Aircraft Cryogenic Tank Walls With Integrated Sensor Power Tracks

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Solution Overview

Problem

Current methods for monitoring cryogenic liquid tanks in aircraft, such as using optical fibers and sensor networks, require extensive cabling for power supply, which is complex and not always viable, especially considering the harsh cryogenic environments and large temperature ranges.

Innovation Solution

Integration of electrically conductive tracks directly onto the tank walls to replace cables, allowing for power and data transfer to sensors, with sensors being either integral to the tracks or separately mounted, and using metal layers for conductive paths and insulation, enabling reduced cabling effort and easier manufacturing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If optical fibers or sensor networks are used for monitoring, then measurement capability is improved, but device complexity increases due to extensive cabling requirements

Engineering Contradiction:
Improvemonitoring capabilityVSAvoidcabling complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent combines the sensor mounting structure with the electrical connection function into a single integrated component. The sensor mounting structure includes integrated conductive elements that directly electrically connect the sensor to the tank wall, eliminating the need for separate cabling and reducing overall system complexity while maintaining monitoring capability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The sensor mounting structure serves multiple functions simultaneously: it mechanically mounts the sensor to the tank wall, provides electrical connection through integrated conductive elements, and acts as part of the overall sensing system. This multi-functionality reduces the number of separate components needed and simplifies the overall system architecture.

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

2Measurement precision

If sensors are mounted on tank walls, then monitoring is enabled, but manufacturing complexity increases

Engineering Contradiction:
Improvemonitoring capabilityVSAvoidmanufacturing complexity
Core Design Contradiction:
Measurement precisionVSEase of manufacture

Solution Approach 1:

The sensor mounting structure combines mechanical mounting and electrical connection functions into a single integrated component that is manufactured as one piece. This integration simplifies the manufacturing process by reducing the number of assembly steps and components, while still enabling effective sensor mounting and monitoring.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The sensor mounting structure is designed and prepared in advance during the tank manufacturing process, with conductive elements pre-integrated into the structure. This preliminary preparation simplifies subsequent sensor installation and reduces manufacturing complexity by having connection pathways ready before sensors are mounted.

Inventive Principle:
Principle #10Preliminary action

3Use of energy by moving object

If extensive cabling is used for power supply, then power delivery is ensured, but weight increases

Engineering Contradiction:
Improvepower supply capabilityVSAvoidcable weight
Core Design Contradiction:
Use of energy by moving objectVSWeight of moving object

Solution Approach 1:

The patent extracts the electrical connection function from separate external cables and integrates it directly into the sensor mounting structure. The conductive elements are built into the mounting structure itself, eliminating the need for separate cabling and thereby reducing the overall weight of the system while maintaining power supply capability.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The mounting structure merges the mechanical support function with the electrical connection function, creating a single component that both holds the sensor and provides electrical pathways. This consolidation eliminates redundant materials and reduces weight compared to using separate mounting brackets and cables.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS20230271715A1Cryogenic liquid tank for an aircraft and method for manufacturing the same
Publication Date: 2023.08.31 AIRBUS (SAS)
  • US20230271715A1 patent drawing
  • US20230271715A1 patent drawing
  • US20230271715A1 patent drawing

AI summary

Measures for monitoring and manufacturing tanks for cryogenic liquids. The tank is manufactured in a way that signal and power lines from a control unit to sensors of the cryogenic tank are integrated with the tank walls. The conductive track structure so formed has a layer structure that uses the naturally occurring or artificially generated insulating layer on the tank wall material as a substrate on top of which conductive paths are formed that connect the sensors to the control unit.