Aircraft Master Indicator for Checklist Display

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Solution Overview

Problem

Current aircraft instrumentation relies on paper-based checklists that require significant time and effort to analyze multiple systems, necessitating a more efficient method to present checklist information to operators.

Innovation Solution

An aircraft instrumentation system with a master indicator that activates in response to trigger events, allowing user input to display relevant information, including checklists and synoptics, to facilitate quicker response times and reduced effort.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If paper-based checklists are used to present aircraft system information, then comprehensive information can be provided, but the response time and effort required by pilots increase significantly

Engineering Contradiction:
Improvechecklist informationVSAvoidresponse time
Core Design Contradiction:
Loss of informationVSLoss of time

Solution Approach 1:

The patent creates an electronic copy of the paper-based checklist system, displaying checklist items and synoptic diagrams on an electronic display unit. This electronic copy provides the same comprehensive information as the paper version while enabling faster access and interaction through electronic interfaces, directly resolving the contradiction between information completeness and response time.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent replaces the mechanical paper-based system with an electronic display and control system. Pilots interact with electronic checklists through display units rather than physically handling paper checklists, enabling faster information retrieval and reducing the time required to respond to system warnings while maintaining comprehensive information delivery.

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

2Loss of information

If paper-based checklists are used, then all necessary information can be displayed, but the complexity of analyzing multiple components increases pilot effort

Engineering Contradiction:
Improvesystem informationVSAvoidpilot effort
Core Design Contradiction:
Loss of informationVSEase of operation

Solution Approach 1:

The patent segments the checklist information into distinct displayable items and synoptic diagrams that can be individually selected and viewed on the electronic display. This segmentation allows pilots to access specific system information without having to analyze entire paper checklists, reducing cognitive effort while maintaining comprehensive information availability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The electronic display unit acts as an intermediary between the aircraft's multiple components and the pilot. It processes and presents information in an organized, selectable format that reduces the pilot's analytical burden compared to reviewing comprehensive paper checklists, while still providing access to all necessary system information.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If multiple warning and caution lights are used to indicate system status, then comprehensive system monitoring is achieved, but the time to identify and respond to issues increases

Engineering Contradiction:
Improvesystem monitoringVSAvoididentification time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent merges the information from multiple warning and caution lights with corresponding synoptic diagrams and checklist items on a single electronic display. This integration allows pilots to see the relationship between multiple system alerts and their corresponding components simultaneously, reducing the time required to identify and respond to issues while maintaining comprehensive system monitoring.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS9114887B2Methods and systems for displaying aircraft information
Publication Date: 2015.08.25 GULFSTREAM AEROSPACE CORP
  • US9114887B2 patent drawing
  • US9114887B2 patent drawing
  • US9114887B2 patent drawing

AI summary

A method and an instrumentation system for an aircraft are provided. The method of presenting aircraft information includes activating a master indicator in response to a trigger event associated with operation of the aircraft, receiving a user input associated with the master indicator, and displaying information associated with the trigger event in response to receiving the user input associated with the master indicator. The instrumentation system performs the operations of the method.