Radome Plasma Shutter for Radar Signature Reduction

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Solution Overview

Problem

Radomes on military aircraft suffer from high radar signatures due to electromagnetic transparency, which allows undesirable electromagnetic waves to interfere with antennas, and existing solutions compromise structural strength or introduce additional scattering centers.

Innovation Solution

A radome with a sandwich structure incorporating a plasma-guiding layer within a honeycomb core and high-frequency transparent electrodes, which integrates the plasma shutter into the radome's primary structure, ensuring structural integrity and homogeneous electromagnetic fields.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a radome is made electromagnetically transparent to allow antenna operation, then the antenna can function properly, but the radar signature increases due to reflections from the radome interior

Engineering Contradiction:
Improveantenna operationVSAvoidradar signature
Core Design Contradiction:
Ease of operationVSObject-generated harmful factors

Solution Approach 1:

The radome employs a plasma layer that can dynamically change its electromagnetic properties between transparent and reflective states. The plasma density is controlled by electrode discharge, allowing the radome to adapt its transparency level based on operational requirements, thus resolving the contradiction between antenna operation and radar signature reduction

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention changes the electromagnetic parameters of the radome by introducing a plasma layer with variable electron density. By adjusting the plasma density through controlled discharge, the radome's electromagnetic transparency is modulated, enabling it to switch between transparent state (for antenna operation) and reflective state (for radar signature reduction)

Inventive Principle:
Principle #35Parameter changes

2Object-generated harmful factors

If mechanical shutter systems are used to block electromagnetic waves, then the radar signature is reduced, but the structural strength of the radome is compromised

Engineering Contradiction:
Improveradar signatureVSAvoidradome structural strength
Core Design Contradiction:
Object-generated harmful factorsVSStrength

Solution Approach 1:

The invention replaces mechanical shutter systems with a plasma-based electromagnetic shielding mechanism. The plasma layer, generated and controlled by electrodes, provides the shielding function without requiring any moving mechanical parts, thus maintaining the radome's structural integrity while achieving radar signature reduction

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 effectively shields antennas from undesirable radiation without weakening the radome structure or creating additional scattering centers, maintaining radar signature camouflage and improving electromagnetic field homogeneity.

Implementation Method 1

A plasma layer is electrically conductive, and a sufficiently high electrical conductivity for the reflection or damping of electromagnetic waves can be achieved depending on the charge density in the plasma

Methodology Applied
Scientific EffectPlasma: Plasma

Implementation Method 2

The desired switching action can be achieved by switching the plasma on and off

Methodology Applied
Scientific EffectElectrical discharge: Electric Spark

Data Source

PatentUS8159407B2Radome with integrated plasma shutter
Publication Date: 2012.04.17 AIRBUS DEFENCE & SPACE GMBH
  • US8159407B2 patent drawing
  • US8159407B2 patent drawing
  • US8159407B2 patent drawing

AI summary

Radome with an integrated plasma shutter covering an antenna and method for selectively shielding an antenna. The radome includes a honeycomb core formed to contain a plasma-guiding layer, and coverplates arranged to sandwich the honeycomb core. Electrodes are structured and arranged for plasma excitation, the electrodes being high frequency (HF)—transparent at least in an operating frequency range of the antenna. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.