Aircraft Weather Radar Lightning Flash Rate Estimation

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Solution Overview

Problem

Conventional aircraft weather radar systems fail to accurately indicate the severity of weather hazards, particularly convective threats like lightning, leading to inefficient weather avoidance decisions by pilots.

Innovation Solution

A method and system that estimate a lightning flash rate using radar reflectivity and temperature data from horizontal and vertical scans, adjusting the display to better map weather hazards and aid pilots in navigating through severe weather conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional radar reflectivity processing is used to determine threat level, then the system is simple to operate, but the measurement precision of weather hazard severity is insufficient

Engineering Contradiction:
Improvethreat level indication accuracyVSAvoidprocessing complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent segments the weather hazard assessment into multiple independent components: radar reflectivity analysis, lightning flash rate estimation, and threat level mapping. Each component processes specific parameters separately before integration, allowing complex processing to be divided into manageable segments that improve measurement precision without overwhelming system complexity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces a new dimension of lightning flash rate estimation based on radar reflectivity data, transforming the traditional single-parameter reflectivity measurement into a multi-parameter assessment system. This dimensional expansion enables more accurate threat level indication by adding vertical depth analysis through flash rate calculations

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

2Reliability

If pilots avoid less severe weather cells by too much, then safety is improved, but flight efficiency deteriorates

Engineering Contradiction:
Improveflight safetyVSAvoidflight efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent implements feedback by continuously monitoring radar reflectivity and lightning flash rate, then updating threat level indications in real-time. This feedback loop provides pilots with accurate, dynamic weather hazard information, enabling them to make informed navigation decisions that balance safety with flight efficiency by avoiding only genuinely severe cells

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent changes the parameter representation from simple color-coded reflectivity levels to a more nuanced system incorporating lightning flash rate estimates. This parameter transformation provides pilots with better discrimination between different hazard levels, allowing more precise weather avoidance decisions that maintain safety while improving flight efficiency

Inventive Principle:
Principle #35Parameter changes

3Productivity

If pilots fly too close to severe cells, then flight efficiency is improved, but exposure to harmful factors increases

Engineering Contradiction:
Improveflight efficiencyVSAvoidconvective hazard exposure
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The patent performs preliminary action by estimating lightning flash rates and determining threat levels before pilots encounter severe weather cells. This advance warning allows pilots to plan efficient routes that maintain safe distances from hazardous cells while minimizing deviation from optimal flight paths

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 provides a more accurate assessment of weather hazard threat levels, enabling pilots to avoid severe convective-related hazards by identifying high lightning flash rates and surrounding regions to be avoided, thus enhancing safety and efficiency in flight operations.

Implementation Method 1

An airborne radar of an aircraft may be configured to detect reflectivity of weather cells in front of the aircraft

Methodology Applied
Scientific EffectRadar: Radar

Data Source

PatentUS9134418B1Weather hazard threat level computation and display
Publication Date: 2015.09.15 ROCKWELL COLLINS INC
  • US9134418B1 patent drawing
  • US9134418B1 patent drawing
  • US9134418B1 patent drawing

AI summary

A method for computing and displaying a weather hazard threat level for a weather radar system of an aircraft includes receiving weather radar returns from a radar antenna of the weather radar system. The weather radar returns include at least one of horizontal scans and vertical scans. Radar reflectivity may be determined from the weather radar returns, and, for at least one of the horizontal scan data and the vertical scan data, areas of radar reflectivity and a temperature associated with the areas of radar reflectivity may be determined. A lightning flash rate may be estimated using the radar reflectivity, areas of radar reflectivity, and temperature associated with the areas of radar reflectivity. Weather radar information may then be displayed, wherein the weather radar information is adjusted on the display based on the lightning flash rate.