Wind Turbine Rotor Blade Joint Gap Adhesive Bonding

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Solution Overview

Problem

The existing methods for manufacturing rotor blades for wind turbines are time-consuming and inefficient due to the use of slow-hardening adhesives and the need for external pressure during bonding, which leads to mechanical stresses and increased processing times.

Innovation Solution

A method where highly viscous adhesive is introduced directly into a joint gap between rotor blade elements, allowing for rapid curing and eliminating the need for external pressure, using sensors to detect adhesive filling and automation for precise adhesive introduction, enabling the use of adhesives with short pot life and reducing mechanical stresses.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If adhesive is applied to large areas of rotor blade elements, then bonding strength is improved, but processing time increases significantly

Engineering Contradiction:
Improvebonding strengthVSAvoidprocessing time
Core Design Contradiction:
StrengthVSLoss of time

Solution Approach 1:

The invention extracts the adhesive from the traditional large-area application method and concentrates it into a precisely controlled joint gap between rotor blade elements. This is achieved through positioning devices that create a defined gap and adhesive introduction devices that deliver adhesive only where needed, eliminating the time-consuming large-area application while maintaining bonding strength through concentrated adhesive placement.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention applies local quality by concentrating the adhesive in a specific localized region (the joint gap) rather than distributing it over large areas. The positioning devices and adhesive introduction devices ensure that adhesive is placed precisely where required for bonding, with controlled quantity and distribution, achieving effective bonding with minimal adhesive and reduced processing time.

Inventive Principle:
Principle #3Local quality

2Manufacturing precision

If external pressure is applied during bonding, then adhesive distribution is improved, but mechanical stresses in the rotor blade increase

Engineering Contradiction:
Improveadhesive distributionVSAvoidmechanical stresses
Core Design Contradiction:
Manufacturing precisionVSStress or pressure

Solution Approach 1:

The invention replaces the mechanical pressure application system with a positioning-based system. Instead of using external pressure devices to distribute adhesive, the invention uses positioning devices to create a defined joint gap and adhesive introduction devices to deliver adhesive precisely into this gap. The adhesive's own viscosity and flow properties, combined with the controlled gap dimensions, achieve proper distribution without external pressure, thereby eliminating the mechanical stresses that would result from pressure application.

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

Solution Approach 2:

The invention changes the key parameter from applied pressure to gap dimension control. By precisely controlling the joint gap size through positioning devices and adjusting adhesive introduction parameters (flow rate, viscosity, temperature), the invention achieves proper adhesive distribution without the need for external pressure, thus avoiding the generation of mechanical stresses in the rotor blade.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If slow-hardening adhesives are used, then processing time is extended, but bonding reliability is improved

Engineering Contradiction:
Improvebonding reliabilityVSAvoidmanufacturing efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The invention introduces feedback mechanisms through sensors that detect the adhesive filling level in the joint gap in real-time. This feedback allows for precise control of the adhesive introduction process, ensuring optimal adhesive distribution and bonding quality. The feedback system enables the use of fast-hardening adhesives by providing real-time information about adhesive placement, allowing operators to make immediate adjustments to achieve reliable bonds before the adhesive sets, thereby maintaining bonding reliability while improving manufacturing efficiency.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The invention performs preliminary actions by precisely positioning the rotor blade elements to create the optimal joint gap before adhesive introduction. The positioning devices pre-establish the correct geometry and alignment, and the adhesive introduction devices are pre-positioned to deliver adhesive exactly where needed. This preliminary preparation enables the use of fast-hardening adhesives by ensuring optimal bonding conditions are already in place, achieving reliable bonds quickly without the need for slow-hardening materials.

Inventive Principle:
Principle #10Preliminary action

4Ease of manufacture

If adhesive is pressed out of the joint gap, then adhesive application is simplified, but material waste increases

Engineering Contradiction:
Improveadhesive application simplicityVSAvoidadhesive waste
Core Design Contradiction:
Ease of manufactureVSLoss of substance

Solution Approach 1:

The invention extracts the excess adhesive that would normally be pressed out of the joint gap and eliminates it through precise control of the adhesive introduction process. The positioning devices create a defined joint gap with specific dimensions, and the adhesive introduction devices are controlled to deliver exactly the right amount of adhesive needed to fill this gap. This extraction of the excess adhesive elimination approach maintains ease of manufacture through automated controlled application while significantly reducing material waste.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention enables the adhesive application system to serve itself by using the joint gap dimensions and adhesive properties to automatically control the adhesive distribution. The positioning devices establish the gap that defines the adhesive quantity needed, and the controlled introduction process allows the adhesive to self-distribute within the gap boundaries without requiring external pressure to force it out. This self-service mechanism simplifies the application process while preventing material waste through precise quantity control.

Inventive Principle:
Principle #25Self-service

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

This method significantly reduces processing time, eliminates the need for post-processing annealing, and minimizes adhesive waste, while ensuring a strong and reliable bond, thereby enhancing the efficiency and quality of rotor blade manufacturing.

Implementation Method 1

adhesive being introduced into the joint gap to join the first rotor blade element and the second rotor blade element, the degree of adhesive filling in the joint gap being detected by means of a sensor

Methodology Applied
Scientific EffectAdhesive: Adhesive

Data Source

PatentEP2627899B1Manufacture of a rotor blade for a wind turbine
Publication Date: 2016.08.17 SENVION GMBH
  • EP2627899B1 patent drawingFigure 1~2
  • EP2627899B1 patent drawingFigure 3a~3b
  • EP2627899B1 patent drawingFigure 4~5b

AI summary

The invention relates to a method for manufacturing a rotor blade (5) for a wind turbine (1) from at least a first rotor blade element (11, 11', 12, 12') and a second rotor blade element (11, 11', 12, 12'). In a further development of the method according to the invention the first rotor blade element (11, 11', 12, 12') and the second rotor blade element (11, 11', 12, 12') are positioned in the desired relative arrangement with respect to one another, such that a joint gap (13) remains between the first rotor blade element (11, 11', 12, 12') and the second rotor blade element (11, 11', 12, 12'), wherein adhesive is introduced into the joint gap (13) for joining the first rotor blade element (11, 11', 12, 12') and the second rotor blade element (11, 11', 12, 12'). The invention further relates to a manufacturing unit for manufacturing a rotor blade (5) by the method according to the invention. The invention also relates to a rotor blade (5) manufactured accordingly and to a wind turbine (1) having a rotor blade (5) according to the invention.