Aircraft Lighting Controller Automates External Lights

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Solution Overview

Problem

Aircraft pilots face a high task load during takeoff, landing, and taxiing due to the complexity of managing various external light systems, which can lead to reduced visibility and increased pilot distraction from inappropriate lighting.

Innovation Solution

An aircraft lighting system with a controller that determines the operational state of the aircraft and automatically activates, deactivates, or adjusts the brightness of various lights, such as taxi, takeoff, landing, and logo lights, using sensors and data sources to optimize visibility and reduce pilot workload.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the pilot manually manages various external light systems during taxiing, takeoff, and landing, then the lighting can be controlled, but the pilot task load increases and visibility may be reduced due to distraction

Engineering Contradiction:
Improvepilot task loadVSAvoidvisibility
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The lighting system automatically determines the aircraft operational state using sensors and data sources, then autonomously controls the activation and configuration of appropriate lights without requiring manual pilot input. The system serves itself by monitoring its own operational context and adjusting lighting accordingly, eliminating the burden of manual management while ensuring appropriate visibility.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system continuously monitors aircraft operational state through multiple sensors and data sources, using this feedback to dynamically adjust lighting configuration. This closed-loop control ensures the lighting system responds appropriately to changing operational conditions, maintaining optimal visibility while reducing pilot workload.

Inventive Principle:
Principle #23Feedback

2Illumination intensity

If multiple external lights are activated simultaneously, then visibility is improved, but inappropriate lighting may cause pilot distraction

Engineering Contradiction:
ImprovevisibilityVSAvoidpilot distraction
Core Design Contradiction:
Illumination intensityVSEase of operation

Solution Approach 1:

The system activates specific lights based on the local operational context of the aircraft. Different lighting configurations are applied to different operational states (taxiing, takeoff, landing, in-flight), ensuring that only the appropriate lights for the current situation are activated. This localized approach to lighting control provides necessary visibility without causing pilot distraction from inappropriate lighting.

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If the pilot manually switches on and off various external lights during operational stages, then lighting control is achieved, but the complexity of aircraft systems increases

Engineering Contradiction:
Improvelighting controlVSAvoidaircraft systems complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The controller serves multiple functions: it determines aircraft operational state, selects appropriate lighting configurations, controls light activation, and monitors operational parameters. This multi-functional approach consolidates what would otherwise require separate manual controls for each light and operational stage, reducing overall system complexity while maintaining adaptability across different operational conditions.

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

Data Source

PatentEP3254972B1Systems and methods for dynamic light control
Publication Date: 2023.04.26 GOODRICH CORP
  • EP3254972B1 patent drawingFigure 1
  • EP3254972B1 patent drawingFigure 2
  • EP3254972B1 patent drawingFigure 3

AI summary

A light system for an aircraft is provided. A light system may include a sensor (90) and a first aircraft light (22). A controller (110) may be coupled to the sensor and the first aircraft light and may perform operations including receiving data from the sensor, determining a status of the aircraft based on the data, and controlling the first aircraft light based on the status of the aircraft. The first aircraft light may include an external aircraft light and the operations may further include at least one of activating or deactivating the external aircraft light based on the status of the aircraft.