Onboard Weather Radar Wake Vortex Prediction From Aircraft Returns

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Solution Overview

Problem

Existing aircraft radar systems lack the capability to reliably and accurately predict wake vortices from nearby aircraft, relying on external systems like TCAS or ADS-B, which can be unreliable or unavailable.

Innovation Solution

Aircraft-mounted weather radar systems are configured to emit radar signals, process return signals to detect and identify nearby aircraft, determine their size and characteristics, and predict wake vortices based on these parameters, providing real-time alerts and displays.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If aircraft rely on external systems like TCAS or ADS-B to detect wake vortices, then wake vortex detection capability is provided, but system reliability deteriorates when external systems are unavailable or unreliable

Engineering Contradiction:
Improvewake vortex detection reliabilityVSAvoiddependence on external systems
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The weather radar system is configured to perform multiple functions: traditional weather detection and new wake vortex detection. By utilizing the existing radar infrastructure for dual purposes, the system eliminates dependence on external systems while maintaining reliability. The radar processor analyzes return signals to detect both weather patterns and wake vortex signatures, making the aircraft self-sufficient for wake vortex detection.

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

Solution Approach 2:

The aircraft uses its own onboard weather radar system to detect wake vortices generated by other aircraft, rather than relying on external systems. The radar transmitter emits signals that reflect off wake vortices, and the radar processor analyzes these returns to determine wake vortex presence, position, and intensity, enabling the aircraft to serve its own wake vortex detection needs independently.

Inventive Principle:
Principle #25Self-service

2Measurement precision

If dedicated wake vortex detection systems are implemented, then wake vortex detection accuracy is improved, but size, weight, power, and cost increase

Engineering Contradiction:
Improvewake vortex detection accuracyVSAvoiddetection system weight
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The existing weather radar system is repurposed to perform both traditional weather detection and wake vortex detection functions. The same antenna, transmitter, and processor are used for dual purposes, eliminating the need for additional dedicated hardware. This multi-functional approach achieves accurate wake vortex detection without increasing system weight.

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

Solution Approach 2:

The wake vortex detection functionality is merged with the existing weather radar system rather than being implemented as a separate dedicated system. The radar processor combines analysis of return signals for both weather phenomena and wake vortex characteristics, consolidating detection capabilities into a single integrated system that reduces overall weight and complexity.

Inventive Principle:
Principle #5Merging (Combining)

3Adaptability or versatility

If weather radar systems are configured for wake vortex detection, then detection functionality is enhanced, but system complexity increases

Engineering Contradiction:
Improvedetection functionalityVSAvoidradar system configuration
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The radar system dynamically adjusts its operational mode based on detection needs. The processor can switch between weather detection mode and wake vortex detection mode, or operate in combined mode. This dynamic adaptability allows the system to enhance detection functionality while managing complexity through flexible, reconfigurable processing rather than fixed complex hardware.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The radar system is configured to perform multiple detection functions using the same hardware infrastructure. The processor analyzes return signals to identify both weather patterns and wake vortex characteristics, providing enhanced detection versatility without proportionally increasing system complexity through shared computational resources and unified signal processing.

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

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

Enhances detection functionality with reduced size, weight, power, and cost, improving responsivity and accuracy in predicting wake vortices, ensuring safer and smoother flights without reliance on external systems.

Implementation Method 1

The onboard radar system may be mounted on the aircraft and may use radar beams to detect reflected radar signals from weather formations such as convective weather cells associated with turbulence, rain, lightning, and hail

Methodology Applied
Scientific EffectRadar: Radar

Implementation Method 2

Radar systems may, in some examples, emit one or more radar signals. These radar signals may reflect and/or scatter off one or more objects and return to the radar system as radar return signals

Methodology Applied
Scientific EffectReflection: Reflection

Data Source

PatentUS20260043901A1Wake vortex prediction using weather radar
Publication Date: 2026.02.12 HONEYWELL INTERNATIONAL INC
  • US20260043901A1 patent drawing
  • US20260043901A1 patent drawing
  • US20260043901A1 patent drawing

AI summary

An example weather radar system includes one or more antennae configured to transmit a radar signal and receive a radar return signal and processing circuitry configured to detect an aircraft based on the radar return signal. The processing circuitry is further configured to, in response to detecting the aircraft, determine, based on a strength of the radar return signal, a size of the aircraft and predict, based on the size of the aircraft, a wake vortex of the aircraft including a predicted position of the predicted wake vortex.