Aircraft Cabin Lighting Spectral Mode Control for Adaptive Effects

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Solution Overview

Problem

Current aircraft lighting systems lack the ability to dynamically adjust their spectral output based on various parameters, such as chromacity coordinates, color temperature, and brightness, to achieve specific desired effects like peak wakefulness or ambient mood changes.

Innovation Solution

A lighting system comprising multiple LEDs, controlled by a processor that transitions between different spectral weighting modes to optimize specific variables within defined domains, allowing for dynamic adjustment of lighting effects.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a lighting system uses fixed spectral output, then the device complexity is reduced, but the adaptability to different lighting conditions and desired effects is limited

Engineering Contradiction:
Improveadaptability to different lighting conditionsVSAvoiddevice complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The lighting system dynamically adjusts spectral output by transitioning between different spectral weighting modes (first, second, third modes) that optimize different variables (chromacity coordinates, color brightness temperature, color brightness) based on desired effects, making the system adaptive to different lighting conditions while managing complexity through controlled dynamic adjustment

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes spectral parameters by optimizing different predetermined variables within different predetermined domains corresponding to different spectral weighting modes, allowing adaptation to various lighting conditions and desired effects without requiring complete system redesign

Inventive Principle:
Principle #35Parameter changes

2Reliability

If the lighting system optimizes for peak wakefulness, then the lighting effectiveness for alertness is improved, but the power consumption increases

Engineering Contradiction:
Improvelighting effectivenessVSAvoidpower consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The system optimizes specific spectral parameters (chromacity coordinates, color brightness temperature) within predetermined domains to achieve desired effects like peak wakefulness, adjusting parameters dynamically to balance effectiveness with power consumption constraints in aircraft lighting

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If the lighting system transitions between multiple spectral weighting modes, then the versatility of lighting effects is improved, but the control complexity increases

Engineering Contradiction:
Improveversatility of lighting effectsVSAvoidcontrol complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The controller dynamically transitions between multiple spectral weighting modes (first, second, third modes) that correspond to different predetermined domains (chromacity coordinates, color brightness temperature, color brightness), enabling versatile lighting effects while managing control complexity through structured mode transitions

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The lighting system achieves multi-functionality by implementing multiple spectral weighting modes that can be activated based on different desired effects, allowing a single system to provide diverse lighting functions (mood creation, wakefulness enhancement, ambient lighting) without requiring separate dedicated systems

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

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 generates desired lighting effects by optimizing variables such as color saturation, CRI, and brightness, enhancing the cabin experience and operational efficiency.

Implementation Method 1

A first light emitting diode (LED) configured to emit a first electromagnetic radiation having a first wavelength

Methodology Applied
Scientific EffectLight emitting diode: Light Emitting Diode

Implementation Method 2

Each LED in the plurality of LEDs may be configured to emit an electromagnetic radiation having a wavelength, the wavelength being different for each LED in the plurality of LEDs

Methodology Applied
Scientific EffectElectromagnetic radiation emission: Electroluminescence

Data Source

PatentUS12227128B2Systems and methods for improved lighting
Publication Date: 2025.02.18 BE AEROSPACE INC
  • US12227128B2 patent drawing
  • US12227128B2 patent drawing
  • US12227128B2 patent drawing

AI summary

A method may comprise: commanding, by a processor, a lighting system to generate a first desired effect in accordance with a first spectral weighting mode; determining, by the processor, a first optimized predetermined variable within a first predetermined domain to generate the desired effect based on the first spectral weighting mode; commanding, by the processor, the lighting system to transition from the first desired effect to a second desired effect, the second desired effect in accordance with a second spectral weighting mode; and determining by the processor, a second optimized predetermined variable within a second predetermined domain to generate the second desired effect based on the second spectral weighting mode, the first optimized predetermined variable being different from the second optimized predetermined variable.