Specular Conductive Path Deicing Structure for Radar Stealth

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Solution Overview

Problem

Electro-thermal deicing systems with metallic heating elements increase the radar cross-section of structures, making them more vulnerable to enemy radar detection, which is a concern for military applications where stealthiness is crucial.

Innovation Solution

The use of conductive paths arranged in a specular pattern on the surface of structures to reduce radar cross-section, combined with a control unit to manage heating energy and create varying radar signatures by selectively applying electrical energy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If metallic heating elements are used for electro-thermal deicing, then deicing effectiveness is improved, but radar cross-section increases making the structure more detectable

Engineering Contradiction:
Improvedeicing effectivenessVSAvoidradar detectability
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The continuous metallic heating element is segmented into discrete conductive paths arranged in a specular pattern. This segmentation breaks up the continuous reflective surface that causes high radar cross-section, while maintaining the distributed heating function across the airfoil surface.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The heating element pattern transitions from symmetric or random circuit traces to an asymmetric specular pattern specifically designed to reflect radar waves away from the source. The asymmetric geometry optimizes radar wave deflection while maintaining heating effectiveness.

Inventive Principle:
Principle #4Asymmetry

2Ease of manufacture

If conventional circuit patterns are used for heating elements, then manufacturing simplicity is maintained, but radar cross-section becomes excessively large

Engineering Contradiction:
Improveheating element fabricationVSAvoidradar cross-section
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The design parameters of the heating element are changed from conventional circuit trace geometry to specular pattern geometry. This parameter change optimizes the electromagnetic reflection properties while maintaining compatibility with standard manufacturing processes for applying conductive materials to airfoil surfaces.

Inventive Principle:
Principle #35Parameter changes

3Object-affected harmful factors

If conductive material is applied to reduce radar cross-section, then stealthiness is improved, but deicing functionality must be maintained

Engineering Contradiction:
Improveradar reflectivityVSAvoiddeicing capability
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The conductive material pattern serves dual functions: it provides the necessary heating capability for deicing while simultaneously functioning as a radar reflection control surface. The same specular pattern that reduces radar cross-section also distributes electrical current for effective heating, combining two functions in one structure.

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

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 specular pattern design enhances electromagnetic energy absorption and interference, reducing the structure's radar reflectivity and allowing it to remain stealthy by minimizing returned radar signals, effectively reducing the structure's detectability.

Implementation Method 1

The specular pattern design enhances electromagnetic energy absorption and interference, reducing the structure's radar reflectivity

Methodology Applied
Scientific EffectElectromagnetic absorption: Absorption (EM radiation)

Implementation Method 2

The specular pattern design enhances electromagnetic energy absorption and interference, reducing the structure's radar reflectivity

Methodology Applied
Scientific EffectElectromagnetic interference: Interference

Implementation Method 3

a plurality of conductive paths arranged in a specular pattern to reduce the radar cross section of the structure

Methodology Applied
Scientific EffectSpecular reflection: Reflection

Implementation Method 4

heat energy is typically applied to the surface of the airfoil or structure through a metallic heating element via electrical power supplied by the aircraft or appropriate application generators

Methodology Applied
Scientific EffectJoule heating: Joule Heating

Data Source

PatentUS7633450B2Radar altering structure using specular patterns of conductive material
Publication Date: 2009.12.15 GOODRICH CORP
  • US7633450B2 patent drawing
  • US7633450B2 patent drawing
  • US7633450B2 patent drawing

AI summary

A radar altering structure comprises: a structure; and at least one layer of conductive material disposed at at least one surface of the structure, the layer comprising a plurality of conductive paths arranged in a specular pattern to reduce the radar cross section of the structure.