Optical Particle Detector Fluorescence Polarization

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Solution Overview

Problem

Current aircraft systems lack effective detection methods for high concentrations of small ice crystals, dust particles, and volcanic ash, which can pose significant hazards to aviation safety and aircraft integrity.

Innovation Solution

An improved optoelectronic device that uses a combination of polarization and fluorescence detection to identify individual water droplets, ice crystals, dust particles, and volcanic ash particles, allowing for precise differentiation between these particle types.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If weather radar is used to detect precipitation-sized cloud particles, then detection of hydrometeors larger than 100 μM is improved, but detection of smaller particles (ice crystals, dust, ash) is lost

Engineering Contradiction:
Improveparticle size detection rangeVSAvoidparticle type detection capability
Core Design Contradiction:
Measurement precisionVSAdaptability or versatility

Solution Approach 1:

The detection system is segmented into multiple independent detection channels: a weather radar channel for detecting larger hydrometeors (>100 μM) and a laser-based optical particle detector for detecting smaller particles (ice crystals, dust, ash). Each channel operates with optimized parameters for its specific particle size range, allowing comprehensive coverage without compromising detection precision in either range

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The optical particle detector serves multiple functions by detecting different particle types (water droplets, ice crystals, dust particles, volcanic ash) using a single integrated system that combines wavelength discrimination and polarization analysis capabilities, enabling one system to perform what previously required multiple specialized detectors

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

2Measurement precision

If polarization detection is used to distinguish ice crystals from water droplets, then discrimination capability is improved, but detection of volcanic ash particles remains insufficient

Engineering Contradiction:
Improveparticle type discrimination accuracyVSAvoidparticle type coverage
Core Design Contradiction:
Measurement precisionVSAdaptability or versatility

Solution Approach 1:

The system uses wavelength-dependent detection to distinguish particle types. Volcanic ash particles exhibit different optical properties and light scattering characteristics at different wavelengths compared to ice crystals and water droplets. By analyzing the spectral characteristics and polarization state across multiple wavelengths, the system can identify and differentiate volcanic ash particles in addition to ice crystals and water droplets

Inventive Principle:
Principle #32Color changes

Solution Approach 2:

The detection approach combines multiple detection modalities (polarization detection, wavelength discrimination, fluorescence detection) into a composite detection system. This composite approach leverages the complementary strengths of each detection method to achieve comprehensive particle type identification, including the differentiation of volcanic ash which has distinct optical signatures when analyzed through multiple parameters simultaneously

Inventive Principle:
Principle #40Composite materials

3Device complexity

If visual observation by flight crew is used to detect particles, then system complexity is minimized, but detection reliability and precision are severely limited

Engineering Contradiction:
Improvedetection system structureVSAvoidparticle detection accuracy
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The system replaces manual visual observation by flight crew with an automated optoelectronic detection system that uses laser illumination, photodetectors, and signal processing electronics. This substitution eliminates human limitations in detecting small or transparent particles while providing continuous, objective measurements with quantifiable precision and reliability

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The detection system is designed to operate autonomously without requiring manual intervention or interpretation by flight crew. The system self-calibrates, automatically processes detected signals, identifies particle types based on optical characteristics, and provides real-time alerts, thereby maintaining high reliability while minimizing the operational burden on the flight crew

Inventive Principle:
Principle #25Self-service

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 device enables accurate detection and differentiation of hazardous particles, providing critical information for flight crews to take necessary avoidance measures, thereby enhancing aviation safety and reducing potential damage to aircraft.

Implementation Method 1

Return signals from scattered or reflected light are processed to provide the particle polarization information

Methodology Applied
Scientific EffectLight scattering: Scattering

Implementation Method 2

A source of polarized, monochromatic radiation transmits light along an optical pathway to illuminate a sample volume of air external to the aircraft

Methodology Applied
Scientific EffectPolarization: Polarisation

Implementation Method 3

a second optical system was added that processes fluorescent light from the same particles and can distinguish between particle types

Methodology Applied
Scientific EffectFluorescence: Fluorescence

Data Source

PatentUS12222276B2Optical particle detector with fluorescence
Publication Date: 2025.02.11 DROPLET MEASUREMENT TECHNOLOGIES LLC
  • US12222276B2 patent drawing
  • US12222276B2 patent drawing
  • US12222276B2 patent drawing

AI summary

Embodiments of the invention are directed to an optoelectronic device for detection and identification of individual water droplets, ice crystals, dust particles and volcanic ash particles, the device comprising a source of ultraviolet collimated monochromatic radiation that illuminates an area of air external to the aircraft through which freely pass individual atmospheric particles to create an illuminated sample volume of air; an optical surveillance system for monitoring the clarity of light transmission through the light transmissive window to indicate a need for preventive maintenance; a first optical detection system that is constructed and arranged to collect light scattered from individual particles over an explicit angle ranging from 137° to 173° that defines the illuminated sample volume for measurement of S and P components of return scattered light from the sample volume to photodetectors that provide signals representative of intensity and change in polarization state caused by the interaction of particles with the incident illumination in the sample volume; a second optical detection system for selectively detecting fluorescence emanating from individual ash particles over an explicit angle ranging from 137° to 173° that defines the illuminated sample volume for measurement of fluoresence from the sample volume to a photodetector that provide a signal representative of intensity caused by the interaction of particles with the incident illumination in the sample volume; a signal processor that is constructed and arranged to condition the signals from the photodetectors by removing electronic noise, restoring baseline shifts and analyzing the pulse shapes to provide processed signals; a signal analyzer configured to operate upon the processed signals for extraction of data representing maximum amplitude, width, rise time and fall time of individual pulses in the S and P components, and the magnitude of the fluorescence signal which correlates to the size and/or composition of ash particles present; an information synthesizer that receives the data and produces analytical results allocated to particles by particle type including equivalent optical diameter (EOD), number and mass size distributions, and number and mass concentrations, the particle type being selected as at least one member among the group consisting of individual water droplets, ice crystals, dust particles and volcanic ash particles; and a report generator that creates an information packet utilizing information from the information synthesizer to assist in decision making related to hazard avoidance for aircraft flight, the optoelectronic system being adapted for mounting and operation on an aircraft.