conduction. The conductive tracks integrated into the tank walls provide both structural reinforcement and electrical pathways, eliminating the need for separate cable systems and reducing overall manufacturing complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

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

Reduces cabling effort, simplifies manufacturing, and enables redundant electrical networks with integrated multifunctional metal layers, facilitating easier installation and improved monitoring capabilities.

Implementation Method 1

an electrically conductive track structure that is formed on the at least one tank wall and configured for conducting electricity from a terminal to a sensor

Methodology Applied
Scientific EffectElectrical conduction: Conduction (electrical)

Implementation Method 2

oxidizing or letting oxidize the metal material so as to form an insulating substrate layer

Methodology Applied
Scientific EffectOxidation: Oxidation

Data Source

PatentEP4235013B1Cryogenic liquid tank for an aircraft and method for manufacturing the same
Publication Date: 2025.12.31 AIRBUS (SAS)
  • EP4235013B1 patent drawingFigure 1
  • EP4235013B1 patent drawingFigure 2
  • EP4235013B1 patent drawingFigure 3

AI summary

The invention provides improved measures for monitoring and manufacturing tanks for cryogenic liquids. It is proposed that the tank (22) is manufactured in a way that signal and power lines from a control unit (38) to sensors (34) of the cryogenic tank (22) are integrated with the tank walls (24, 26). The conductive track structure (32) so formed has a layer structure (47) that uses the naturally oc-curing or artificially generated insulating layer (48) on the tank wall material as a substrate on top of which conductive paths (32a-d) are formed that connect the sensors (34) to the control unit (38).