Magnetic Composite Antenna for Bandwidth and Size Reduction

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Solution Overview

Problem

Existing low profile antennas, such as planar and patch antennas, are bandwidth-limited and unsuitable for low frequency applications due to their resonant nature and the properties of conductive materials used in aircraft surfaces, necessitating a solution for enhanced bandwidth and reduced size and weight for increased installation flexibility.

Innovation Solution

An electrically small low profile antenna is developed using a composite laminate with a magnetic material, featuring an aperture coupled antenna element with an inclusive slot and microstrip feed network, and a lower ground plane to minimize electrical behavior changes caused by conductive surfaces, allowing for efficient signal propagation and circular polarization with increased bandwidth.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If existing planar antennas and patch antennas are used, then the antenna structure is simple and easy to manufacture, but the bandwidth is limited due to resonant nature

Engineering Contradiction:
Improveantenna structure simplicityVSAvoidbandwidth
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent employs a composite laminate structure consisting of magnetic material layers (providing high permeability for bandwidth enhancement), dielectric layers (for signal isolation and structural support), and conductive layers (for electromagnetic radiation). This multi-material composite approach enables the antenna to achieve enhanced bandwidth through magnetic resonance while maintaining a planar geometry that is relatively simple to manufacture using standard PCB and lamination techniques.

Inventive Principle:
Principle #40Composite materials

2Ease of manufacture

If conventional dielectric materials are used in patch antennas, then the manufacturing process is straightforward, but the bandwidth at lower frequencies is very small

Engineering Contradiction:
Improvemanufacturing process simplicityVSAvoidbandwidth at lower frequencies
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent fundamentally changes the electromagnetic parameters of the antenna system by incorporating magnetic material with high permeability (μr = 55-65). This parameter change enables magnetic resonance operation at lower frequencies with significantly enhanced bandwidth compared to conventional dielectric-only patch antennas. The magnetic material allows the antenna to operate in a different resonance regime (magnetic dipole resonance) that provides broader bandwidth at lower frequency ranges while maintaining compatibility with standard manufacturing processes.

Inventive Principle:
Principle #35Parameter changes

3Volume of moving object

If antenna size is reduced for low profile applications, then the antenna becomes more compact and suitable for aircraft surfaces, but the bandwidth and performance deteriorate

Engineering Contradiction:
Improveantenna sizeVSAvoidbandwidth and performance
Core Design Contradiction:
Volume of moving objectVSAdaptability or versatility

Solution Approach 1:

The patent uses a composite laminate structure with magnetic material layers (high permeability) combined with dielectric and conductive layers. The magnetic material enables the antenna to achieve enhanced bandwidth and improved performance in a compact form factor by utilizing magnetic resonance effects that are not dependent on large physical dimensions. This allows the antenna to maintain low profile characteristics while overcoming the typical bandwidth limitations of electrically small antennas.

Inventive Principle:
Principle #40Composite materials

4Strength

If conductive materials are used for aircraft surfaces, then the structural integrity and conductivity are improved, but the antenna behavior changes and performance is affected

Engineering Contradiction:
Improvestructural integrity and conductivityVSAvoidantenna behavior stability
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The patent introduces dielectric layers as intermediary materials between the conductive aircraft surface and the antenna elements. These dielectric layers serve as isolation barriers that prevent direct interaction between the conductive aircraft surface and the antenna's electromagnetic fields, thereby stabilizing the antenna's electrical behavior. The dielectric material with appropriate permittivity (εr = 3.0-4.0) provides both mechanical support and electromagnetic decoupling, allowing the antenna to maintain consistent performance regardless of variations in the underlying conductive surface properties.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 solution provides a bandwidth-enhanced, low-profile antenna with reduced size and weight, capable of operating effectively across a broader frequency range while maintaining low air drag and visibility, suitable for applications in structural health monitoring and UAVs, with improved performance compared to existing antennas.

Implementation Method 1

a magnetic material, the magnetic material having a relative permeability of, for example, 55-65

Methodology Applied
Scientific EffectMagnetic material properties: Magnetism

Implementation Method 2

a conductor, extending through the composite laminate between the top surface and the bottom surface of the composite laminate, the conductor forming a microstrip feed extending from an antenna input to the antenna element

Methodology Applied
Scientific EffectMicrostrip transmission: Electromagnetic Induction

Implementation Method 3

the at least one antenna element comprises an antenna element portion and a slot

Methodology Applied
Scientific EffectAperture coupling: Electromagnetic Induction

Data Source

PatentUS11069953B2Electrically small antenna
Publication Date: 2021.07.20 THE BOEING CO
  • US11069953B2 patent drawing
  • US11069953B2 patent drawing
  • US11069953B2 patent drawing

AI summary

An electrically small low profile antenna is disclosed. The antenna comprises circuit board comprising a composite laminate, formed of a magnetic material and having at least one antenna element disposed on a top surface of the composite laminate, a conductive ground plane disposed on a bottom surface of the composite laminate, and a conductor, extending through the composite laminate between the top surface and the bottom surface of the composite laminate, the conductor forming a microstrip feed extending from an antenna input to the antenna element.