Wind Turbine Blade Conductive Layer Radar Signature Reduction

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Solution Overview

Problem

The co-location of wind turbines and electromagnetic radiation systems, such as radar stations, leads to disruptions due to the Doppler effect caused by wind turbine blades, making it difficult for radar systems to accurately differentiate between static and moving objects, and existing solutions like upgrading radar systems or modifying turbine blades are limited in effectiveness.

Innovation Solution

Incorporating a conductive layer into wind turbine blades, such as a woven or stitched fabric structure with a conductive layer on its surface, to reduce the radar cross-section (RCS) by at least 20 dB compared to conventional blades, without degrading mechanical performance or altering the blade profile.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If a conductive layer is added to the turbine blade to reduce radar cross-section, then the radar signature is reduced by at least 20 dB, but the device complexity and manufacturing complexity increase

Engineering Contradiction:
Improveradar signatureVSAvoidblade structure complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The patent applies composite materials by integrating a conductive layer (such as carbon fiber, metallic coating, or conductive polymer) into the turbine blade structure. This composite construction allows the blade to maintain its aerodynamic function while simultaneously reducing radar cross-section by at least 20 dB through the electromagnetic properties of the conductive material.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent changes the electromagnetic parameters of the blade by incorporating materials with specific electrical conductivity properties. The conductive layer alters the blade's interaction with radar waves, transforming it from a radar-reflective surface to a radar-absorbing or radar-scattering-reducing structure, achieving the required 20 dB reduction in radar signature.

Inventive Principle:
Principle #35Parameter changes

2Object-affected harmful factors

If the profile of the turbine blade is modified to minimize radar cross-section, then the radar signature is reduced, but the wind energy capturing capability is compromised

Engineering Contradiction:
Improveradar signatureVSAvoidwind energy capture
Core Design Contradiction:
Object-affected harmful factorsVSUse of energy by moving object

Solution Approach 1:

The patent applies local quality by modifying only specific portions of the blade (such as the leading edge, trailing edge, or specific sections) with conductive materials rather than altering the entire blade profile. This localized approach reduces radar cross-section while preserving the overall aerodynamic shape and wind energy capturing capability of the blade.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent uses composite materials to combine the aerodynamic surface with conductive layers in a way that maintains both functions. The conductive layer is integrated into the blade structure without disrupting the aerodynamic profile, allowing the blade to capture wind energy effectively while simultaneously reducing radar signature.

Inventive Principle:
Principle #40Composite materials

3Ease of manufacture

If conventional fiber lay-up techniques are used to incorporate novel materials, then the manufacturing process remains simple, but the ability to incorporate conductive materials is limited

Engineering Contradiction:
Improvemanufacturing process simplicityVSAvoidmaterial incorporation capability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent extends conventional fiber lay-up techniques to incorporate conductive materials by treating them as additional reinforcement layers. Conductive fibers (such as carbon fiber) or conductive coatings are applied using existing composite manufacturing processes like wet lay-up, resin transfer molding (RTM), or vacuum-assisted resin transfer molding (VARTM), maintaining manufacturing simplicity while expanding material versatility.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent makes conventional manufacturing processes multi-functional by enabling them to produce both structural and electromagnetic-functional components. The same fiber lay-up techniques that create the blade's structural integrity also incorporate conductive materials that provide radar signature reduction, eliminating the need for separate manufacturing processes.

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 conductive layer significantly reduces the radar signature of wind turbine blades, improving the accuracy of nearby electromagnetic signaling systems by minimizing interference, with a 20 dB reduction in RCS achieved across various frequency ranges.

Implementation Method 1

Inclusion of the conductive layer in the wind turbine blade can cause a reduction in radar signature of the wind turbine blade to be reduced by at least 20 dB

Methodology Applied
Scientific EffectElectromagnetic radiation absorption: Absorption (EM radiation)

Implementation Method 2

motion of blade(s) 1130 can engender a Doppler effect in reflected waves 1160, which are generated by reflection of the electromagnetic waves 1110 by blade(s) 1130

Methodology Applied
Scientific EffectDoppler effect: Doppler Effect

Data Source

PatentUS9404371B1Reduction of radar cross-section of a wind turbine
Publication Date: 2016.08.02 NATIONAL TECHNOLOGY & ENGINEERING SOLUTIONS OF SANDIA LLC
  • US9404371B1 patent drawing
  • US9404371B1 patent drawing
  • US9404371B1 patent drawing

AI summary

The various technologies presented herein relate to formation of a wind turbine blade having a reduced radar signature in comparison with a turbine blade fabricated using conventional techniques. Various techniques and materials are presented to facilitate reduction in radar signature of a wind turbine blade, where such techniques and materials are amenable for incorporation into existing manufacturing techniques without degradation in mechanical or physical performance of the blade or major alteration of the blade profile.