Aircraft ECS Heat Exchanger Fouling Prediction

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Solution Overview

Problem

Accurately predicting the maintenance needs of aircraft heat exchangers in environmental control systems is challenging, leading to potential premature or delayed replacements that result in unnecessary downtime and operational inefficiencies.

Innovation Solution

A maintenance system that includes a data acquisition module to determine ambient temperature and altitude, a fouling module to generate a fouling condition based on these parameters, and a reporting module to provide users with predictive alerts and health indicators for the heat exchangers, allowing for timely maintenance decisions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If heat exchanger replacement is performed based on fixed schedules, then maintenance reliability is improved, but device complexity and operational downtime increase due to premature or delayed replacements

Engineering Contradiction:
Improvemaintenance reliabilityVSAvoidmaintenance operation complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system transitions from fixed-schedule maintenance to condition-based maintenance by continuously monitoring operational parameters (ambient temperature, altitude, compressor temperature) and using these parameter changes to dynamically determine heat exchanger fouling status and replacement timing

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces manual inspection and fixed-schedule maintenance mechanisms with an automated electronic monitoring and prediction system that uses sensors, data processing, and algorithms to detect fouling conditions and predict maintenance needs

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

2Reliability

If heat exchanger replacement is performed early, then system reliability is improved, but loss of time and productivity decrease due to unnecessary downtime

Engineering Contradiction:
ImproveECS reliabilityVSAvoidaircraft downtime
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system performs preliminary detection and prediction of fouling conditions before actual degradation occurs, allowing maintenance to be scheduled at the optimal time rather than replacing components prematurely, thus reducing unnecessary downtime while maintaining reliability

Inventive Principle:
Principle #10Preliminary action

3Productivity

If heat exchanger replacement is delayed, then productivity is improved by reducing downtime, but reliability deteriorates due to operational inefficiencies and passenger discomfort

Engineering Contradiction:
Improvemaintenance efficiencyVSAvoidoperational efficiency
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system continuously monitors operational parameters and provides feedback on heat exchanger condition, enabling dynamic adjustment of maintenance timing to optimize both productivity (by avoiding unnecessary replacements) and reliability (by preventing operational inefficiencies from excessive degradation)

Inventive Principle:
Principle #23Feedback

4Measurement precision

If comprehensive monitoring parameters are collected, then measurement precision is improved, but device complexity increases

Engineering Contradiction:
Improvefouling detection precisionVSAvoidmonitoring system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system uses existing multi-functional sensors and data processing capabilities from the ECS to simultaneously monitor multiple parameters (temperature, altitude, pressure) for fouling detection, avoiding the need for dedicated specialized sensors and reducing overall system complexity

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

Data Source

PatentEP3346345B1Diagnosis system for fouling prediction of aircraft aircondition systems
Publication Date: 2019.04.10 HONEYWELL INTERNATIONAL INC
  • EP3346345B1 patent drawingFigure 1
  • EP3346345B1 patent drawingFigure 2
  • EP3346345B1 patent drawingFigure 3

AI summary

A maintenance system is provided for an environmental conditioning element of an environmental control system of an aircraft. The maintenance system includes a data acquisition module (310) configured to determine an ambient temperature, an altitude of the aircraft, and a measured ECS compressor temperature; a fouling module (320) coupled to receive the ambient temperature, the altitude, and the measured ECS compressor temperature from the data acquisition module and configured to generate a fouling condition of the environmental conditioning element based on at least the ambient temperature, the altitude, and the measured ECS compressor temperature; and a reporting module (340) coupled to receive the fouling condition from the fouling module and configured to generate a report for a user that includes the fouling condition.