Wind Turbine Blade Insert for Retrofitting and Deflection Control

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Solution Overview

Problem

Longer wind turbine rotor blades experience increased deflection forces, leading to fatigue and the risk of striking the tower, especially in high-speed winds, due to the need for significantly longer tip extensions to accommodate loading, which are costly and inefficient.

Innovation Solution

A blade insert is coupled between pre-existing rotor blade segments, allowing for an increase in blade length without excessive elongation, using a configuration that matches the aerodynamic profile and structural components of the segments, with optional twisting and curving to optimize performance and reduce loading.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Length of moving object

If conventional tip extensions are used to increase rotor blade length, then blade span is extended, but the extension must be significantly longer than the actual increase needed, leading to prohibitively high manufacturing and transportation costs

Engineering Contradiction:
Improverotor blade spanVSAvoidmanufacturing and transportation cost
Core Design Contradiction:
Length of moving objectVSEase of manufacture

Solution Approach 1:

The rotor blade is divided into multiple segments (root segment, insert segment, tip segment) that can be manufactured separately and assembled together. This allows the blade insert to be a compact, manageable component rather than requiring an excessively long extension, reducing manufacturing complexity and transportation costs while achieving the desired span increase.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The blade insert is designed to be coupled between existing blade segments, with the insert fitting into a gap or interface between the root and tip segments. This nested arrangement allows the insert to provide the necessary length extension without requiring the entire extension structure to be as long as conventional solutions, making the component more manageable and cost-effective.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Productivity

If rotor blade length is increased, then energy output is improved, but deflection forces increase, leading to fatigue and risk of tower striking

Engineering Contradiction:
Improveenergy outputVSAvoidblade fatigue resistance
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The blade insert is designed with specific local structural characteristics at its interfaces with the root and tip segments, including matching aerodynamic profiles and structural components. This localized optimization ensures that the insert properly distributes and manages loads at the junction points, reducing stress concentrations and fatigue risks while maintaining the aerodynamic benefits of increased blade span.

Inventive Principle:
Principle #3Local quality

3Productivity

If rotor blade length is increased, then energy output is improved, but the risk of striking the tower increases

Engineering Contradiction:
Improveenergy outputVSAvoidtower strike risk
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The blade insert incorporates optional twisting and curving capabilities that allow dynamic adjustment of the blade's spatial configuration. This dynamic design feature enables the blade to optimize its aerodynamic performance for energy capture while simultaneously managing its trajectory and clearance from the tower, reducing the risk of tower strikes even at increased span lengths.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP2634418B1Blade insert for a wind turbine rotor blade and related methods
Publication Date: 2021.03.31 GENERAL ELECTRIC CO
  • EP2634418B1 patent drawingFigure 1
  • EP2634418B1 patent drawingFigure 2
  • EP2634418B1 patent drawingFigure 3

AI summary

A method for retrofitting a rotor blade 16 of a wind turbine 10 is disclosed. The method may generally include cutting the rotor blade 16 at a specified location in order to form a root segment 20 and a tip segment 22 and positioning a blade insert 106 between the root segment 20 and the tip segment 22.