Wireless Aircraft Engine Emissions Monitoring for Predictive Maintenance

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Solution Overview

Problem

Current aircraft engine monitoring systems fail to effectively real-time monitor environmental emissions and determine maintenance schedules, leading to increased pollutant emissions and maintenance costs, while also requiring redundant wiring that increases weight and reduces efficiency.

Innovation Solution

A wireless engine monitoring system with sensors that transmit engine data to a processor for real-time analysis, generating alarm reports when emissions exceed thresholds and using Bayesian networks to determine maintenance schedules based on flight phases and engine performance parameters.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If wireless engine monitoring system is implemented, then emission monitoring capability is improved, but device complexity increases

Engineering Contradiction:
Improveemission monitoring capabilityVSAvoiddevice complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The wireless engine monitoring system integrates multiple functions including emission parameter monitoring, maintenance schedule determination, and alarm generation within a single unified system. The processor executes multiple algorithms (Bayesian networks for maintenance scheduling, threshold comparisons for alarm generation) and handles various emission parameters (NOx, CO, HC, PM) through a common hardware platform, thereby improving measurement capability while managing device complexity through functional integration.

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

2Weight of moving object

If redundant wiring is removed, then aircraft weight is reduced, but system reliability deteriorates

Engineering Contradiction:
Improveaircraft weightVSAvoidsystem reliability
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The patent replaces the traditional mechanical/wired sensor network with a wireless monitoring system. Sensors transmit emission data wirelessly to the processor, eliminating the need for redundant physical wiring harnesses and connectors. This substitution reduces aircraft weight while maintaining system reliability through the robustness of wireless communication protocols and the integrated nature of the monitoring system.

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

3Object-affected harmful factors

If real-time emission monitoring is implemented, then emission compliance is improved, but energy consumption increases

Engineering Contradiction:
Improveemission complianceVSAvoidenergy consumption
Core Design Contradiction:
Object-affected harmful factorsVSUse of energy by moving object

Solution Approach 1:

The system continuously monitors emission parameters and provides real-time feedback through alarm generation when thresholds are exceeded. The processor compares measured emission values against predetermined thresholds and immediately generates alarms for compliance violations. This feedback mechanism ensures emission compliance while optimizing energy consumption by only activating intensive processing and alarm generation when necessary, rather than continuously operating at full power.

Inventive Principle:
Principle #23Feedback

4Productivity

If maintenance scheduling is optimized, then maintenance cost is reduced, but measurement precision requirements increase

Engineering Contradiction:
Improvemaintenance efficiencyVSAvoiddata accuracy requirements
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

The system determines maintenance schedules in advance by analyzing emission data trends and comparing them against baseline values using Bayesian networks. By performing preliminary analysis of emission patterns and predicting future maintenance needs, the system enables proactive maintenance planning that reduces costs while minimizing the need for high-precision real-time measurements during operation, as the focus shifts to trend analysis rather than continuous high-precision monitoring.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP3910604B1Monitoring system for an aircraft engine configured to determine a maintenance schedule for the aircraft engine
Publication Date: 2024.05.01 HARRIS CORP
  • EP3910604B1 patent drawingFigure 1
  • EP3910604B1 patent drawingFigure 2
  • EP3910604B1 patent drawingFigure 3

AI summary

A wireless engine monitoring system for an aircraft engine includes a housing and wireless transceiver that receives engine data, including engine data relating to environmental engine emissions. The collected engine data is provided to a ground based receiver and processor that is configured to correlate the engine data to a phase of flight and determine a maintenance schedule on the basis of an analysis.