Aircraft Exit Door Indication System Using Dynamic Light Sequencing

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Solution Overview

Problem

Current emergency exit guidance systems in aircraft are inadequate as they may not be highly visible in low-light or smoky conditions, leading to confusion and misinterpretation of exit locations during emergencies.

Innovation Solution

An aircraft emergency exit door indication system using a controller and sensors to operate light sources along aisles, which are sequentially pulsed to direct passengers to available exits, with color changes indicating exit availability and unavailability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Illumination intensity

If static signs and phosphorescent floor marking are used for exit identification, then the system structure is simple, but the visibility and effectiveness are reduced in darkness or smoky conditions

Engineering Contradiction:
Improvevisibility of exit signsVSAvoidsystem structure
Core Design Contradiction:
Illumination intensityVSDevice complexity

Solution Approach 1:

The patent transforms static exit signs into dynamic lighting systems that can change intensity, color, and pattern. The lighting system responds to sensor inputs (smoke detection, motion detection) and actively adjusts its behavior to guide passengers to available exits, resolving the contradiction between visibility and complexity by using adaptive control algorithms.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes multiple parameters simultaneously: illumination intensity (brightness levels), color (to indicate exit availability or hazards), and temporal patterns (flashing sequences). These parameter changes enable the system to communicate complex information about multiple exits and their status without requiring proportionally complex hardware.

Inventive Principle:
Principle #35Parameter changes

2Loss of information

If multiple light sources are used to indicate different exit directions, then the guidance information becomes more comprehensive, but the system complexity and cost increase

Engineering Contradiction:
Improveexit availability informationVSAvoidnumber of light sources
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

Each light source in the system is designed to perform multiple functions: indicating exit location, showing exit availability status, providing directional guidance through sequential activation, and alerting passengers to hazards. This multi-functionality reduces the need for separate specialized components for each function, thereby reducing overall system complexity while maintaining comprehensive information delivery.

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

Solution Approach 2:

The system uses color changes in the light sources to encode different types of information about exit availability and conditions. Different colors represent different states (e.g., green for available, red for blocked), allowing the system to communicate complex status information using the same physical light sources without requiring additional indicators.

Inventive Principle:
Principle #32Color changes

3Ease of operation

If light sources are sequentially pulsed to create travelling light paths, then the directional guidance becomes more clear and unambiguous, but the control system complexity increases

Engineering Contradiction:
Improvedirectional guidance clarityVSAvoidcontrol system
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The system uses periodic pulsing of light sources in sequential patterns to create travelling light paths that clearly indicate direction. The periodic nature of this action (repeating sequences) simplifies the control logic compared to continuous variable control, as it relies on timing and sequencing rather than analog control, thereby reducing control system complexity while maintaining guidance clarity.

Inventive Principle:
Principle #19Periodic action

4Measurement precision

If real-time sensor feedback is implemented to indicate exit availability, then the guidance accuracy improves, but the system complexity and power consumption increase

Engineering Contradiction:
Improveexit availability detectionVSAvoidpower consumption
Core Design Contradiction:
Measurement precisionVSUse of energy by moving object

Solution Approach 1:

The system implements sensor feedback loops that detect exit conditions (availability, hazards) and automatically adjust the lighting guidance accordingly. The feedback is processed using threshold-based logic and simple state machines rather than complex continuous control, enabling real-time adaptation while maintaining reasonable power consumption through event-triggered updates rather than continuous operation.

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 effectively guides passengers to the nearest safe exit by providing clear and unambiguous visual cues, reducing confusion and ensuring rapid evacuation in emergency situations.

Implementation Method 1

a first plurality of light sources, a controller in electronic communication with the first plurality of light sources

Methodology Applied
Scientific EffectLight emission: Light

Data Source

PatentUS10997831B2Exit door indication system
Publication Date: 2021.05.04 GOODRICH LIGHTING SYSTEMS INC
  • US10997831B2 patent drawing
  • US10997831B2 patent drawing
  • US10997831B2 patent drawing

AI summary

An aircraft emergency exit door indication system may comprise a first plurality of light sources, a controller, and a first sensor associated with a first exit door. The first sensor feedback signal indicates an availability for egress through the first exit door. The first plurality of light sources is operated by the controller based upon the first sensor feedback signal. The light sources may be lights that already exist in an aircraft such as ceiling wash lights, sidewall wash lights, floor path lights, dome lights, or passenger service unit lights. The system may include a second plurality of light sources logically separated from the first plurality of light sources based upon its location relative to the first exit door and a second exit door.