Dual-Function Antenna Switching Between Phased Array and Low RCS

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Solution Overview

Problem

Aircraft antennas often reflect radar signals back towards the source, increasing detectability, and existing solutions struggle to efficiently switch between communication and low radar cross-section modes.

Innovation Solution

A dual-function antenna structure with a substrate and an array of antenna elements, coupled with a beam forming network and a controller, allows switching between a steerable phased array communication mode and a low radar cross-section (RCS) mode using controllable switches and phase shifters.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If the antenna operates in maximum power transfer mode for communication, then communication efficiency is improved, but radar cross-section increases making the aircraft more detectable

Engineering Contradiction:
Improvecommunication efficiencyVSAvoidradar detectability
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The antenna system dynamically switches between two operational modes: maximum power transfer mode for communication and low RCS mode for stealth. The controllable switches and phase shifters enable real-time reconfiguration of the antenna elements' electrical connections and signal phases, allowing the system to adapt its radiation pattern and impedance characteristics based on operational requirements.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes key electrical parameters including impedance matching (from 50 ohms for power transfer to shorted conditions for low RCS), phase relationships between elements (using controllable phase shifters), and current distribution patterns. These parameter changes transform the antenna's electromagnetic characteristics to achieve either communication efficiency or radar evasion.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If the antenna is designed for directional communication capabilities, then communication performance is improved, but the antenna structure becomes more complex

Engineering Contradiction:
Improvecommunication performanceVSAvoidantenna structure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The antenna system performs multiple functions using a single integrated structure: it provides steerable beam communication, low RCS stealth mode, and automatic radar detection. The same array of dipole elements, when reconfigured through switches and phase shifters, can function as a communication antenna with directional control or as a low-visibility structure, eliminating the need for separate antenna systems.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent combines the communication antenna function with the radar evasion function into a single integrated structure. The dipole array, feed network, switches, and phase shifters work together as one system that can alternatively provide either communication service or stealth protection, rather than requiring separate dedicated antennas for each function.

Inventive Principle:
Principle #5Merging (Combining)

3Object-affected harmful factors

If the antenna elements are spaced to provide capacitive coupling for low RCS mode, then radar cross-section is reduced, but communication efficiency decreases

Engineering Contradiction:
Improveradar cross-sectionVSAvoidcommunication efficiency
Core Design Contradiction:
Object-affected harmful factorsVSProductivity

Solution Approach 1:

The electrical coupling between antenna elements is dynamically adjusted through controllable switches. In low RCS mode, the switches configure the elements to provide capacitive coupling with specific spacing that reduces radar reflectivity. In communication mode, the switches reconfigure the same elements to provide optimal impedance matching and current distribution for efficient power transfer, transforming the coupling characteristics as needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the effective electrical parameters of the antenna elements including their impedance (from matched to shorted), phase relationships, and current magnitudes. These parameter changes allow the same physical structure with fixed element spacing to exhibit different electromagnetic behaviors - either as efficient radiating elements for communication or as coupled structures that present a low radar cross-section.

Inventive Principle:
Principle #35Parameter changes

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 system effectively reduces radar detectability by switching to a low RCS mode, while maintaining communication capabilities, thereby enhancing the stealth and operational effectiveness of aircraft.

Implementation Method 1

adjacent legs of adjacent dipole antenna elements including respective spaced apart end portions having shapes and relative positioning to provide capacitive coupling between the adjacent dipole antenna elements

Methodology Applied
Scientific EffectCapacitive coupling: Capacitance

Data Source

PatentEP4513674A1System with dual-function antenna structure and associated methods
Publication Date: 2025.02.26 EAGLE TECHNOLOGY LLC
  • EP4513674A1 patent drawingFigure 1
  • EP4513674A1 patent drawingFigure 2
  • EP4513674A1 patent drawingFigure 3

AI summary

A system to be carried by a vehicle may include a dual-function antenna structure that includes a substrate and an array of antenna elements carried thereby. A beam forming network may be coupled to the dual-function antenna structure. A radar detector to be carried by the vehicle may be configured to detect radar signals directed to the vehicle. A controller may be configured to control the dual-function antenna structure to switch between a steerable phased array communication mode and a low radar cross section (RCS) mode responsive to the radar detector.