Conformal UAV Patch Antenna Using Magneto-Dielectric Stack-Up
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Conventional patch antennas on UAVs have narrow bandwidth and low gain characteristics, which can be improved by increasing thickness, but this results in larger size and weight, affecting flight performance and requiring non-conformal mounting, impacting aerodynamics and radar detection.
Innovation Solution
A conformal patch antenna design using a stack-up of dielectric materials, including a magneto-dielectric substrate, to achieve wide bandwidth and high gain while maintaining a small size, integrated into the UAV fuselage with a recess to minimize size and weight impact.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If the thickness of the patch antenna is increased to improve bandwidth and gain characteristics, then the bandwidth and gain are improved, but the antenna size and weight increase
Solution Approach 1:
The patent employs a composite stack-up structure consisting of multiple dielectric layers with different properties. Specifically, it uses a low-loss dielectric substrate, a magneto-dielectric layer, and a ground plane layer, where each layer contributes different electromagnetic characteristics. This composite structure enables enhanced bandwidth and gain without requiring a single thick layer, thus avoiding the weight penalty of a monolithic thick antenna while achieving superior performance through material composition.
2Reliability
If the thickness of the patch antenna is increased to improve bandwidth and gain characteristics, then the bandwidth and gain are improved, but the antenna size increases
Solution Approach 1:
The patent transitions from a conventional single-layer thick antenna design to a multi-layer stacked configuration. By distributing the functional requirements across multiple thin layers in the vertical dimension, the design achieves equivalent or superior electromagnetic performance without increasing the overall thickness. The stack-up approach uses interfaces between different dielectric layers to create resonant structures that provide broad bandwidth and high gain while maintaining a compact profile suitable for conformal mounting on UAV surfaces.
3Ease of operation
If the patch antenna is mounted on the outer surface of the UAV fuselage to maintain conformality, then the aerodynamic performance is maintained, but the antenna bandwidth and gain are reduced
Solution Approach 1:
The patent uses a composite multi-layer dielectric structure that can be fabricated as a thin, flexible conformal layer that adheres to the UAV fuselage surface. This composite stack-up includes a magneto-dielectric layer combined with low-loss dielectric materials, creating a structure that maintains conformality for aerodynamic performance while the specific material composition and layering provide enhanced bandwidth and gain characteristics compared to conventional single-layer conformal antennas.
4Reliability
If a thick patch antenna extends past the outer surface of the fuselage to achieve better performance, then the bandwidth and gain are improved, but the flight performance is negatively impacted
Solution Approach 1:
The patent resolves the conflict between antenna performance and flight performance by using a multi-layer stacked configuration that achieves broad bandwidth and high gain within a thin profile. The dimensionality change from a single thick layer to multiple thin layers allows the antenna to maintain conformality with the fuselage surface, avoiding aerodynamic penalties while achieving superior electromagnetic performance through the engineered stack-up of different dielectric and magneto-dielectric materials.
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 conformal patch antenna achieves broad bandwidth and high gain in the UHF or VHF range with a reduced size and weight, enhancing communication range and reducing radar detection, without compromising flight performance.
Implementation Method 1
an intermediate substrate provided from a magneto-dielectric material disposed between the first substrate and the bottom substrate
Implementation Method 2
The stack-up comprises a first substrate, a patch conductor disposed on a surface of the first substrate
Data Source
AI summary
Embodiments of the present disclosure relate to a UAV comprising a fuselage, a rotor, and a patch antenna element. The patch antenna element, which is provided from a patch antenna stack-up, is conformally disposed on an outer surface of the UAV's fuselage. The patch antenna comprises a first substrate, patch conductor, intermediate substrate, bottom substrate, and ground plane. The patch conductor is disposed on a top surface of the first substrate. A first surface of the intermediate substrate, which is a magneto-dielectric material, is disposed on a bottom surface of the first substrate. A top surface of the bottom substrate is disposed on a second surface of the intermediate substrate. A ground plane conductor is disposed on a bottom surface of the bottom substrate.


