Aircraft Display Monitoring Circuit for Critical Data Integrity

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Solution Overview

Problem

Existing display systems for critical aircraft information are prone to alteration during processing, which can compromise safety and require rigorous certification, increasing costs.

Innovation Solution

A system comprising an electronic processing circuit and a monitoring circuit within a single housing to process and verify critical information, ensuring its integrity before display.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If critical information is processed by electronic circuits for display, then the information can be displayed on screen, but the information may be altered during processing, compromising safety

Engineering Contradiction:
Improvedisplay capabilityVSAvoidinformation integrity
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

A monitoring circuit is introduced as an intermediary component that receives the original critical information directly from the data source and independently verifies it against the processed information in the image signal. This mediator detects any alterations without interfering with the normal display processing function.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The monitoring circuit creates a feedback mechanism by continuously comparing the original critical information with the processed information and generating a verification signal. This feedback loop ensures that any deviations or alterations are detected and can trigger alerts or corrective actions.

Inventive Principle:
Principle #23Feedback

2Reliability

If rigorous certification procedures are implemented for critical display systems, then reliability is improved, but manufacturing costs increase

Engineering Contradiction:
Improvedisplay system certificationVSAvoidmanufacturing cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The display system performs self-verification through the integrated monitoring circuit that automatically checks the integrity of critical information during processing. This self-service capability reduces the need for external certification procedures and manual verification, thereby lowering manufacturing and certification costs while maintaining high reliability.

Inventive Principle:
Principle #25Self-service

3Ease of operation

If critical and non-critical information are displayed together on the same screen, then crew comfort is improved, but the complexity of the display system increases

Engineering Contradiction:
Improvecrew comfortVSAvoiddisplay system complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The display system segments information processing into two independent pathways: one for critical information that includes verification by the monitoring circuit, and another for non-critical information that does not require such verification. This segmentation allows the system to maintain high reliability for critical data while reducing overall complexity by not applying the same verification procedures to all information types.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP4330635B1System for displaying critical and non-critical information
Publication Date: 2026.03.11 SAFRAN ELECTRONICS & DEFENSE (FR)
  • EP4330635B1 patent drawingFigure 1~2
  • EP4330635B1 patent drawingFigure 3~4

AI summary

System for displaying critical and non-critical information on a screen (9), comprising, in the same housing (101), at least one electronic computing circuit (110) and an electronic monitoring circuit (120). The electronic computing circuit (110) is programmed to process the critical information to be displayed, construct at least one image from non-critical information and incorporate therein the critical information to be displayed in order to form, on an output (104.1) of the electronic computing circuit (110), an image signal intended to be transmitted to the screen. The electronic monitoring circuit (120) has an input (105.1) connected to said output (104.1) and is programmed to determine expected critical information for the display and to verify whether the image signal contains information corresponding to the expected critical information. Aircraft equipped with such a system.