Aircraft Passenger Service Unit Lighting for Low-Weight Cabin Illumination

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Solution Overview

Problem

Conventional passenger cabin lights in aircraft are heavy and require significant electric power, lacking energy efficiency.

Innovation Solution

An aircraft overhead passenger service unit with integrated visual sign structures that include switchable LED lights for signaling and wall illumination, allowing for efficient cabin illumination without additional dedicated lighting devices.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Illumination intensity

If conventional passenger cabin lights are used for illuminating the passenger cabin, then the passenger cabin can be illuminated, but the weight of the aircraft increases considerably and a large amount of electric power is required

Engineering Contradiction:
Improvepassenger cabin illuminationVSAvoidaircraft weight
Core Design Contradiction:
Illumination intensityVSWeight of moving object

Solution Approach 1:

The patent combines the illumination function with the existing overhead passenger service unit (PSU) structure. The PSU, which already houses lighting elements for passenger information display, is used to provide cabin illumination as well. This merging of functions eliminates the need for separate dedicated illumination devices, thereby reducing the additional weight that would otherwise be required for independent lighting systems.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The overhead passenger service unit is designed to perform multiple functions: it displays passenger information through light sources and simultaneously provides illumination for the passenger cabin. By making the PSU multi-functional, the patent avoids the need for separate dedicated illumination devices, thereby reducing the additional weight that would otherwise be required.

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

2Illumination intensity

If conventional passenger cabin lights are used for illuminating the passenger cabin, then the passenger cabin can be illuminated, but a large amount of electric power is required

Engineering Contradiction:
Improvepassenger cabin illuminationVSAvoidelectric power consumption
Core Design Contradiction:
Illumination intensityVSUse of energy by moving object

Solution Approach 1:

The patent combines the illumination function with the existing overhead passenger service unit (PSU) structure. The PSU, which already houses lighting elements for passenger information display, is used to provide cabin illumination as well. This merging of functions eliminates the need for separate dedicated illumination devices, thereby reducing the additional weight that would otherwise be required for independent lighting systems.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The overhead passenger service unit utilizes its own existing light sources and electrical infrastructure to provide illumination functionality. The PSU's lighting elements, which are already powered and positioned within the unit, are repurposed to also illuminate the passenger cabin, allowing the system to serve dual purposes without requiring additional power infrastructure.

Inventive Principle:
Principle #25Self-service

3Illumination intensity

If separate dedicated illumination devices are installed for cabin illumination, then the illumination function is enhanced, but the device complexity increases

Engineering Contradiction:
Improvepassenger cabin illuminationVSAvoidlighting system complexity
Core Design Contradiction:
Illumination intensityVSDevice complexity

Solution Approach 1:

The patent combines the illumination function with the existing overhead passenger service unit (PSU) structure. The PSU, which already houses lighting elements for passenger information display, is used to provide cabin illumination as well. This merging of functions eliminates the need for separate dedicated illumination devices, thereby reducing the additional weight that would otherwise be required for independent lighting systems.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The overhead passenger service unit is designed to perform multiple functions: it displays passenger information through light sources and simultaneously provides illumination for the passenger cabin. By making the PSU multi-functional, the patent avoids the need for separate dedicated illumination devices, thereby reducing the additional weight that would otherwise be required.

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

Provides high-energy efficiency and reduced weight by utilizing the overhead passenger service unit for both signaling and wall illumination, reducing the need for separate lighting systems.

Implementation Method 1

The signal light comprises at least one first switchable light source

Methodology Applied
Scientific EffectLight Emitting Diode: Light Emitting Diode

Implementation Method 2

The wall illumination light comprises at least one second switchable light source

Methodology Applied
Scientific EffectLight Emitting Diode: Light Emitting Diode

Data Source

PatentUS12503230B2Aircraft overhead passenger service unit, aircraft, and method of illuminating a passenger cabin of an aircraft
Publication Date: 2025.12.23 GOODRICH LIGHTING SYST GMBH
  • US12503230B2 patent drawing
  • US12503230B2 patent drawing
  • US12503230B2 patent drawing

AI summary

An aircraft overhead passenger service unit, which is configured to be mounted in a passenger cabin of an aircraft above a passenger seating space, comprises a visual sign structure extending downward from the aircraft overhead passenger service unit. The visual sign structure comprises a signal light and a wall illumination light. The signal light is arranged on a first side of the visual sign structure facing rearward. The signal light comprises at least one first switchable light source. The wall illumination light is arranged on a second side of the visual sign structure facing forward. The wall illumination light comprises at least one second switchable light source and a light directing element. The at least one second switchable light source and the light directing element are arranged to provide a wall illumination light output towards a lateral side of the aircraft overhead passenger service unit.