Flexible High-Impedance Antenna Decoupling Device

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Solution Overview

Problem

Existing decoupling solutions for antennas on aircraft fuselages, such as high-impedance surfaces, face challenges due to rigid structures that do not conform well to curved surfaces, leading to aerodynamic disturbances and requiring complex installation and additional equipment, which increases weight and maintenance costs.

Innovation Solution

A flexible high-impedance device with a dielectric substrate and conducting patches, integrated with a ground plane, that can be easily fixed to the fuselage using adhesive, allowing for effective decoupling without significant aerodynamic disruption, suitable for both new and existing aircraft.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a rigid high-impedance surface device is used for decoupling antennas, then decoupling performance is improved, but aerodynamic disturbances increase and installation complexity increases

Engineering Contradiction:
Improvedecoupling performanceVSAvoidaerodynamic disturbances
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent applies this principle by replacing the rigid substrate with a flexible substrate that can conform to the curved surface of the aircraft fuselage. The flexible substrate eliminates the need for rigid structural support, thereby removing aerodynamic disturbances while maintaining the decoupling function through the high-impedance surface structure formed by conducting patches and ground plane.

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The patent applies this principle by designing the device to conform to the curved surface of the fuselage using a flexible substrate. The flexible nature allows the device to adapt to the spherical/curved geometry of the aircraft body, ensuring proper contact and decoupling performance without creating aerodynamic disruptions that would result from rigid, non-conforming structures.

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Reliability

If a rigid high-impedance surface device is used for decoupling antennas, then decoupling performance is improved, but device complexity and maintenance costs increase

Engineering Contradiction:
Improvedecoupling performanceVSAvoidinstallation complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The flexible substrate eliminates the need for complex rigid structural support systems, simplifying both the device structure and installation process. The flexibility allows direct mounting on curved surfaces without requiring additional mechanical components or complex assembly procedures, thereby reducing device complexity and maintenance requirements while preserving decoupling effectiveness.

Inventive Principle:
Principle #30Flexible shells and thin films

3Reliability

If antenna separation distance is increased to reduce coupling, then decoupling performance is improved, but space availability on fuselage is insufficient

Engineering Contradiction:
Improvedecoupling performanceVSAvoidavailable space on fuselage
Core Design Contradiction:
ReliabilityVSArea of stationary object

Solution Approach 1:

The patent introduces a high-impedance surface device as an intermediary element placed between the transmitting and receiving antennas. This intermediary structure creates an electromagnetic barrier that prevents direct coupling between the antennas, allowing them to be positioned closer together on the fuselage while maintaining effective decoupling performance, thus solving the space constraint problem.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Reliability

If redundant systems are provided to detect measurement errors from coupling, then measurement reliability is improved, but aircraft weight increases

Engineering Contradiction:
Improvemeasurement reliabilityVSAvoidaircraft weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent converts the harmful effect of antenna coupling into a beneficial solution by using the high-impedance surface to actively prevent coupling rather than merely detecting its effects. The flexible substrate with conducting patches and ground plane creates an electromagnetic barrier that proactively eliminates coupling issues, making redundant detection systems unnecessary and avoiding the weight penalty of additional equipment.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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 flexible device provides effective radioelectric decoupling between antennas on non-planar surfaces with minimal aerodynamic impact and simplified installation, reducing weight and maintenance costs while maintaining decoupling performance.

Implementation Method 1

a flexible high-impedance device with a dielectric substrate and conducting patches, integrated with a ground plane, that can be easily fixed to the fuselage using adhesive, allowing for effective decoupling

Methodology Applied
Scientific EffectHigh-impedance surface effect: Dielectric Permittivity

Data Source

PatentUS9577326B2Device for decoupling antennas mounted on an aircraft
Publication Date: 2017.02.21 EURON AERONAUTIC DEFENCE & SPACE
  • US9577326B2 patent drawing
  • US9577326B2 patent drawing
  • US9577326B2 patent drawing

AI summary

A high-impedance passive device to radio-electrically decouple two antennas operating at least partially within a common frequency band and arranged on a surface of the carrier structure. A substrate of the device has a flexible dielectric material layer having a predetermined thickness with patches of conductive material arranged on its surface and a layer to attach the device onto the surface of the carrier structure. The patches having predetermined shape and arrangement. The body of the substrate separates the dielectric layer from the surface of the carrier structure. The substrate thickness is determined based on the size, number, and arrangement of the patches, and further it is based on the aerodynamic constraints imposed on the device. The device having an impedance to cause the desired decoupling in the common frequency band.