Passive Thermal Imaging for Aircraft Hazards

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Solution Overview

Problem

Current systems fail to effectively detect clear air turbulence (CAT), high altitude ice crystals (HAIC), and volcanic ash clouds (VAC) in a single, efficient manner, posing risks to aircraft safety and comfort.

Innovation Solution

A passive thermal imaging system with multiple detection units and processing electronics that utilize thermal electromagnetic radiation, cross-correlation techniques, and brightness temperature difference analysis to distinguish between CAT, HAIC, and VAC, reducing false alarm rates and enabling detection up to 200 miles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If separate detection systems are used for CAT, HAIC, and VAC, then detection reliability for each hazard is improved, but device complexity increases and operational efficiency decreases

Engineering Contradiction:
Improvedetection reliabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines three separate detection systems (CAT detection, HAIC detection, and VAC detection) into a single integrated optical system that uses one detector array to detect all three hazards simultaneously by analyzing thermal radiation at different wavelength ranges, thereby reducing device complexity while maintaining detection reliability

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The optical system is designed with multi-functionality to detect multiple types of atmospheric hazards (CAT, HAIC, and VAC) using a single detector array by processing thermal radiation signals at different wavelength ranges, allowing one system to perform multiple detection functions

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

2Device complexity

If multiple detection channels are integrated into a single system, then device complexity is reduced, but measurement precision for distinguishing between different hazards may worsen

Engineering Contradiction:
Improvesystem complexityVSAvoidhazard differentiation precision
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The detection system segments the thermal radiation spectrum into different wavelength ranges (first wavelength range and second wavelength range) that are selectively processed to distinguish between different hazards, allowing precise differentiation while using a single integrated detector array

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system applies different detection criteria and processing methods to different wavelength ranges detected by the same detector array, with specific wavelength ranges optimized for detecting specific hazards (e.g., certain wavelengths for ice crystals, others for volcanic ash), enabling precise hazard identification through localized analysis

Inventive Principle:
Principle #3Local quality

3Length of stationary object

If detection range is extended to 200 miles, then early warning capability is improved, but false alarm rate increases

Engineering Contradiction:
Improvedetection rangeVSAvoidfalse alarm rate
Core Design Contradiction:
Length of stationary objectVSReliability

Solution Approach 1:

The system uses feedback mechanisms where detected signals are continuously analyzed and cross-correlated to distinguish between actual hazards and false alarm sources, with processing electronics that adjust detection thresholds based on signal patterns to maintain low false alarm rates at extended detection ranges

Inventive Principle:
Principle #23Feedback

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 achieves low false alarm rates and effective detection of CAT, HAIC, and VAC, providing enhanced safety and comfort for aircraft by accurately identifying these hazards at significant ranges.

Implementation Method 1

a first detection unit comprising at least one first detector array configured to detect thermal electromagnetic radiation (EMR)

Methodology Applied
Scientific EffectThermal radiation: Thermal Radiation

Data Source

PatentUS9924138B1Combined air-turbulence, ice, volcanic-ash aerosols, passive LWIR optical systems for cruising-airplane safety
Publication Date: 2018.03.20 ROCKWELL COLLINS INC
  • US9924138B1 patent drawing
  • US9924138B1 patent drawing
  • US9924138B1 patent drawing

AI summary

A passive thermal imaging system, includes a first detection unit, a second detection unit, imaging optics and processing electronics. The first detection unit and second detection unit each include at least one first detector array. The imaging optics are configured to image a first wavelength range of received EMR onto the at least one first detector array, and to image a second wavelength range of the received EMR onto the at least one second detector array. The processing electronics are configured to receive a first detected signal from the at least one first detector array and to determine whether a first detection event has occurred based on the first detected signal, and to receive a second detected signal from the at least one second detector array and to determine whether a second detection event and a third detection event have occurred based on the second detected signal.