Predictive Wind Shear Radar Icon for Early Detection

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Solution Overview

Problem

Conventional wind shear detection systems in aircraft do not provide an advance warning of impending wind shear conditions, as they only indicate wind shear events when the F-factor exceeds a threshold of 0.085, failing to alert pilots of potential threats before they become critical.

Innovation Solution

A predictive wind shear warning system that uses radar returns to detect potential wind shear activity and provides a unique, smaller, and simpler visual indicator on the weather radar display, alerting pilots to developing wind shear conditions before they reach the standard warning threshold, with dynamic textual and graphical data updates in real-time.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the conventional PWS icon threshold (F-factor 0.085) is used to detect wind shear events, then the system maintains simplicity and clarity in display, but it fails to provide advance warning of potential wind shear conditions

Engineering Contradiction:
Improvewind shear detection accuracyVSAvoidwarning lead time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system performs preliminary detection of potential wind shear conditions by monitoring radar returns and calculating F-factor values before they reach the critical threshold. A new icon is displayed when the F-factor exceeds a lower threshold (e.g., 0.065), providing advance warning before a full wind shear event occurs at the higher threshold (0.085). This preliminary action allows pilots to take preventive measures before the actual wind shear event develops.

Inventive Principle:
Principle #10Preliminary action

2Loss of information

If a new potential wind shear icon is added to the display, then advance warning capability is improved, but the display complexity and information overload increase

Engineering Contradiction:
Improvewind shear information completenessVSAvoiddisplay complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The system applies local quality by creating a distinct, simplified icon design specifically for potential wind shear conditions. The new icon uses a unique graphical representation (e.g., different shape, color, or pattern) that is locally optimized for indicating developing threats, while the standard PWS icon remains unchanged for confirmed wind shear events. This localized differentiation allows pilots to quickly distinguish between potential and actual wind shear conditions without confusion.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The wind shear detection and display system is segmented into two distinct alert levels: a first alert level for potential wind shear conditions (F-factor > 0.065) displayed with a new icon, and a second alert level for confirmed wind shear events (F-factor > 0.085) displayed with the standard PWS icon. This segmentation allows the system to provide differentiated information for different threat levels, improving information completeness while maintaining display organization through clear visual separation of alert types.

Inventive Principle:
Principle #1Segmentation

3Loss of information

If the system monitors and displays developing wind shear activity below the PWS threshold, then situational awareness is improved, but the threshold criteria complexity increases

Engineering Contradiction:
Improvewind shear development informationVSAvoidthreshold criteria flexibility
Core Design Contradiction:
Loss of informationVSAdaptability or versatility

Solution Approach 1:

The system introduces a new parameter threshold (F-factor of 0.065) that is lower than the conventional PWS threshold (0.085). This parameter change enables the system to detect and display potential wind shear conditions at an earlier stage of development. The dual-threshold approach maintains adaptability by allowing the system to respond to different levels of wind shear activity with appropriate alert levels, providing versatile monitoring capability across the full range of wind shear development stages.

Inventive Principle:
Principle #35Parameter changes

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

This system allows pilots to anticipate wind shear warnings, enabling them to take proactive measures by providing earlier detection and more lead time to avoid potential wind shear events, thereby enhancing safety and decision-making.

Implementation Method 1

The weather radar system of the aircraft detects the presence of the wind shear event by detecting the Doppler frequency shift associated with the radar returns

Methodology Applied
Scientific EffectDoppler frequency shift: Doppler Effect

Data Source

PatentUS9658328B1System and method for indicating potential wind shear events
Publication Date: 2017.05.23 ROCKWELL COLLINS INC
  • US9658328B1 patent drawing
  • US9658328B1 patent drawing
  • US9658328B1 patent drawing

AI summary

An aircraft weather radar system can include an electronic display, a radar antenna for receiving radar returns, and an electronic processor. The electronic processor can be configured to determine an existence of potential wind shear activity using the radar returns and cause the electronic display to provide an indication of the potential wind shear activity. The potential wind shear activity is different than a wind shear condition associated with a predictive wind shear icon for a wind shear event.