Trailing Edge Bonding Cap for Wind Turbine Blades

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Solution Overview

Problem

Conventional adhesive bonding methods for wind turbine rotor blades result in reduced aerodynamic efficiency, increased noise, and susceptibility to erosion at the trailing edge due to adhesive thickness and application challenges.

Innovation Solution

A trailing edge bonding cap formed from a metal matrix composite material, such as an aluminum alloy with carbon or boron fibers, is used to project outwardly from the blade shell, providing a sharp or cusp trailing edge that matches the aerodynamic profile, enhancing structural integrity and reducing noise.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If adhesive bonding is used to combine shell components, then the blade shell can be manufactured from separate components, but the trailing edge thickness increases reducing aerodynamic efficiency

Engineering Contradiction:
Improvemanufacturability of blade shellVSAvoidtrailing edge thickness tolerance
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

A bonding cap is introduced as an intermediary component between the shell components. The bonding cap provides a precise trailing edge geometry and serves as the bonding substrate, eliminating the need for thick adhesive layers while maintaining the benefit of assembling from separate shell components.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The invention changes the bonding configuration by replacing a thick adhesive bond line with a thin bonding cap. This parameter change in bonding structure thickness directly addresses the trailing edge thickness issue while preserving manufacturability through component assembly.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If adhesive bonding is used to combine shell components, then the blade shell can be assembled from separate parts, but aerodynamic efficiency is reduced due to increased trailing edge thickness

Engineering Contradiction:
Improveassembly of shell componentsVSAvoidaerodynamic efficiency
Core Design Contradiction:
Ease of manufactureVSLoss of energy

Solution Approach 1:

The bonding cap acts as a mediator that enables component assembly while maintaining aerodynamic efficiency. It provides the necessary bonding function with minimal thickness, allowing separate shell components to be assembled without the aerodynamic penalties of thick adhesive layers.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of manufacture

If adhesive bonding is used to combine shell components, then the blade shell can be constructed from multiple components, but noise generation increases due to trailing edge thickness

Engineering Contradiction:
Improvemodular construction of bladeVSAvoidpure tone noise
Core Design Contradiction:
Ease of manufactureVSObject-generated harmful factors

Solution Approach 1:

The bonding cap serves as an intermediary that enables modular construction while eliminating noise generation. By providing a thin, precise trailing edge geometry, it allows modular assembly from separate components without creating the thick trailing edge that generates pure tone noise.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Ease of manufacture

If adhesive bonding is used to combine shell components, then the blade shell can be assembled from separate components, but erosion resistance decreases at the trailing edge

Engineering Contradiction:
Improvecomponent-based manufacturingVSAvoidbond strength against erosion
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The bonding cap serves as a protective intermediary at the trailing edge. It provides erosion resistance while enabling component-based manufacturing, as the cap itself can be made from erosion-resistant materials and protects the adhesive bond line from direct exposure to erosive environments.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The bonding cap can be constructed from composite materials that combine erosion resistance with bonding capability. This allows the trailing edge to withstand erosive conditions while maintaining the structural integrity of the component assembly.

Inventive Principle:
Principle #40Composite materials

5Manufacturing precision

If adhesive is applied in controlled amounts, then precise trailing edge thickness can be achieved, but application difficulty increases

Engineering Contradiction:
Improvetrailing edge thickness controlVSAvoidadhesive application process
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The bonding cap serves as a pre-formed intermediary that eliminates the need for precise adhesive application. The cap itself provides the precise trailing edge geometry, transferring the precision requirement from the adhesive application process to the cap manufacturing process, which is easier to control.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 improves aerodynamic efficiency by increasing the lift-to-drag ratio, reduces noise generation, and enhances structural integrity, preventing buckling and erosion while serving as an effective lightning conductor.

Implementation Method 1

The body may be formed from a metal matrix composite material

Methodology Applied
Scientific EffectComposite materials: Composite Materials

Data Source

PatentUS8043066B2Trailing edge bonding cap for wind turbine rotor blades
Publication Date: 2011.10.25 GE INFRASTRUCTURE TECH LLC
  • US8043066B2 patent drawing
  • US8043066B2 patent drawing
  • US8043066B2 patent drawing

AI summary

A trailing edge bonding cap for use with a rotor blade of a wind turbine is disclosed. The trailing edge bonding cap may include a body projecting outwardly from a blade shell of the rotor blade. The body may have a first outer surface and a second outer surface. The first outer surface may intersect the second outer surface to define a trailing edge of the rotor blade. Additionally, the first and second outer surfaces may have a profile configured to correspond to an aerodynamic profile of the blade shell.