Aircraft Wireless Router Network with Distributed Nodes

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Solution Overview

Problem

Current wireless communication systems for aircraft face challenges in providing robust, broadband connectivity while being cost-effective, due to issues with weight, wiring complexity, and power loss, as well as interference at high altitudes.

Innovation Solution

A wireless communication system for aircraft featuring a router network with distributed connectivity nodes connected via a bus, utilizing both omnidirectional and directional antennas, where the type of antenna used is dynamically adjusted based on altitude to optimize performance and reduce interference.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If many antennas are arranged on the aircraft to provide multiple links and different antenna types, then communication capacity and reliability are improved, but wiring complexity and weight increase significantly

Engineering Contradiction:
Improvecommunication reliabilityVSAvoidwiring weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The router network is divided into multiple distributed connectivity nodes throughout the aircraft. Each node handles a subset of antenna connections, segmenting the wiring load and reducing the complexity of connecting all antennas to a single central router. This segmentation maintains communication reliability through distributed architecture while reducing overall wiring weight.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from a centralized two-dimensional wiring scheme to a three-dimensional distributed network architecture. Connectivity nodes are positioned at different locations throughout the aircraft volume, creating a spatially distributed topology that reduces wiring length and weight while maintaining or improving communication reliability through multiple paths.

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

2Device complexity

If traditional centralized router architecture is used, then system simplicity is maintained, but wiring complexity and power loss increase

Engineering Contradiction:
Improvesystem complexityVSAvoidpower loss
Core Design Contradiction:
Device complexityVSLoss of energy

Solution Approach 1:

The centralized router is segmented into multiple distributed connectivity nodes. Each node independently manages local antenna connections and routing functions, reducing the length of wiring required and thereby reducing power loss. The segmentation distributes the processing load and eliminates the need for long cable runs from a central point.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Distributed connectivity nodes act as intermediaries between antennas and the core routing function. Each node performs local signal processing and routing decisions, eliminating the need for signals to travel long distances through centralized wiring, thereby reducing power loss while maintaining manageable system complexity through standardized node interfaces.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Area of stationary object

If omnidirectional antennas are used at high altitudes, then coverage area is maximized, but interference from multiple ground base stations increases

Engineering Contradiction:
Improvecoverage areaVSAvoidinterference
Core Design Contradiction:
Area of stationary objectVSObject-affected harmful factors

Solution Approach 1:

The system dynamically switches between omnidirectional and directional antenna modes based on altitude. At high altitudes where interference from multiple ground base stations is problematic, the system transitions to directional antennas that provide focused beams. This dynamic adaptation maintains adequate coverage while reducing interference effects.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

Different antenna types are deployed in different spatial locations and operational contexts. Omnidirectional antennas are used when broad coverage is needed and interference is low, while directional antennas are used at high altitudes where interference is problematic. This local quality approach optimizes performance for specific operational conditions.

Inventive Principle:
Principle #3Local quality

4Object-affected harmful factors

If directional antennas are used exclusively, then interference is reduced at high altitudes, but coverage area and link availability decrease

Engineering Contradiction:
ImproveinterferenceVSAvoidcoverage area
Core Design Contradiction:
Object-affected harmful factorsVSArea of stationary object

Solution Approach 1:

The system dynamically selects between omnidirectional and directional antennas based on real-time conditions including altitude and signal quality. When interference is low and coverage is the priority, omnidirectional antennas are used. When altitude increases and interference becomes problematic, the system switches to directional antennas. This dynamic selection ensures optimal coverage while managing interference.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The communication system is designed with multi-functionality, supporting both omnidirectional and directional antenna operations. This universal capability allows the system to adapt to different operational requirements - using omnidirectional mode for maximum coverage and directional mode for interference reduction - thereby achieving both goals under different conditions.

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

Data Source

PatentEP3972153A1Communication system for aircrafts
Publication Date: 2022.03.23 ECOMELA
  • EP3972153A1 patent drawingFigure 1
  • EP3972153A1 patent drawingFigure 2
  • EP3972153A1 patent drawingFigure 3a

AI summary

A system and method for providing wireless data communication between a wireless communication system in an aircraft and a stationary communication server outside the aircraft are disclosed. The wireless communication system comprises a router network connected to a plurality of antennas, wherein the router network is configured to transmit and receive wireless data communication to and from a stationary communication server outside said aircraft through at least one ground base station via said antennas. The plurality of antennas comprises at least four groups of directional antennas, wherein said groups of directional antennas are arranged at separate portions of a fuselage of said aircraft, the fuselage thereby providing separation and shielding between each individual group of directional antennas.