Integrated Flight Dispatch Decision Support System

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Solution Overview

Problem

Current aircraft fault management relies on manual processes for decision-making and documentation, which is inefficient and lacks integration of real-time data, leading to suboptimal fault mitigation and dispatch capabilities.

Innovation Solution

An integrated system that procures onboard aircraft data, MEL constraints, and offboard flight plan information to provide holistic flight dispatch determinations, automating the transfer of discrepancy data and using avionic systems for real-time fault mitigation guidance without paper documents.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If manual processes are used for fault management and documentation, then system complexity is reduced, but productivity and efficiency deteriorate due to time-consuming manual data collection and documentation

Engineering Contradiction:
Improvefault management efficiencyVSAvoidsystem integration complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent merges multiple separate systems (MEL constraints database, aircraft performance database, weather database, flight plan system, and maintenance management system) into an integrated decision support system. This consolidation allows automatic data exchange and eliminates manual processes, directly improving fault management efficiency while the integration complexity is managed through standardized interfaces and protocols.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The integrated system performs multiple functions simultaneously: it evaluates MEL constraints, calculates aircraft performance, checks weather conditions, modifies flight plans, and documents maintenance discrepancies. This multi-functionality consolidates what were previously separate manual processes into a single automated system, improving productivity despite the increased system complexity.

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

2Reliability

If real-time data integration from multiple sources is implemented, then decision accuracy and reliability improve, but device complexity and information processing requirements increase

Engineering Contradiction:
Improvefault mitigation accuracyVSAvoiddata integration complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent introduces an intermediary processing layer that standardizes data from multiple sources (MEL constraints, aircraft performance data, weather information, flight plan details). This intermediary layer translates various data formats into a unified structure, enabling accurate real-time decision-making while managing the complexity of data integration through standardized interfaces and protocols.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Loss of time

If automatic discrepancy recording and data transfer are implemented, then loss of time in documentation is reduced, but device complexity and automation requirements increase

Engineering Contradiction:
Improvedocumentation timeVSAvoidautomatic data transfer complexity
Core Design Contradiction:
Loss of timeVSExtent of automation

Solution Approach 1:

The system implements self-service automation where the integrated decision support system automatically records flight discrepancies, collects relevant data from onboard systems, and transfers maintenance information to the maintenance management system without requiring manual pilot input. This eliminates time-consuming manual documentation while the automation complexity is managed through predefined protocols and automated interfaces.

Inventive Principle:
Principle #25Self-service

4Ease of operation

If comprehensive external data (weather, performance, flight plan) is integrated with MEL constraints, then ease of operation for pilots improves, but device complexity and data processing requirements increase

Engineering Contradiction:
Improvepilot decision-making easeVSAvoidinformation system complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent segments the complex integrated system into distinct functional modules: MEL constraint evaluation module, aircraft performance calculation module, weather assessment module, flight plan modification module, and documentation module. Each module handles specific data processing tasks independently, then integrates results to provide comprehensive guidance. This segmentation improves ease of operation by organizing information logically while managing overall system complexity through modular architecture.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS8514104B1Integrated minimum equipment decision support system
Publication Date: 2013.08.20 ROCKWELL COLLINS INC
  • US8514104B1 patent drawing
  • US8514104B1 patent drawing
  • US8514104B1 patent drawing

AI summary

An integrated system for providing minimum equipment decision support for an aircraft including means for procuring onboard aircraft data and providing a cockpit message. Minimum equipment list (MEL) constraints and offboard flight plan related information are procured. The onboard aircraft flight data, minimum equipment list constraints, and offboard flight plan related information are synthesized to enable holistic flight dispatch determinations within the current fault condition of the aircraft.