Wind Turbine Rotor Blade Segment Joint Design

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Solution Overview

Problem

Current joint designs for wind turbine rotor blade segments are inefficient, leading to increased assembly time due to misalignment and complex interconnecting components, which raises manufacturing, transportation, and installation costs as rotor blades grow in size.

Innovation Solution

A rotor blade assembly design featuring blade segments with a body shell, shear web, spar caps, attachment members, and spar members that diverge to securely engage and align with each other, facilitating accurate and efficient assembly by simplifying the alignment and load transfer processes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If blade segments are manufactured separately to reduce transportation and manufacturing costs, then cost is reduced, but assembly time increases due to alignment difficulties and complex interconnecting components

Engineering Contradiction:
Improvemanufacturing costVSAvoidassembly time
Core Design Contradiction:
Ease of manufactureVSLoss of time

Solution Approach 1:

The rotor blade is divided into multiple blade segments that can be manufactured separately and transported independently. Each segment includes attachment members with alignment features that enable simplified connection during assembly, resolving the contradiction between segmented manufacturing (cost reduction) and assembly complexity (time increase).

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Alignment features are pre-formed as integral parts of the attachment members during blade segment manufacturing. This preliminary action eliminates the need for complex alignment procedures during assembly, allowing segments to be quickly connected while maintaining manufacturing cost benefits.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If complex interconnecting components are used in joint designs to ensure secure connection, then connection reliability is improved, but assembly time increases due to the complexity of the components

Engineering Contradiction:
Improveconnection reliabilityVSAvoidassembly time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

Multiple functions are merged into the attachment members, which simultaneously provide structural connection, alignment, and load transfer capabilities. This integration eliminates the need for separate complex interconnecting components while maintaining connection reliability and reducing assembly time.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The attachment members are designed as multi-functional components that perform alignment, connection, and load bearing functions. This universal design reduces the number of parts needed and simplifies assembly procedures while ensuring reliable blade segment connections.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Measurement precision

If alignment features are added to attachment members to improve assembly accuracy, then alignment precision is improved, but device complexity increases

Engineering Contradiction:
Improvealignment precisionVSAvoidjoint design complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

Alignment features are merged into the attachment members as integral elements rather than separate components. This integration provides precise alignment functionality without increasing overall joint design complexity, as the alignment features are formed as part of the existing structural elements.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS7922454B1Joint design for rotor blade segments of a wind turbine
Publication Date: 2011.04.12 GE INFRASTRUCTURE TECH LLC
  • US7922454B1 patent drawing
  • US7922454B1 patent drawing
  • US7922454B1 patent drawing

AI summary

A blade segment of a rotor blade assembly formed from two or more blade segments is disclosed. The blade segment may generally include a body shell and a shear web extending longitudinally within the body shell. The shear web may be disposed between opposed spar caps. The blade segment may also include an attachment member and a spar member. The attachment member may be at least partially disposed within the body shell. The spar member may generally extend outwardly from the spar caps along an inner surface of the body shell and may be configured to support the attachment member within the body shell.