Welded Metal Joints for Segmented Wind Turbine Blades

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Solution Overview

Problem

Current methods for joining wind turbine rotor blade segments, such as bonded and bolted joints, are complex, inefficient, and costly, requiring significant resources and maintenance, and do not effectively transfer loads from the tip to the root section.

Innovation Solution

A rotor blade assembly using composite material spar cap segments with metal joints welded together, where the metal joints are secured to the spar cap segments via resin or adhesive, and the weld area is positioned to avoid damaging the composite material, with additional features like beveled ends and filler materials to enhance joint strength and stability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If bonded joints are used to connect blade segments, then joint strength and weight efficiency are improved, but assembly complexity and environmental requirements increase

Engineering Contradiction:
Improvejoint strengthVSAvoidassembly complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent replaces bonded joints (chemical/adhesive system) with welded metal joints (mechanical/thermal system). The metal joints are secured to the composite spar cap segments through mechanical attachment and then welded together to form a continuous load-bearing structure, eliminating the need for adhesives and complex environmental controls during assembly

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

Solution Approach 2:

The patent employs a hybrid composite structure combining metal joints with composite material spar cap segments. The metal joints provide structural continuity and load transfer capability, while the composite spar cap segments maintain the aerodynamic and weight-efficient properties of the original blade design

Inventive Principle:
Principle #40Composite materials

2Ease of operation

If bolted joints are used to connect blade segments, then ease of field assembly is improved, but load transfer efficiency and structural weight increase

Engineering Contradiction:
Improveease of field assemblyVSAvoidload transfer efficiency
Core Design Contradiction:
Ease of operationVSStrength

Solution Approach 1:

The patent replaces bolted mechanical connections with welded connections between metal joints. The welding process creates a continuous metallurgical bond that provides superior load transfer efficiency compared to bolted joints, while the metal joints themselves are designed for straightforward attachment to the composite spar cap segments

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

Solution Approach 2:

The patent uses metal joints attached to composite spar cap segments to create a hybrid structure that achieves both ease of assembly and superior load transfer. The metal joints serve as intermediaries that can be easily attached to composites and then welded together for optimal structural performance

Inventive Principle:
Principle #40Composite materials

3Quantity of substance

If blade segments are manufactured separately for transport, then manufacturing and transport costs are reduced, but joint assembly complexity and maintenance requirements increase

Engineering Contradiction:
Improvetransport efficiencyVSAvoidjoint assembly complexity
Core Design Contradiction:
Quantity of substanceVSDevice complexity

Solution Approach 1:

The patent divides the rotor blade into multiple transportable segments that can be manufactured separately and assembled in the field. Each segment includes spar cap segments with attached metal joints, designed for efficient transport and streamlined assembly through welding

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent replaces complex bonded or bolted joint assemblies with welded metal joints, simplifying the field assembly process for segmented blades. The welding process creates permanent, maintenance-free connections that eliminate the need for long-term monitoring and maintenance of joint systems

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

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 solution simplifies the assembly of rotor blade segments, enhances load transfer efficiency, and reduces maintenance needs while maintaining structural integrity and energy efficiency, thereby lowering the costs associated with larger wind turbines.

Implementation Method 1

the first and second metal joints are welded together at a weld area

Methodology Applied
Scientific EffectWelding: Welding

Implementation Method 2

the metal joints are secured to the spar cap segments via resin or adhesive

Methodology Applied
Scientific EffectAdhesive bonding: Adhesive

Data Source

PatentUS10605227B2Segmented wind turbine rotor blade with welded joint
Publication Date: 2020.03.31 GE INFRASTRUCTURE TECH LLC
  • US10605227B2 patent drawing
  • US10605227B2 patent drawing
  • US10605227B2 patent drawing

AI summary

The present disclosure is directed to a rotor blade assembly for a wind turbine having a first rotor blade segment with a first spar cap segment and a second rotor blade segment with a second spar cap segment. The first and second spar cap segments are arranged together at an interface and are constructed of a composite material. Further, the rotor blade assembly includes a joint assembly at the interface of the first and second spar cap segments. The joint assembly is constructed of a first metal joint secured to the first spar cap segment and a second metal joint secured to second spar cap segment. Moreover, the first and second metal joints are welded together at a weld area.