Conformal Planar Dipole Antenna for UAVs

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Solution Overview

Problem

Existing antennas are bandwidth-limited and suffer from polarization loss due to their resonant nature and sensitivity to orientation, making them inefficient for conformal applications on non-planar surfaces, especially on vehicles with low radii of curvature like UAVs, where low air drag and radar cross section are crucial.

Innovation Solution

A conformal planar dipole antenna configuration with multiple layers, including a ground plane, microstrip, and dipole antenna elements embedded within a composite substrate, allowing for efficient signal propagation and reduced polarization loss through circular polarization, which is achieved by orienting dipole antenna elements at specific angles to each other.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

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

Engineering Contradiction:
ImprovebandwidthVSAvoidantenna structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The antenna is divided into multiple dipole elements arranged in a specific geometric configuration. Each dipole element contributes to the overall bandwidth by operating at different resonant frequencies, collectively providing wideband performance while maintaining individual element simplicity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The antenna employs a composite structure combining multiple dipole elements with different orientations and lengths, creating a composite antenna system that achieves wideband characteristics through the synergistic effect of individual elements rather than requiring complex single-structure designs

Inventive Principle:
Principle #40Composite materials

2Reliability

If existing dipole antennas are used, then polarization loss occurs due to sensitivity to orientation, but the antenna design is straightforward

Engineering Contradiction:
Improvepolarization lossVSAvoidantenna configuration
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The antenna uses asymmetric arrangement of dipole elements with different orientations (e.g., horizontal and vertical dipoles at specific angles). This asymmetric configuration creates circular polarization that is insensitive to receiver orientation, eliminating polarization loss while maintaining reasonable design complexity

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The antenna transitions from simple planar dipole configuration to a three-dimensional spatial arrangement of multiple dipoles oriented in different directions. This dimensional expansion allows the antenna to radiate circularly polarized waves that maintain consistent performance regardless of the receiving antenna's orientation

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

3Adaptability or versatility

If pin fed antennas are used for conformal applications, then signal loss increases through electrical vias during conformal bending, but the antenna can be mounted on curved surfaces

Engineering Contradiction:
Improveconformal mounting capabilityVSAvoidsignal loss
Core Design Contradiction:
Adaptability or versatilityVSLoss of energy

Solution Approach 1:

The design removes the problematic pin feed and electrical via structures from the conformal antenna system. Instead, it uses surface-wave excitation or direct edge coupling that eliminates the need for penetrating vias through the substrate, thereby eliminating the primary source of signal loss during conformal bending while preserving curved surface mounting capability

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The antenna introduces an intermediate coupling mechanism (such as edge coupling or surface wave excitation) that transfers energy from the feed line to the radiating elements without requiring direct through-substrate vias. This intermediary coupling method protects the signal path from the mechanical stress and discontinuities caused by conformal bending

Inventive Principle:
Principle #24Intermediary (Mediator)

4Loss of energy

If lightweight antennas are used for UAVs, then air drag is reduced for improved efficiency, but structural strength may be compromised

Engineering Contradiction:
Improveair dragVSAvoidstructural strength
Core Design Contradiction:
Loss of energyVSStrength

Solution Approach 1:

The antenna is constructed as a thin, flexible planar structure that can be conformally mounted on UAV surfaces. This thin-film construction minimizes the antenna's profile and weight, reducing air drag, while the flexible nature allows it to conform to the UAV's aerodynamic contours without requiring heavy structural support

Inventive Principle:
Principle #30Flexible shells and thin films

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 low-profile, lightweight antenna that conforms to curved surfaces with minimal signal loss and reduced air drag, maintaining efficient electrical performance regardless of conductive surfaces, and achieving circular polarization for improved signal transmission and reception.

Implementation Method 1

achieving circular polarization for improved signal transmission and reception

Methodology Applied
Scientific EffectCircular polarization: Polarisation

Implementation Method 2

efficient signal propagation and reduced polarization loss

Methodology Applied
Scientific EffectElectromagnetic signal propagation: Electromagnetic Induction

Data Source

PatentUS11018431B2Conformal planar dipole antenna
Publication Date: 2021.05.25 THE BOEING CO
  • US11018431B2 patent drawing
  • US11018431B2 patent drawing
  • US11018431B2 patent drawing

AI summary

Systems and methods for a conformal planar dipole antenna is described herein. In one example, the antenna can include a first dipole layer, a second dipole layer, a microstrip layer, and a ground plane. The first dipole layer can include a first antenna element. The second dipole layer can include a second antenna element. The microstrip layer can include a microstrip. The first antenna element, the second antenna element, and the microstrip can be electrically coupled to each other.