Aircraft Wire Routing Using EM Disturbance Bundle Modeling

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Solution Overview

Problem

Aircraft wire routing is challenging due to electromagnetic disturbances, and existing methods struggle with data accuracy, efficiency, and scalability in reevaluating wire routes during design changes.

Innovation Solution

A computing system uses an authoritative aircraft design database to model wire bundles, determining electromagnetic effects, and compares them to acceptance criteria to ensure compliance with design specifications, allowing for efficient and reliable wire routing decisions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If manual wire routing evaluation methods are used, then design flexibility is maintained, but data accuracy and reliability deteriorate due to human error and inconsistency

Engineering Contradiction:
Improvewire routing evaluation reliabilityVSAvoidrouting evaluation system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces manual mechanical evaluation methods with an automated computing system that retrieves wire routing data from an authoritative aircraft design database and performs electromagnetic disturbance analysis computationally. This substitution eliminates human error and inconsistency while maintaining design flexibility through programmable evaluation criteria.

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

Solution Approach 2:

The patent creates a virtual model of wire bundles by retrieving data from the aircraft design database, allowing the system to evaluate routing options without physically manipulating actual wires. This digital copying enables repeated evaluation of multiple routing scenarios without affecting the physical aircraft design.

Inventive Principle:
Principle #26Copying

2Measurement precision

If comprehensive electromagnetic disturbance analysis is performed on each wire bundle, then measurement precision improves, but computing resource consumption increases

Engineering Contradiction:
Improveelectromagnetic effect estimation precisionVSAvoidcomputing resource consumption
Core Design Contradiction:
Measurement precisionVSUse of energy by moving object

Solution Approach 1:

The patent applies partial action by focusing electromagnetic disturbance analysis only on specific wire bundles that are candidates for routing, rather than analyzing all wires in the aircraft. The system selectively evaluates bundles based on their exposure to electromagnetic disturbances, performing comprehensive analysis only where necessary to meet design specifications.

Inventive Principle:
Principle #16Partial or excessive action

Solution Approach 2:

The patent performs preliminary retrieval of wire bundle data from the authoritative aircraft design database before conducting electromagnetic disturbance analysis. This preliminary data gathering organizes information about wire positions, shielding, and routing paths, enabling more efficient computation during the actual electromagnetic effect estimation without redundant data processing.

Inventive Principle:
Principle #10Preliminary action

3Adaptability or versatility

If wire routing is reevaluated during design changes, then design adaptability improves, but time consumption increases due to reevaluation requirements

Engineering Contradiction:
Improvewire routing adaptability to design changesVSAvoidreevaluation time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The patent implements feedback by automatically detecting design changes in the aircraft design database and triggering reevaluation of affected wire bundles. The system monitors for changes in wire routing, shielding configurations, or electromagnetic disturbance sources, and only reevaluates bundles whose electromagnetic exposure may have changed, rather than performing full reanalysis of all wires.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent creates a dynamic wire routing evaluation system that adapts to design changes automatically. The system can be reexecuted at any stage during aircraft design, manufacturing, or post-production to account for changes in wire routing decisions, allowing the evaluation process to remain synchronized with the evolving aircraft design without manual intervention.

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach improves the reliability and efficiency of wire routing by reducing errors, saving computing resources, and enabling automatic updates based on design changes, ensuring compliance with electromagnetic disturbance standards.

Implementation Method 1

generating a transmission line model to determine an estimated effect of an electromagnetic disturbance on the wire bundle

Methodology Applied
Scientific EffectElectromagnetic disturbance: Electromagnetic Induction

Data Source

PatentUS12585843B2Aircraft wire routing to account for electromagnetic disturbances
Publication Date: 2026.03.24 THE BOEING CO
  • US12585843B2 patent drawing
  • US12585843B2 patent drawing
  • US12585843B2 patent drawing

AI summary

A computing device includes a memory storing instructions. The computing device also includes one or more processors coupled to the memory and configured to execute the instructions to perform operations including obtaining data specifying a wire to be routed; selecting a wire bundle as a candidate for routing the wire; determining bundle parameters; generating a transmission line model to determine an estimated effect of an electromagnetic disturbance on the wire bundle; performing a comparison of the estimated effect of the electromagnetic disturbance to an acceptance criterion; and generating output indicating whether, based on the comparison, a particular routing of the wire satisfies a design specification.