Modular Wind Turbine Blade Scarf Joint Alignment

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The challenge in modular wind turbine blades is ensuring precise alignment and achieving a consistent bond thickness between modules, which affects the strength and structural performance of the blade, especially when assembling large modules in remote and difficult-to-access locations.

Innovation Solution

The method involves using blade modules with tapered spar cap sections connected via an adhesively bonded scarf joint, where a separating layer is strategically placed to control the bond thickness, ensuring precise alignment and a strong joint without complex alignment tooling, and using a moulding process to form the modules with a separating layer that defines the bond gap, allowing for consistent and strong bonding.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If blade modules are assembled in the field at remote locations, then transportation difficulty is reduced, but alignment precision deteriorates

Engineering Contradiction:
Improveassembly location accessibilityVSAvoidblade module alignment precision
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

Alignment features (guide rails, positioning pins, tapered surfaces) are pre-integrated into the blade module structures during manufacturing. This preliminary preparation enables precise alignment to be achieved during field assembly without requiring complex alignment tooling or skilled operations, thus resolving the contradiction between assembly accessibility and alignment precision

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

Alignment features act as intermediary elements between blade modules during assembly. These features (guide rails, positioning pins, tapered surfaces) mediate the alignment process by providing physical references and constraints that ensure precise relative positioning of modules in the field, eliminating the need for complex measurement and adjustment procedures

Inventive Principle:
Principle #24Intermediary (Mediator)

2Manufacturing precision

If complex alignment tooling is used to ensure precise alignment, then alignment precision improves, but device complexity increases

Engineering Contradiction:
Improveblade module alignment precisionVSAvoidalignment tooling complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The blade modules are designed to be self-aligning through integrated alignment features such as guide rails, positioning pins, and tapered surfaces. These features enable the modules to align themselves during assembly without requiring external alignment tooling or complex adjustment procedures, thus achieving high alignment precision while minimizing device complexity

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The alignment function is extracted from the assembly process and embedded directly into the blade module structures. Instead of using separate alignment tools and procedures, the alignment capabilities are built into the modules themselves through features like guide rails and positioning pins, eliminating the need for complex external alignment equipment

Inventive Principle:
Principle #2Taking out (Extraction)

3Ease of manufacture

If bond thickness is not controlled, then assembly process simplicity is maintained, but bond strength deteriorates

Engineering Contradiction:
Improveassembly process simplicityVSAvoidbonded joint strength
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

A separating layer is introduced as an intermediary element between the blade modules during assembly. This layer acts as a spacer that controls the bond thickness of the adhesive joint, ensuring consistent and appropriate adhesive distribution while maintaining assembly simplicity. The separating layer is removed after bonding, leaving a controlled bond line

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The required bond thickness is predetermined and built into the assembly process through the use of a separating layer with a specific thickness. This preliminary determination of bond thickness eliminates the need for complex thickness control procedures during assembly, while ensuring the bonded joint achieves the required strength

Inventive Principle:
Principle #10Preliminary action

4Ease of operation

If modular design is implemented, then transportation ease improves, but joint strength deteriorates

Engineering Contradiction:
Improvecomponent transportation easeVSAvoidjoint region strength
Core Design Contradiction:
Ease of operationVSStrength

Solution Approach 1:

Tapered surfaces with curved profiles are used at the bonding interfaces of the modular blade sections. These tapered geometries provide large bonding areas and facilitate stress distribution across the joint regions, enhancing joint strength while maintaining the modular design that enables easy transportation

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

Multiple bonding methods are combined in the modular joint design, including adhesive bonding, mechanical interlocking through tapered surfaces, and structural integration of alignment features. This combination of bonding approaches ensures high joint strength while maintaining the modular configuration for easy transportation and assembly

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS11396154B2Modular wind turbine blade and associated method of manufacture
Publication Date: 2022.07.26 VESTAS WIND SYSTEMS AS
  • US11396154B2 patent drawing
  • US11396154B2 patent drawing
  • US11396154B2 patent drawing

AI summary

A method of making a modular wind turbine blade is described. The modular blade comprises first and second blade modules connected together by a scarf joint between tapered spar caps of the respective blade modules. According to the method, first and second blade modules are laid up in the same mould assembly. A separating layer is arranged between the layups of the first and second module in a joint region of the mould. The separating layer has a thickness corresponding to a required bond thickness in the scarf joint when the modules are bonded together.