Aircraft Component Identification Verification for Correct Installation

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Solution Overview

Problem

Modern aircraft have multiple apparatuses with communication-enabled components of identical design, making it challenging to uniquely identify and address each component for error-free communication with the server, especially when multiple components of the same type are installed.

Innovation Solution

A method involving the transmission of a configuration signal from a terminal to a host system, which includes principal datasets with unique apparatus identifications and associated auxiliary datasets for each component, allowing the host system to store and compare reference piece-part identifications with actual piece-part identifications to verify correct component installation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple communication-enabled components of identical design are installed in an aircraft, then the apparatus can perform required functions with standardized parts, but it becomes difficult to uniquely identify and address each component for error-free communication

Engineering Contradiction:
ImproveAbility to install standardized componentsVSAvoidComponent identification accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The identification system is segmented into multiple hierarchical levels: apparatus identification for the overall device, component identification for individual parts, and serial number identification for unique component instances. This segmentation allows standardized components to be distinguished through their serial numbers while maintaining compatibility through common identification structures.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The host system pre-stores reference datasets containing correct component identifications and serial numbers before the aircraft production or maintenance process begins. This preliminary preparation enables rapid verification and identification during assembly or repair without requiring complex real-time analysis.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If a configuration verification system is implemented to verify correct component installation, then communication errors can be prevented, but the complexity of the system increases due to additional identification and verification steps

Engineering Contradiction:
ImproveCommunication error preventionVSAvoidSystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system automatically compares detected component identifications and serial numbers against pre-stored reference datasets, generating feedback signals that indicate whether components are correctly installed. This automated feedback mechanism provides reliable verification without requiring complex manual inspection procedures.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The host system performs multiple functions using a unified identification framework: it stores reference data, detects component identifiers, compares actual versus reference data, and generates verification signals. This multi-functionality reduces overall system complexity by consolidating verification tasks into a single integrated system.

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

3Measurement precision

If detailed identification data is collected and stored for each component, then unique identification and verification become possible, but the amount of data to be processed and stored increases

Engineering Contradiction:
ImproveComponent identification accuracyVSAvoidData volume
Core Design Contradiction:
Measurement precisionVSQuantity of substance

Solution Approach 1:

Identification data is segmented into distinct hierarchical levels: apparatus identification (common to all components of an apparatus), component identification (specific to component type), and serial number identification (unique to each component instance). This segmentation allows the system to store and process only the necessary level of detail for each verification task, reducing overall data volume.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Reference datasets containing component identifications and serial numbers are pre-stored in the host system before verification processes begin. This preliminary data preparation eliminates the need to collect and process extensive identification data during actual verification operations, significantly reducing real-time data processing requirements.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS12179924B2Method for processing identifications
Publication Date: 2024.12.31 AIRBUS OPERATIONS GMBH
  • US12179924B2 patent drawing
  • US12179924B2 patent drawing
  • US12179924B2 patent drawing

AI summary

A method for processing previously detected identifications of apparatuses of an aircraft, wherein each apparatus has at least one communicative component. A reference dataset is used to compare the actual identifications with specified identifications, as a result of which a report signal based on the comparison result indicates whether the detected identifications correspond to the identifications represented by the reference dataset. If there is a positive match, this allows the conclusion that the apparatuses are correctly installed in the aircraft.