Aircraft Engine Usage Analysis for Corrosion and Erosion Mitigation

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Solution Overview

Problem

Aircraft engines face challenges in mitigating corrosion and erosion due to exposure to various environmental conditions such as rain, snow, sand, and salt, which can lead to premature wear and increased maintenance costs if not addressed effectively.

Innovation Solution

A method and system utilizing machine learning to analyze usage data from accumulated media inside the engine, determining the engine condition, and initiating targeted corrosion-mitigating or erosion-mitigating actions, such as inspections or component replacements, based on risk assessments.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional fixed-schedule maintenance is used, then maintenance coverage is comprehensive, but maintenance costs increase and engine availability decreases

Engineering Contradiction:
Improveengine reliabilityVSAvoidengine availability
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The maintenance schedule transitions from a static fixed-interval approach to a dynamic condition-based approach. The system continuously monitors engine conditions through sensors and adjusts maintenance timing based on actual engine state, allowing maintenance to occur only when necessary rather than following a predetermined schedule.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The engine effectively monitors its own condition through integrated sensors and communication systems that detect corrosion and erosion risks. This self-diagnosis capability enables the engine to signal when maintenance is needed, replacing the need for external fixed-schedule inspections.

Inventive Principle:
Principle #25Self-service

2Object-affected harmful factors

If frequent maintenance actions are performed, then corrosion and erosion risks are reduced, but maintenance costs and operational disruptions increase

Engineering Contradiction:
Improvecorrosion and erosion riskVSAvoidmaintenance costs
Core Design Contradiction:
Object-affected harmful factorsVSLoss of energy

Solution Approach 1:

The system performs preliminary detection of corrosion and erosion risks using sensors that monitor engine conditions in real-time. By identifying potential issues before they manifest as actual damage, the system enables preventive maintenance only when necessary, avoiding unnecessary maintenance actions and associated costs.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The monitoring system provides continuous feedback on engine condition parameters such as salt accumulation, dust ingestion, and component degradation. This feedback loop enables dynamic adjustment of maintenance frequency based on actual risk levels, optimizing the balance between protection and cost.

Inventive Principle:
Principle #23Feedback

3Measurement precision

If comprehensive monitoring of engine conditions is implemented, then maintenance precision is improved, but system complexity increases

Engineering Contradiction:
Improvecondition assessment accuracyVSAvoidmonitoring system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The monitoring system is divided into modular functional components: sensors for detecting specific parameters (salt, dust, moisture), processing units for analyzing sensor data, and communication systems for transmitting condition information. This segmentation allows the complex monitoring function to be implemented through manageable, independent modules.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP4379193A1Method and system for mitigating corrosion and erosion in an aircraft engine
Publication Date: 2024.06.05 PRATT & WHITNEY CANADA CORP
  • EP4379193A1 patent drawingFigure 1
  • EP4379193A1 patent drawingFigure 2
  • EP4379193A1 patent drawingFigure 3

AI summary

A method for mitigating corrosion and/or erosion in an aircraft engine includes receiving usage data (202) which characterize a medium accumulated inside the aircraft engine. Using a trained model (204), the usage data (202) is related to an assigned aircraft engine condition (206) from a plurality of aircraft engine conditions (206). The trained model (204) is trained using machine learning and historical data (216) relating characteristics of the medium to the plurality of aircraft engine conditions (206). When the assigned aircraft engine condition (206) is indicative of a corrosion risk (208) for the aircraft engine, a corrosion-mitigating action (212) is initiated for the aircraft engine, such as engine wash. When the assigned aircraft engine condition (206) is indicative of an erosion risk (210) for the aircraft engine, an erosion-mitigating action (214) is initiated for the aircraft engine, such as inspection or component replacement.