Aircraft Diagnostics Adaptive Maintenance

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Solution Overview

Problem

Current aircraft maintenance diagnostics rely on sub-optimal, hard-coded troubleshooting procedures, leading to inefficient fault rectification, increased downtime, and potential damage to reliable components due to incomplete knowledge of complex system failures.

Innovation Solution

A system and method for automatically analyzing aircraft systems data to identify non-predetermined troubleshooting procedures, utilizing a data acquisition, archiving, and analysis module to correlate and update maintenance procedures based on actual maintenance actions and global data analysis.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If hard-coded predetermined troubleshooting procedures are used, then maintenance procedures are standardized and easy to follow, but fault rectification efficiency is reduced and unnecessary component replacements occur

Engineering Contradiction:
Improveease of following maintenance proceduresVSAvoidfault rectification efficiency
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

The system implements feedback by collecting actual maintenance outcome data from multiple sources and using it to dynamically update and improve troubleshooting procedures. The feedback loop allows the system to learn from successful repairs and refine its recommendations, transforming static hard-coded procedures into adaptive, data-driven guidance that improves both ease of operation and fault rectification efficiency

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The troubleshooting procedures transition from static, predetermined sequences to dynamic, adaptive processes that adjust based on real-time data analysis. The system dynamically modifies procedure recommendations based on patterns learned from historical maintenance data, allowing procedures to evolve and optimize themselves while remaining easy to follow through automated guidance

Inventive Principle:
Principle #15Dynamics

2Productivity

If engineers use unofficial troubleshooting procedures based on experience, then fault rectification speed improves, but reliability and peer review are compromised

Engineering Contradiction:
Improvefault rectification speedVSAvoidprocedural reliability through peer review
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system merges the advantages of both formal and informal approaches by combining the structured framework of official procedures with the practical insights from experienced engineers. Multiple data sources including unofficial experience-based procedures are integrated and analyzed together, allowing reliable, peer-reviewed synthesis of maintenance knowledge that maintains both speed and reliability

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

Unofficial experience-based procedures are subjected to feedback mechanisms where outcomes are tracked and analyzed. Successful unofficial procedures are validated through repeated success patterns and integrated into the formal system, while unsuccessful ones are discarded. This feedback loop provides implicit peer review through data-driven validation

Inventive Principle:
Principle #23Feedback

3Stability of the object's composition

If predetermined troubleshooting procedures are followed, then maintenance consistency is maintained, but rare faults and emergent properties are missed

Engineering Contradiction:
Improvemaintenance procedure consistencyVSAvoidability to handle rare and complex faults
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The system maintains consistency through its core analytical framework while adapting to rare and emergent faults through continuous learning from fleet-wide data. The dynamic nature of the system allows it to recognize patterns in rare failures that individual engineers would miss, providing consistent yet adaptable troubleshooting guidance that evolves with new failure modes

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system serves multiple functions simultaneously: it provides consistent step-by-step guidance for common faults while also analyzing complex patterns across the entire fleet to identify rare and emergent failure modes. The multi-functional approach allows the same system to maintain procedural consistency for routine maintenance while adapting to handle diverse and rare fault conditions

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

4Difficulty of detecting and measuring

If components are removed and replaced frequently during troubleshooting, then potential faults are systematically checked, but component reliability is reduced through handling

Engineering Contradiction:
Improvesystematic fault detectionVSAvoidcomponent reliability through reduced handling
Core Design Contradiction:
Difficulty of detecting and measuringVSReliability

Solution Approach 1:

The system replaces physical component manipulation with data-driven diagnostics. Instead of mechanically removing and replacing components to check for faults, the system uses sensor data, system diagnostics, and pattern recognition to identify the actual fault location, thereby eliminating unnecessary component handling while maintaining systematic fault detection

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

Solution Approach 2:

The system introduces an intermediary layer of intelligent analysis between the symptom and the component. Rather than directly testing components through removal and replacement, the system uses diagnostic data analysis as an intermediary to identify the true fault source, reducing unnecessary handling of components that appear suspicious but are actually functional

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS9321542B2Diagnostics for aircraft
Publication Date: 2016.04.26 GE AVIATION SYST LTD
  • US9321542B2 patent drawing
  • US9321542B2 patent drawing
  • US9321542B2 patent drawing

AI summary

A system for automatically analysing aircraft systems data is described. The system comprises a data acquisition module operable to acquire aircraft systems data, a data archiving module operable to store aircraft systems data and a data analysis module operable to analyse the aircraft systems data to identify non-predetermined troubleshooting procedures for fault rectification. Automated identification of improved maintenance techniques can thus be provided, with the added benefit that maintenance manuals and procedures may thereby be automatically adapted over time. A related method is also described.