Aviation Weather Control System for Aircraft Notification

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Solution Overview

Problem

Current aviation weather systems face challenges in accurately predicting and notifying air traffic controllers about sudden weather phenomena like torrential rainstorms, which can affect airplanes during takeoff and landing, requiring reliance on experience and increased controller burden.

Innovation Solution

An aviation weather control system that utilizes a phased array weather radar to provide real-time weather information, predicts hazardous areas affected by weather phenomena, and notifies controllers of affected airplanes through a display system showing positional relationships, reducing the need for prior experience and minimizing controller workload.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If air traffic controllers manually monitor weather information and determine affected airplanes, then they can identify weather impacts, but the workload increases and requires prior experience

Engineering Contradiction:
Improveaccuracy of weather impact identificationVSAvoidcontroller workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system enables automatic identification of weather-affected airplanes through automated data processing that combines weather radar information with flight management system data. The calculation unit automatically determines which airplanes are affected by weather phenomena without requiring controller intervention, thus reducing workload while maintaining reliability

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The invention introduces an intermediary system comprising a communication unit and calculation unit that acts as a mediator between weather radar data and flight information. This intermediary automatically processes and correlates data from multiple sources to identify affected airplanes, relieving controllers of this complex analytical task

Inventive Principle:
Principle #24Intermediary (Mediator)

2Loss of information

If traditional weather monitoring systems are used, then basic weather information is available, but sudden weather phenomena cannot be predicted and affected airplanes cannot be identified

Engineering Contradiction:
Improveweather information completenessVSAvoidweather phenomenon detection accuracy
Core Design Contradiction:
Loss of informationVSMeasurement precision

Solution Approach 1:

The system establishes a feedback loop where the communication unit continuously receives weather radar information and flight data, the calculation unit processes this information to identify weather-affected airplanes, and the notification unit provides feedback to controllers. This closed-loop system ensures complete and accurate weather information is maintained and acted upon

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system performs preliminary action by proactively identifying and notifying controllers about airplanes that will be affected by sudden weather phenomena before the controllers would need to manually determine this. The calculation unit continuously analyzes data to predict and prepare notifications in advance

Inventive Principle:
Principle #10Preliminary action

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system effectively identifies and notifies controllers of airplanes likely to be affected by sudden weather phenomena, allowing for timely action and reducing the burden on air traffic controllers by providing accurate and automatic data processing and visualization of hazardous areas and affected aircraft.

Implementation Method 1

a phased array weather radar to provide real-time weather information

Methodology Applied
Scientific EffectRadar: Radar

Data Source

PatentEP3686866B1Aviation weather control system
Publication Date: 2024.06.26 KK TOSHIBA
  • EP3686866B1 patent drawingFigure 1
  • EP3686866B1 patent drawingFigure 2A~2B
  • EP3686866B1 patent drawingFigure 3A~3B

AI summary

According to one embodiment, there is provided an aviation weather control system including a processing unit including means for receiving weather information of an area to be overseen, specifying a weather phenomenon in the area to be overseen, and selecting an airplane affected by the weather phenomenon based on the weather phenomenon and takeoff/landing information of airplanes, and a notification unit configured to notify the selected airplane.