Flight Calculation Discrepancy Detection System

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Solution Overview

Problem

The process of comparing flight calculations among multiple pilots is time-consuming and tedious, often leading to discrepancies due to human errors, which can compromise flight safety.

Innovation Solution

A system with multiple user interfaces and a control unit that allows simultaneous comparison of calculations entered by different pilots, identifying discrepancies and restricting aircraft operation until calculations agree, optionally with AI or machine learning for enhanced accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If each pilot manually compares calculations with all other pilots, then calculation accuracy can be verified, but the process becomes time-consuming and tedious

Engineering Contradiction:
Improvecalculation accuracyVSAvoidcomparison time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

A control unit is introduced as an intermediary system that automatically receives, stores, and compares calculation data from multiple pilots. This intermediary performs the comparison function that would otherwise require manual effort from each pilot, thereby maintaining calculation accuracy verification while dramatically reducing the time required.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The manual mechanical process of pilots physically comparing calculations is replaced by an automated electronic system. The control unit electronically receives, stores, and compares calculation data, substituting the manual comparison process with an automated computational system that achieves the same reliability goal much faster.

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

2Ease of operation

If manual calculation comparison is used, then pilots can independently verify calculations, but human errors such as writing incorrect numbers or erroneous calculations occur

Engineering Contradiction:
Improveindependent verificationVSAvoidcalculation accuracy
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system maintains independent verification capability while improving reliability by having each pilot input their own calculations independently into the control unit. The system then automatically compares all inputs, eliminating human error in the comparison process itself while preserving the independence of each pilot's calculation work.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The control unit provides automated feedback by comparing each pilot's calculations against others and identifying discrepancies. This feedback mechanism systematically highlights errors such as incorrect numbers or erroneous calculations, allowing pilots to review and correct their work while maintaining the benefit of independent verification.

Inventive Principle:
Principle #23Feedback

3Productivity

If a centralized system automatically compares calculations, then comparison time is reduced and accuracy is improved, but system complexity increases

Engineering Contradiction:
Improvecomparison efficiencyVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The control unit is designed as a multi-functional device that not only compares calculations but also receives data from multiple pilots, stores calculation data, displays results, and can restrict aircraft operation based on comparison outcomes. By consolidating these functions into a single universal system, the patent reduces overall system complexity while maintaining high productivity.

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

Data Source

PatentUS20250319988A1Systems and methods for confirming flight calculations for an aircraft
Publication Date: 2025.10.16 THE BOEING CO
  • US20250319988A1 patent drawing
  • US20250319988A1 patent drawing
  • US20250319988A1 patent drawing

AI summary

A system and a method include multiple user interfaces. Different sets of calculations for a flight of an aircraft are configured to be input through the user interfaces. A control unit is in communication with the different user interfaces. The control unit is configured to receive the different sets of calculations for the flight of the aircraft, and compare the different sets of calculations for the flight of the aircraft to determine presence of one or more discrepancies therebetween.