Aircraft Tank Level Sensing via Remote Connector Access

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing aircraft oil reservoirs require accessible positioning for level checks, limiting their placement flexibility and necessitating power availability for monitoring.

Innovation Solution

An aircraft tank with an integrated electrical level sensor and remote connector system, allowing level monitoring via a cable loop circuit independent of the aircraft's power supply, enabling access from a distance and during propulsion system shutdown.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the tank is positioned in an inaccessible location, then the aircraft design flexibility is improved, but the ease of operation for level monitoring deteriorates

Engineering Contradiction:
Improvetank placement flexibilityVSAvoidlevel monitoring accessibility
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The patent replaces the mechanical/visual inspection method (requiring physical access to the tank) with an electrical sensing system. The level sensor electrically detects liquid level and transmits signals remotely, eliminating the need for operator access to the tank location.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent introduces an intermediary measurement system between the liquid and the operator. The level sensor acts as an intermediary that converts liquid level information into electrical signals, which are then transmitted to the operator without requiring direct access to the liquid.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If the level sensor is connected to the aircraft power supply, then the measurement precision is improved, but the ease of operation during shutdown deteriorates

Engineering Contradiction:
Improvelevel signal accuracyVSAvoidmonitoring during shutdown
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The patent makes the power supply configuration dynamic and adaptable. The level sensor can operate in two modes: powered by the aircraft electrical system during operation, or by its own battery during shutdown, allowing the system to adapt to different operational states.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The level sensor is equipped with an autonomous power source (battery) that allows it to independently monitor liquid levels without relying on the aircraft's power supply. This self-service capability ensures continuous monitoring regardless of aircraft operational state.

Inventive Principle:
Principle #25Self-service

3Ease of operation

If a remote connector is used for level monitoring, then the ease of operation is improved, but the device complexity increases

Engineering Contradiction:
Improveremote access capabilityVSAvoidcable loop circuit
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The cable bundle serves multiple functions simultaneously: it transmits both power and level signals through a single connection point. This multi-functionality reduces the number of separate connections needed and simplifies the overall system architecture.

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

Solution Approach 2:

The patent combines the power supply connection and the level signal transmission into a single integrated cable assembly. By merging these two functions into one physical connection, the system reduces complexity at the connection point while maintaining remote accessibility.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP4671133A1Aircraft comprising a tank equipped with a level sensor connected to a remote connector and device for controlling a liquid level in such a tank
Publication Date: 2025.12.31 AIRBUS OPERATIONS (SAS)
  • EP4671133A1 patent drawingFigure 1~4
  • EP4671133A1 patent drawing
  • EP4671133A1 patent drawing

AI summary

The invention relates to an aircraft comprising at least one tank (40), at least one electrical level sensor (42) positioned in the tank (40) and configured to generate a level signal (NS) based on the liquid level in the tank (40), at least one first connector (44) located away from the tank (40), and at least one link (46) configured to transmit the level signal (NS) generated by the level sensor (42) and electrical power to supply the level sensor (42), said link (46) connecting the first connector (44) and the level sensor (42). This solution allows for monitoring the fill level of a tank (40) that is difficult to access. The invention also relates to a device (48) for monitoring the liquid level of such a tank by connecting to the first connector (44).