Amphibious Aircraft Landing Surface Detection Using Multi-Wavelength Transceivers

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Solution Overview

Problem

Amphibious aircraft accidents often occur due to improper landing gear configuration, with existing warning and anti-flip systems being unreliable, requiring pilot input, and susceptible to errors and environmental interference.

Innovation Solution

A safety arrangement using multiple transceivers operating on different electromagnetic wavelengths to detect the landing surface type by analyzing reflection properties, including timing, intensity, and polarization, and automatically determining the correct landing gear position for the surface.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If warning systems are installed to alert pilots about improper landing gear configuration, then pilot awareness is improved, but system complexity increases

Engineering Contradiction:
Improvelanding safetyVSAvoidwarning system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical warning systems with a simple optical detection system using light transceivers. The system uses light transmission through water to automatically detect the landing surface type (water or ground) and provides warnings without requiring complex mechanical sensors or pilot input, thereby improving reliability while reducing system complexity.

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

Solution Approach 2:

The system automatically detects the landing surface type and provides warnings without requiring pilot input or manual operation. The transceivers continuously monitor the environment and the control unit automatically processes the information and generates warnings when improper gear configuration is detected, making the system self-operating and reducing complexity.

Inventive Principle:
Principle #25Self-service

2Device complexity

If single wavelength transceivers are used for detection, then device complexity is reduced, but measurement precision deteriorates due to environmental interference

Engineering Contradiction:
Improvetransceiver system complexityVSAvoidlanding surface detection accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The detection system is segmented into multiple transceivers operating at different wavelengths. Each transceiver measures light transmission at its specific wavelength, and the control unit processes these segmented measurements to determine the landing surface type. This segmentation allows the system to distinguish between water and ground by analyzing the differential absorption characteristics at different wavelengths, improving measurement precision while maintaining manageable device complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system changes the parameter of detection by using multiple wavelengths instead of a single wavelength. Different wavelengths of light are absorbed differently by water versus ground materials. By measuring transmission at multiple wavelengths and analyzing the differential absorption patterns, the system achieves high measurement precision in distinguishing landing surface types while avoiding the complexity of more sophisticated single-wavelength detection methods.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If retractable landing gear is used for amphibious aircraft, then adaptability is improved, but reliability deteriorates due to gear status errors

Engineering Contradiction:
Improvelanding surface adaptabilityVSAvoidgear configuration reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The system provides continuous feedback to the pilot about the correspondence between landing gear configuration and the actual landing surface type. The control unit monitors both the gear status and the detected surface type, and provides warnings when they do not match (e.g., gear extended when approaching water, or gear retracted when approaching ground). This feedback mechanism significantly improves reliability by preventing gear status errors while maintaining the adaptability of retractable landing gear for both water and ground operations.

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

Enhances the reliability of landing surface detection and landing gear configuration verification, reducing accidents by providing accurate and automatic alerts, and is less susceptible to environmental factors like dirt and shallow water conditions.

Implementation Method 1

the transceivers are configured to transmit electromagnetic wavelengths essentially towards the landing surface and at least one of the transceivers is configured to receive the reflections of the electromagnetic wavelengths

Methodology Applied
Scientific EffectReflection: Reflection

Data Source

PatentUS9586694B2Safety arrangement for aircraft and method for determining type of the landing surface for an aircraft
Publication Date: 2017.03.07 SUOKAS AVIONICS
  • US9586694B2 patent drawing
  • US9586694B2 patent drawing
  • US9586694B2 patent drawing

AI summary

A safety arrangement for an aircraft, especially for amphibious aircraft, being configured for determining a type of landing surface (such as water/solid ground) and including: two transceivers (301, 302); the first transceiver (301) configured to operate on first electromagnetic wavelength and the second transceiver (302) configured to operate on second electromagnetic wavelength differing from the first wavelength, and at least one of transceivers is configured to receive the reflections electromagnetic wavelengths, and determining element for determining the type of the landing surface based on the properties of two electromagnetic wavelengths reflected from the landing surface and for outputting a signal indicating the type of the determined landing surface.