Satellite Diversity Antenna System with Adjustable Elevation Angles

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Solution Overview

Problem

Current satellite diversity antenna systems for vehicles face challenges in achieving higher gains for satellite signal reception while maintaining vehicle aesthetics and simplicity in design and installation, particularly for satellite digital audio radio services (SDARS) operating in the 2320-2345 MHz frequency band.

Innovation Solution

The proposed antenna system employs two patch antennas with adjustable elevation angles and a ground plane, optimized for maximum gain, which can be fixed or adjustable, and incorporates diversity switching electronics to enhance signal reception and reduce design complexities, maintaining a visually appealing 'hidden antenna' design.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If SDARS patch antennas are mounted on the vehicle exterior (roof) to achieve proper reception, then signal reception is improved, but vehicle aesthetics are compromised

Engineering Contradiction:
Improvesignal receptionVSAvoidvehicle aesthetics
Core Design Contradiction:
ReliabilityVSShape

Solution Approach 1:

The antenna elements are nested within a radome that is integrated into the vehicle body, concealing the antenna structure while maintaining reception functionality. The radome acts as a protective cover that hides the antenna elements from external view, allowing the antenna to be 'hidden' within the vehicle structure rather than mounted externally.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Reliability

If multiple antennas are positioned at different locations with phase array summation to achieve higher gains, then antenna performance is improved, but design and installation complexities increase

Engineering Contradiction:
Improveantenna performanceVSAvoiddesign and installation complexities
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Multiple antenna elements are combined within a single integrated module structure, sharing common support, grounding, and control systems. This merging approach achieves the performance benefits of multiple antennas while reducing overall system complexity compared to separate antenna installations.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The antenna system is segmented into modular elements that can be independently optimized but are integrated into a unified structure. Each antenna element within the module can be independently positioned and tuned, allowing performance optimization without requiring complex external installation of multiple separate antenna systems.

Inventive Principle:
Principle #1Segmentation

3Reliability

If two or more antennas are positioned at different locations in a switched diversity application, then signal reception reliability is improved, but gain of the received satellite signal is not increased

Engineering Contradiction:
Improvesignal receptionVSAvoidgain of received signal
Core Design Contradiction:
ReliabilityVSPower

Solution Approach 1:

Multiple antenna elements are combined with their outputs fed to a common receiver through a diversity switch. This merging of multiple antenna paths allows the system to achieve both diversity reliability and signal gain by combining the electromagnetic energy from multiple elements while maintaining the ability to switch between them.

Inventive Principle:
Principle #5Merging (Combining)

4Shape

If hidden antenna application is used to maintain vehicle aesthetics, then vehicle appearance is improved, but reception performance is compromised

Engineering Contradiction:
Improvevehicle appearanceVSAvoidreception performance
Core Design Contradiction:
ShapeVSReliability

Solution Approach 1:

The antenna elements are nested within a radome integrated into the vehicle body surface, concealing them from external view. The radome is designed to be aesthetically pleasing and blend with the vehicle appearance while providing the necessary electromagnetic transparency for signal reception.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The radome material and structure are specifically designed with local electromagnetic properties that allow satellite signal penetration while maintaining aesthetic appearance from external viewing angles. The local quality of the radome material enables it to be transparent to satellite frequencies while appearing solid and aesthetic from ground level.

Inventive Principle:
Principle #3Local quality

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

This configuration increases average and minimum gain values by more than 2.0dB over conventional designs, providing improved satellite signal reception while maintaining vehicle aesthetics and simplifying installation, and can be adjusted for optimal performance across different geographic locations.

Implementation Method 1

antennas that receive and process signals other than traditional AM/FM signals, such as, for example, satellite signals

Methodology Applied
Scientific EffectElectromagnetic radiation reception: Electromagnetic Induction

Implementation Method 2

two patch antennas with adjustable elevation angles and a ground plane, optimized for maximum gain

Methodology Applied
Scientific EffectElectromagnetic reflection: Reflection

Data Source

PatentEP1744470B1Satellite diversity antenna system
Publication Date: 2017.10.11 DELPHI TECHNOLOGIES INC
  • EP1744470B1 patent drawingFigure 1A~1C
  • EP1744470B1 patent drawingFigure 2A
  • EP1744470B1 patent drawingFigure 2B

AI summary

A satellite antenna module (12a-12c) is disclosed. The satellite antenna module (12a-12c)includes at least one antenna element (14a-14c, 16a-16c) disposed on a ground plane (18a-18c). The ground plane (18a-18c) is capacitivly coupled to a vehicle surface (22a-22c). The ground plane (18a-18c) is disposed over the vehicle surface (22a-22c) at an elevation angle (θ1-θ4, Δ1, Δ2) that achieves a higher gain of the at least one antenna element (14a-14c, 16a-16c).