Rogue Component Detection in Aircraft Systems

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Solution Overview

Problem

Monitoring and maintaining the health of numerous components in complex systems, such as aircraft, is time-consuming and often relies on anecdotal methods, making it difficult to identify rogue components that may fail and affect system performance.

Innovation Solution

A system comprising a scanning device and a server that identifies unique components, determines operating parameters, compares them to predefined baselines, and determines whether a component is rogue, generating alerts and recommending actions to predict potential failures and maintain component availability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If manual monitoring of each component is performed, then component health can be tracked, but the process becomes time-consuming and tedious

Engineering Contradiction:
Improvecomponent health trackingVSAvoidmonitoring time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system enables components to self-report their health status through embedded sensors and identifiers. Each component automatically transmits operational data and status information to the monitoring system, eliminating the need for manual inspection while maintaining comprehensive health tracking.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Manual monitoring processes are replaced with an automated electronic system that uses scanners, databases, and algorithms to identify components, retrieve their health data, and analyze their status. This substitution transforms a labor-intensive mechanical process into an efficient automated information processing system.

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

2Reliability

If conservative maintenance scheduling is used, then component failures are reduced, but maintenance frequency increases leading to loss of time

Engineering Contradiction:
Improvecomponent failure preventionVSAvoidmaintenance time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system performs preliminary identification and assessment of component conditions before failures occur. By continuously monitoring operational parameters and comparing them against baseline data, the system detects early signs of degradation and schedules maintenance only when actually needed, rather than following fixed conservative intervals.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system transitions from fixed-time maintenance scheduling to condition-based scheduling by monitoring actual operational parameters such as usage hours, cycles, and health metrics. Maintenance decisions are made based on real-time parameter analysis rather than predetermined time intervals, optimizing the balance between reliability and time loss.

Inventive Principle:
Principle #35Parameter changes

3Measurement precision

If component identification and analysis is automated, then rogue component detection is improved, but system complexity increases

Engineering Contradiction:
Improverogue component detection accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The automated system is divided into distinct functional modules: component identification module (scanners reading identifiers), data retrieval module (accessing component histories), analysis module (comparing current status to baseline), and decision module (determining rogue status). This segmentation allows each module to perform its specific function independently, improving detection precision while managing complexity through modular design.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS9327846B2Fleet performance optimization tool enhancement
Publication Date: 2016.05.03 THE BOEING CO
  • US9327846B2 patent drawing
  • US9327846B2 patent drawing
  • US9327846B2 patent drawing

AI summary

Methods and systems are provided for enhancing performance of a system that includes a plurality of components. A server is coupled to a scanning device that is configured to scan a first component of the plurality of components for an identifier that uniquely identifies the first component. The server receives, from the scanning device, an identification of the first component of the plurality of components. The server also determines an operating parameter that is uniquely related to the first component, compares the operating parameter to a predefined baseline for the first component, and determines whether the first component is a rogue component.