Aircraft Lighting Pod Merging Multiple Lights to Cut Weight

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Solution Overview

Problem

Conventional external lighting systems in aircraft are cumbersome, heavy, and require complex and laborious wiring, which adds significant weight and reduces efficiency in flight.

Innovation Solution

A multifunction lighting pod with an aerodynamic housing that integrates various lights, including taxi, landing, scene, hover, hoist, and searchlights, mounted underneath the aircraft's avionics bay, reducing wiring complexity and weight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Illumination intensity

If multiple external lights are deployed throughout the aircraft airframe, then illumination coverage and operational visibility are improved, but aircraft weight increases significantly due to additional lighting components and extensive wiring

Engineering Contradiction:
Improveillumination coverageVSAvoidaircraft weight
Core Design Contradiction:
Illumination intensityVSWeight of moving object

Solution Approach 1:

The patent consolidates multiple separate lighting systems (taxi lights, landing lights, scene lights, hover lights, searchlights, and indicator lights) into a single integrated lighting pod assembly. This merging approach maintains comprehensive illumination coverage while dramatically reducing the total weight by eliminating redundant mounting structures, housings, and extensive wiring harnesses that would be required if each light were installed separately throughout the airframe.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The lighting pod is designed as a multi-functional unit that performs the roles of multiple different lighting systems simultaneously. The single pod contains various types of lights (taxi, landing, scene, hover, search, and indicator lights) that can serve different operational purposes, replacing what would traditionally require multiple separate lighting installations distributed across the aircraft structure.

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

2Illumination intensity

If multiple lights are installed distributed throughout the aircraft, then comprehensive illumination is achieved, but installation complexity and labor requirements increase

Engineering Contradiction:
Improveillumination coverageVSAvoidinstallation complexity
Core Design Contradiction:
Illumination intensityVSEase of manufacture

Solution Approach 1:

By combining all lighting functions into a single pre-assembled pod unit, the installation process is simplified from multiple separate installations to one unified mounting operation. The pod arrives as a complete assembly with all lights, wiring, and mounting hardware integrated, requiring only a single attachment point to the aircraft structure rather than multiple distributed installations.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The lighting pod is pre-assembled and pre-wired as a complete functional unit before installation on the aircraft. All electrical connections, mounting brackets, and light positions are predetermined and configured in advance, eliminating the need for complex on-site wiring and installation work. This preliminary preparation significantly reduces installation time and complexity.

Inventive Principle:
Principle #10Preliminary action

3Weight of moving object

If a single integrated lighting pod is used, then weight and wiring complexity are reduced, but the ability to provide distributed illumination throughout the aircraft is limited

Engineering Contradiction:
Improveaircraft weightVSAvoiddistributed illumination
Core Design Contradiction:
Weight of moving objectVSIllumination intensity

Solution Approach 1:

The lighting pod employs adjustable and movable lighting elements that can direct illumination in multiple directions and angles from a single mounted position. Searchlights with adjustable aim, lights with varying beam patterns, and strategically positioned light sources within the pod create distributed illumination effects throughout the aircraft environment without requiring the pod to be physically distributed across multiple locations.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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 lighting pod provides efficient and stable illumination with reduced air drag and weight, improving flight balance and reducing certification costs, while allowing for quick installation and wireless control options.

Implementation Method 1

a vibration proof and G-force absorbing coupling bracket mounted to a base plate of the housing

Methodology Applied
Scientific EffectVibration absorption: Damping

Implementation Method 2

a vibration proof and G-force absorbing coupling bracket mounted to a base plate of the housing

Methodology Applied
Scientific EffectG-force absorption: Damping

Data Source

PatentUS12319436B1Aircraft fuselage lighting pod
Publication Date: 2025.06.03 NIELSEN CHRISTIAN R
  • US12319436B1 patent drawing
  • US12319436B1 patent drawing
  • US12319436B1 patent drawing

AI summary

A lighting pod for an aircraft, such as a helicopter. The lighting pod includes aerodynamic housing in which multiple lights are mounted in optimum positions providing efficient lighting and lesser air drag. The lighting pod includes taxi lights, landing lights, scene lights, rear lights, hover lights, hoist lights, and headlights. The lighting pod having all the essential lights can be easily installed and removed from an aircraft.