Aircraft Turbulence Display Using Connected Flight-Path Data

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Solution Overview

Problem

Current aircraft turbulence detection systems provide sparse data points that make it difficult for pilots to assess turbulence conditions between measurements, leading to incomplete information and potential safety risks.

Innovation Solution

A system that obtains and visually connects turbulence datapoints with lines to indicate turbulence severity and corridors between sparse measurements, using color coding and thickness to differentiate turbulence levels and fill gaps in data presentation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If turbulence measurements are taken only when turbulence is experienced, then measurement frequency increases during turbulent conditions, but data points become sparsely distributed during calm conditions making it difficult to assess turbulence between measurements

Engineering Contradiction:
Improveturbulence detection accuracyVSAvoidturbulence information between data points
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The system performs preliminary actions by continuously recording aircraft position and flight path data regardless of turbulence conditions. This preparatory data collection enables the later generation of connection lines that fill information gaps between sparse turbulence measurements, allowing pilots to assess turbulence conditions in areas between measured data points.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

Connection lines serve as an intermediary visual element that mediates between sparse turbulence data points. These lines represent the aircraft's flight path and indicate turbulence conditions in intermediate areas, providing pilots with continuous visual information rather than discrete, spaced-apart data points.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Device complexity

If data points are displayed as sparse individual points, then device complexity is reduced, but pilots cannot visually assess turbulence conditions in areas between data points

Engineering Contradiction:
Improvedisplay system simplicityVSAvoidturbulence information coverage
Core Design Contradiction:
Device complexityVSLoss of information

Solution Approach 1:

The system transitions from displaying zero-dimensional individual data points to displaying one-dimensional connection lines that trace the aircraft's flight path. This dimensional expansion provides continuous visual information about turbulence conditions along the flight path without requiring complex additional hardware or processing systems.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Loss of energy

If turbulence measurements are reported less frequently during calm conditions, then data transmission and processing requirements are reduced, but the ability to distinguish between flown and unflown areas is compromised

Engineering Contradiction:
Improvedata transmission energyVSAvoidspatial turbulence information
Core Design Contradiction:
Loss of energyVSLoss of information

Solution Approach 1:

The system performs preliminary action by continuously recording and storing aircraft position and flight path data during calm conditions. This preparatory data collection requires minimal energy for transmission while enabling the later generation of connection lines that provide comprehensive spatial turbulence information when displayed.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP4672199A1Turbulence detection and presentation system and method
Publication Date: 2025.12.31 THE BOEING CO
  • EP4672199A1 patent drawingFigure 1~2
  • EP4672199A1 patent drawingFigure 3
  • EP4672199A1 patent drawingFigure 4

AI summary

A method (300) for detecting and presenting turbulence can include obtaining turbulence datapoints (202, 204, 206) indicative of at least locations and turbulence measurements obtained during one or more aircraft flights, identifying increases or decreases between the turbulence measurements in the turbulence datapoints (202, 204, 206), and visually presenting the turbulence datapoints (202, 204, 206) and at least one connection between the turbulence datapoints (202, 204, 206). The turbulence datapoints (202, 204, 206) can be displayed to visually indicate and differentiate between the turbulence measurements, the connections (208) displayed to visually indicate turbulence between the locations of the turbulence measurements.