Aircraft Fuel Collector Pipe Disconnection Detection Using Fuel Trends

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Solution Overview

Problem

The disconnection of a pipe from an injection pump in an aircraft's fuel collector, although not immediately affecting operation, leads to medium- or long-term wear and potential damage, necessitating costly repairs and grounding of the aircraft.

Innovation Solution

A method and device using a receiver, processor, and transmitter to monitor fuel quantity in the collector, classify values as normal or abnormal, compute a health indicator based on a sliding window of values, and compare it with thresholds to detect pipe disconnection, transmitting a warning when necessary.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the pipe is mechanically separated from the injection pump, then the fuel system can continue operating, but the collector suffers medium- or long-term wear and potential damage

Engineering Contradiction:
Improvefuel system operation continuityVSAvoidcollector wear and damage
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The system performs preliminary detection of the pipe disconnection state by monitoring fuel quantity trends before significant damage occurs to the collector. The health indicator computation and threshold comparison enable early warning, allowing maintenance personnel to intervene before severe wear or damage accumulates.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system establishes a feedback loop where fuel quantity measurements are continuously monitored, classified as normal or abnormal, and used to compute a health indicator. This feedback mechanism enables ongoing assessment of the pipe connection status and triggers warnings when disconnection is detected, allowing for timely maintenance intervention.

Inventive Principle:
Principle #23Feedback

2Reliability

If fuel quantity monitoring is implemented to detect pipe disconnection, then maintenance can be alerted timely, but the device complexity increases

Engineering Contradiction:
Improvedisconnection detection accuracyVSAvoidmonitoring system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system uses the existing fuel quantity measurement capability of the aircraft to perform self-diagnosis of the pipe connection status. By leveraging already-available sensors and data, the system avoids adding separate complex detection hardware while still achieving reliable disconnection monitoring through health indicator computation based on fuel quantity trends.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS20250333186A1Method and device for detecting a disconnection state of a pipe forming part of a pumping system of a fuel collector of an aircraft
Publication Date: 2025.10.30 AIRBUS OPERATIONS (SAS)
  • US20250333186A1 patent drawing
  • US20250333186A1 patent drawing
  • US20250333186A1 patent drawing

AI summary

A method includes a receiving step for receiving a value of the quantity of fuel present in the collector, a processing step including a sub-step for classifying the value received in the receiving step as a normal value, or as an abnormal value, a sub-step for computing the value of a health indicator, based on the received value, as well as on a predetermined number of values received beforehand, and a sub-step for comparing the value of the health indicator with a threshold to be able to detect a disconnection state, as well as a warning step for transmitting a warning in the event of the detection of a disconnection state, the method allowing, by taking into account the quantity of fuel present in the collector, reliable detection of a disconnection state and allowing operators, notably maintenance operators, to be warned.