Electronic Flight Bag Testing via Central Maintenance Computer

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Solution Overview

Problem

There is a need for an effective method to test the functionality of electronic flight bags (EFBs) to ensure they can recover from power losses and maintain communication links with aircraft systems, as existing methods do not comprehensively address these critical functions.

Innovation Solution

A method involving a central maintenance computer (CMC) that initiates power loss presence tests and communication bus tests with the EFB, using existing data bus communication links or wireless protocols, to determine if critical applications recover and communication links are adequate, generating failure messages if tests are not passed.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If comprehensive functionality tests are implemented for EFB, then reliability of EFB operation is improved, but device complexity and testing time increase

Engineering Contradiction:
ImproveEFB functionality reliabilityVSAvoidtesting system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent introduces a Central Maintenance Computer (CMC) as an intermediary system that coordinates and manages all EFB testing operations. The CMC establishes communication links with EFBs, initiates power loss presence tests and communication bus tests, and processes test results. This intermediary approach centralizes testing complexity in a dedicated system rather than distributing it across multiple ad-hoc test setups, thereby improving reliability while managing device complexity through specialization.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If comprehensive functionality tests are implemented for EFB, then reliability of EFB operation is improved, but testing time increases

Engineering Contradiction:
ImproveEFB functionality reliabilityVSAvoidtesting time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent implements preliminary testing actions by conducting power loss presence tests and communication bus tests before actual flight operations. The CMC initiates these tests in advance to verify EFB functionality, including testing critical application recovery after simulated power losses and verifying communication links with Line Replacement Units (LRUs). By performing these comprehensive tests preliminarily, the system ensures reliability is verified before use, preventing in-flight failures while the tests are completed during scheduled maintenance windows rather than delaying operations.

Inventive Principle:
Principle #10Preliminary action

3Productivity

If multiple EFBs are tested simultaneously, then productivity of maintenance operations is improved, but communication system complexity increases

Engineering Contradiction:
Improvemaintenance productivityVSAvoidcommunication system complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent designs the Central Maintenance Computer (CMC) with universal communication capabilities that can simultaneously establish and manage communication links with multiple EFBs. The CMC uses standardized communication protocols and data bus interfaces that allow it to interact with any EFB in the fleet using the same methodology. This universal approach enables parallel testing of multiple EFBs without requiring separate specialized test systems for each device, thereby improving maintenance productivity while managing communication complexity through standardization and multi-functionality.

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

Data Source

PatentEP3434603B8Method for testing the functionality of an electronic flight bag
Publication Date: 2019.12.11 HONEYWELL INTERNATIONAL INC

AI summary

A method for testing the functionality of an electronic flight bag (EFB) has been developed. First a communication link is established between the EFB and a central maintenance computer (CMC). Next, a power loss presence test is initiated for the EFB. This test determines if critical applications of the EFB are recovered during a restart after a power loss. If the EFB fails the test, a failure message is transmitted to the CMC. Next, a communication bus test is initiated for the EFB. The communication bus test determines if adequate communication links exist between the EFB and a data source for critical applications. If the EFB fails the test, a failure message is transmitted to the CMC.