Automated Aircraft Software Update and Documentation Sync

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Solution Overview

Problem

Aircraft manufacturers face challenges in managing and updating the documentation of aircraft configurations due to customized configurations by airline companies, numerous clients, varying technical solutions for equipment items, and the selection of component versions following modifications and service bulletins, leading to potential non-conformity with actual aircraft configurations.

Innovation Solution

A computer method for automated software updating and documentation management, where operators receive indications of software modifications from manufacturers, perform automatic updates, and report execution to ensure coherent documentation, reducing downtime and maintaining accurate records.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If manual software updating and documentation management is performed, then customization and control are possible, but time consumption and operational complexity increase

Engineering Contradiction:
Improvesoftware updating processVSAvoiddowntime
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The system enables automated self-updating of software applications through uploaded update packages, eliminating the need for manual intervention in the updating process itself. The documentation system similarly updates automatically based on detected software configurations, reducing operational burden and time requirements.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Software update packages are prepared and validated in advance before being uploaded to the aircraft system. The documentation is pre-configured with templates and structures that enable automatic population based on software configurations, allowing rapid deployment without time-consuming manual processes.

Inventive Principle:
Principle #10Preliminary action

2Loss of time

If automated software updating is implemented, then downtime is reduced, but ensuring documentation accuracy becomes more challenging

Engineering Contradiction:
ImprovedowntimeVSAvoiddocumentation accuracy
Core Design Contradiction:
Loss of timeVSReliability

Solution Approach 1:

The system implements a feedback mechanism where the documentation generation process continuously references the actual software configuration data from the aircraft system. This closed-loop approach ensures that documentation accurately reflects the current software state by automatically detecting and reporting any configuration discrepancies.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

A configuration data structure serves as an intermediary between the software applications and the documentation system. This intermediate layer automatically captures software configuration information and translates it into documentation format, ensuring accuracy without requiring direct manual intervention or complex integration.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If comprehensive documentation is maintained for all aircraft configurations, then regulatory compliance is improved, but data management complexity increases

Engineering Contradiction:
Improveregulatory complianceVSAvoiddata management system
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The documentation system is segmented into modular templates that correspond to different aircraft configurations and software applications. Each template can be independently configured and updated, allowing comprehensive documentation to be managed through discrete, manageable units rather than as a monolithic system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The documentation system uses universal templates and data structures that can accommodate multiple aircraft configurations and software types through parameterization. A single documentation framework serves multiple purposes by adapting to different configuration scenarios, reducing overall system complexity while maintaining comprehensive coverage.

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

Data Source

PatentUS9075681B2Methods and devices for automated loading of software, in an apparatus such as an aircraft, including the updating of the associated documentation
Publication Date: 2015.07.07 AIRBUS OPERATIONS (SAS)
  • US9075681B2 patent drawing
  • US9075681B2 patent drawing
  • US9075681B2 patent drawing

AI summary

The invention in particular has as an object methods and devices for automated loading of software, in a piece of equipment such as an aircraft, comprising the updating of the associated documentation. After having received an indication relating to a modification of a software application, a command making it possible to perform the required updating automatically is transmitted to a piece of equipment comprising this software application. In response, an indication relating to the execution of the command is received and a report of execution of the command is transmitted to the manufacturer in order to allow it to update the documentation of the piece of equipment accordingly.