Multi-Element Wind Turbine Blade for Low-Wind and Extreme Loads

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional wind turbine blades designed for ideal operating conditions face performance and structural challenges under non-ideal weather conditions, particularly in regions with low average wind speeds and extreme wind events like hurricanes, leading to high structural loads and catastrophic failure.

Innovation Solution

The design incorporates a multi-element airfoil configuration with reduced chord length and a cylindrical or elliptical blade body, combined with flow-enhancing components such as leading edge slats and trailing edge flaps, to optimize performance under both normal and extreme load conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If conventional airfoil design is used, then the blade structure is simple, but the blade cannot operate efficiently in low wind speed environments and is vulnerable to extreme wind events

Engineering Contradiction:
Improveoperational efficiency across varying wind conditionsVSAvoidblade structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The blade is divided into multiple functional regions: a root region with a cylindrical or elliptical cross-section optimized for structural strength, and an outboard region with a multi-element airfoil configuration optimized for aerodynamic performance. This segmentation allows each region to be optimized for its specific function while working together as an integrated system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different portions of the blade are given different structural and aerodynamic properties. The root region has a simplified cylindrical or elliptical cross-section for structural integrity, while the outboard region features a complex multi-element airfoil with slats and flaps for optimized aerodynamics in varying wind conditions.

Inventive Principle:
Principle #3Local quality

2Productivity

If high camber, high lift airfoils are used to capture energy in low wind speeds, then energy capture is improved, but structural reinforcements are required that are rarely used and add unnecessary complexity

Engineering Contradiction:
Improveenergy capture in low wind speedsVSAvoidstructural reinforcement complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The blade is divided into multiple functional regions: a root region with a cylindrical or elliptical cross-section optimized for structural strength, and an outboard region with a multi-element airfoil configuration optimized for aerodynamic performance. This segmentation allows each region to be optimized for its specific function while working together as an integrated system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The blade employs a multi-element airfoil configuration with slats and flaps that can be adjusted to optimize aerodynamic performance across varying wind conditions, replacing the need for fixed high camber designs and associated structural reinforcements.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If the blade is designed for ideal operating conditions, then aerodynamic performance is optimized, but the blade experiences catastrophic failure under extreme wind events

Engineering Contradiction:
Improveaerodynamic performanceVSAvoidstructural integrity under extreme loads
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The blade is divided into multiple functional regions: a root region with a cylindrical or elliptical cross-section optimized for structural strength, and an outboard region with a multi-element airfoil configuration optimized for aerodynamic performance. This segmentation allows each region to be optimized for its specific function while working together as an integrated system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The blade incorporates a root region with enhanced structural design (cylindrical or elliptical cross-section) that provides inherent strength and resilience against extreme wind events, cushioning the blade against catastrophic failure before such events occur.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

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 design enhances lift and reduces extreme loads, allowing wind turbines to operate efficiently in low wind speed environments while withstanding high wind events without sacrificing structural integrity.

Implementation Method 1

the rotor blades have a cross-sectional profile of an airfoil such that, during operation, air flows over the blade producing a pressure difference between the sides. Consequently, an aerodynamic lift force (also referred to as 'lift force'), which is directed from a pressure side towards a suction side, acts on the rotor blade.

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Data Source

PatentUS20250361850A1Wind turbine rotor blade with multi-element airfoil (MEA)
Publication Date: 2025.11.27 GULF WIND TECHNOLOGY
  • US20250361850A1 patent drawing
  • US20250361850A1 patent drawing
  • US20250361850A1 patent drawing

AI summary

A method of manufacturing a wind turbine rotor blade. The method includes providing a blade body having a shape that generates a lift when impacted by an incident airflow, and longitudinally extending the blade body from a root region to a tip region, through a transition region extending between and joining the root and the tip region. The root region may begin from a proximal end of the blade body, extending up to a predetermined first length of the blade body. The tip region may begin from a distal end of the blade body, extending up to a predetermined second length of the blade body. The blade body may include a predetermined structure that is fail-safe under a predetermined operating condition. The method may include providing flow enhancing components configured to enhance aerodynamic flow characteristics of the blade body, and physically coupling the flow enhancing components with the blade body.