Aircraft Lighting System for Trailing Aircraft Warning

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Solution Overview

Problem

Conventional methods for transmitting information from leading aircraft to trailing aircraft are inefficient, particularly in rapidly changing weather conditions, leading to potential hydroplaning and unsafe separation distances due to delayed or missing communications about runway braking conditions.

Innovation Solution

An aircraft lighting system that includes external lights, a memory module, and a processor to compare received aircraft parameters to stored criteria, determining whether to illuminate the lights to convey information about braking conditions or flight path deviations to trailing aircraft.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional communication methods (ATC radio, pilot comments) are used to transmit runway condition information, then information can be transmitted, but the transmission is delayed and may be missed in high workload scenarios

Engineering Contradiction:
Improveinformation transmission reliabilityVSAvoidinformation transmission delay
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent introduces an intermediary system consisting of sensors, processors, and visual display devices that automatically detect runway conditions and flight path deviations, then communicate this information to trailing aircraft through visual displays. This intermediary system relieves the pilot of direct communication responsibilities while ensuring timely and reliable information transmission about braking conditions and flight path stability.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system enables self-service by automatically detecting runway braking conditions and flight path deviations without requiring pilot intervention. The sensor network and processing units continuously monitor conditions and automatically generate visual communications to trailing aircraft, freeing pilots from manual reporting duties while maintaining continuous situational awareness.

Inventive Principle:
Principle #25Self-service

2Loss of information

If pilots manually communicate braking conditions to ATC, then information can be conveyed, but the workload increases and communication may be omitted in high stress situations

Engineering Contradiction:
Improveinformation communication completenessVSAvoidpilot workload
Core Design Contradiction:
Loss of informationVSEase of operation

Solution Approach 1:

The system performs self-service by automatically detecting and communicating runway condition information through visual displays on trailing aircraft. The sensor network monitors braking conditions and the processor automatically generates visual messages, eliminating the need for manual pilot reporting while ensuring complete information transmission about runway surface conditions.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces the mechanical communication system (radio transmissions, verbal reports) with an automated optical display system. Visual display devices project information directly into the flight path of trailing aircraft, substituting the manual radio communication mechanism with an automated visual communication field that continuously displays runway condition data.

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

3Measurement precision

If CFME equipment is used to measure runway friction, then objective braking action data can be obtained, but the system has inherent lag and cannot detect rapid changes in braking conditions

Engineering Contradiction:
Improvebraking condition measurement accuracyVSAvoidresponse speed to changing conditions
Core Design Contradiction:
Measurement precisionVSSpeed

Solution Approach 1:

The patent segments the runway monitoring function into multiple distributed sensors along the runway surface, each independently measuring local braking conditions. This segmentation allows parallel data collection from multiple points simultaneously, providing both precise local measurements and rapid detection of changing conditions across the runway surface without the single-point lag of traditional CFME.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system performs preliminary action by continuously monitoring runway conditions before trailing aircraft reach the runway threshold. Sensors detect braking conditions in advance, and the system proactively displays this information to approaching aircraft, allowing pilots to prepare for anticipated runway conditions rather than reacting to lagged measurements after touchdown.

Inventive Principle:
Principle #10Preliminary action

4Speed

If visual display devices are positioned in the flight path of trailing aircraft, then information is immediately visible, but the display must be highly visible against varying background conditions

Engineering Contradiction:
Improveinformation delivery speedVSAvoiddisplay visibility
Core Design Contradiction:
SpeedVSIllumination intensity

Solution Approach 1:

The patent employs color changes in the visual display devices to convey different runway condition states and attract pilot attention. The display system uses distinct colors to indicate varying braking conditions (e.g., green for good, yellow for medium, red for poor) and adjusts color intensity to ensure visibility against different background conditions, leveraging human color perception to rapidly communicate critical information.

Inventive Principle:
Principle #32Color changes

Solution Approach 2:

The system changes multiple display parameters including brightness, contrast, and spatial positioning to optimize information visibility. The display devices adjust their illumination intensity and positional orientation based on detected background conditions and aircraft approach characteristics, dynamically modifying display parameters to maintain optimal visibility across varying environmental conditions.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10604273B2Aircraft lighting system for informing trailing aircraft
Publication Date: 2020.03.31 HONEYWELL INTERNATIONAL INC
  • US10604273B2 patent drawing
  • US10604273B2 patent drawing
  • US10604273B2 patent drawing

AI summary

Systems and methods for alerting trailing aircraft about conditions experienced by a leading aircraft are disclosed herein. The systems and methods include an aircraft lighting system, which includes at least one external aircraft light and a memory module configured to store at least one criterion associated with an aircraft parameter. The systems and methods further include a receiver module operably connected to the memory module which is configured to receive an aircraft parameter. The systems and methods also include a processor module operably connected to the memory module, the receiver module and the at least one external aircraft light, the processor being configured to compare the received aircraft parameter to the stored at least one criterion and is further configured to determine, on the basis of the comparison, whether to cause illumination of the at least one external aircraft light for observance by trailing aircraft.