Aircraft Fuselage Light Communication for Secure High-Speed Links

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Solution Overview

Problem

Existing radio frequency (RF) communication systems in aircraft face interference issues due to atmospheric noise, limited bandwidth, and security concerns, including easy interception of signals.

Innovation Solution

Implementing light communication (Li-Fi) systems using existing aircraft lighting and dedicated light sources for secure, interference-free data transmission and reception, leveraging a vast bandwidth in the visible and invisible light spectrum.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If radio frequency (RF) communication is used for aircraft communication, then communication capability is provided, but interference from atmospheric noise and limited bandwidth occur

Engineering Contradiction:
Improvecommunication reliabilityVSAvoidatmospheric noise interference
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent replaces RF electromagnetic wave-based communication with visible light-based communication. This substitution moves the communication medium from the RF spectrum to the visible light spectrum, thereby avoiding atmospheric noise interference that affects RF communications while providing abundant bandwidth for aircraft communication.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If RF communication is used, then communication is enabled, but security concerns arise due to easy signal interception

Engineering Contradiction:
Improvecommunication securityVSAvoidsignal interception vulnerability
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent substitutes RF communication with visible light communication. Visible light can be precisely directed and confined to specific spatial paths, making it much harder to intercept compared to omnidirectional RF signals. This provides inherent physical layer security for aircraft communications.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Productivity

If RF communication is used, then communication is provided, but bandwidth is limited and FCC frequency restrictions apply

Engineering Contradiction:
Improvedata transmission rateVSAvoidfrequency band availability
Core Design Contradiction:
ProductivityVSAdaptability or versatility

Solution Approach 1:

The patent changes the fundamental parameter of the communication medium from RF waves to visible light waves. This parameter change opens up the vast visible light spectrum for communication use, providing enormously increased bandwidth and eliminating FCC frequency restrictions that constrain RF communication systems.

Inventive Principle:
Principle #35Parameter changes

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

Enhances security and stealth capabilities by reducing electronic signatures while providing high-speed data transmission, overcoming RF limitations with increased bandwidth and secure data exchange.

Implementation Method 1

The LC transmitter may be a Light Emitting Diode (LED) or a laser

Methodology Applied
Scientific EffectLight Emitting Diode: Light Emitting Diode

Implementation Method 2

The LC receiver may be a photodetector

Methodology Applied
Scientific EffectPhotodetector: Photoelectric Effect

Data Source

PatentEP4016875B1Light communication between aircraft
Publication Date: 2025.09.24 TEXTRON INNOVATIONS INC
  • EP4016875B1 patent drawingFigure 1
  • EP4016875B1 patent drawingFigure 2
  • EP4016875B1 patent drawingFigure 3

AI summary

Embodiments are directed to systems and methods for providing light communication (LC) for an aircraft (101, 201). An LC transmitter (303) is mounted on an aircraft fuselage and is configured to broadcast light signals within a defined region outside the aircraft (101, 201). An LC receiver (313) mounted on the aircraft fuselage (101, 201) is configured to receive light signals broadcast by a remote LC device. A controller (307) is configured to manage LC signals in the aircraft (101, 201), and an interface (704) is provided between the controller (307) and an aircraft data network (309, 705). The light signals may be in a visible light spectrum, an invisible light spectrum, or both. The remote LC device may be, for example, a ground station (401, 401a, 402), an aircraft (502, 503), a ground vehicle, a ship, a building, or a portable transmitter.