Vortex Propeller Blade Design for Wind Turbine Efficiency

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Solution Overview

Problem

Traditional wind turbine propeller designs face inefficiencies due to compromises in aerodynamic and structural optimization, leading to suboptimal power capture and increased costs, with limitations in handling varying wind speeds and turbulence, and inefficiencies in blade design such as narrow blades, high drag, and reduced lift/drag ratios.

Innovation Solution

A propeller device with blades configured to approximate the shape of a vortex, featuring a spiral design along a central axis, optimizing fluid flow and angle of attack, and allowing for adjustable blade spacing to accommodate varying wind conditions, thereby enhancing lift and reducing drag.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If traditional wind turbine propeller designs are used, then structural requirements can be met, but aerodynamic efficiency is compromised and power capture is suboptimal

Engineering Contradiction:
Improvepower captureVSAvoidaerodynamic optimization
Core Design Contradiction:
ProductivityVSEase of manufacture

Solution Approach 1:

The propeller blades are designed with variable pitch angles along their length, allowing different sections to operate at optimal angles for varying wind speeds and turbulence conditions. This dynamic adaptation enables the blades to maintain high aerodynamic efficiency across diverse operating conditions while capturing more power from the wind stream.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention modifies key aerodynamic parameters including blade shape, twist angle distribution, and pitch configuration to optimize the lift-to-drag ratio. By carefully controlling these parameters, the propeller achieves superior aerodynamic performance and power capture efficiency compared to traditional designs.

Inventive Principle:
Principle #35Parameter changes

2Strength

If the number of blades is increased, then structural strength is improved, but power extraction per blade is reduced and drag increases

Engineering Contradiction:
Improveblade structural strengthVSAvoidpower extraction
Core Design Contradiction:
StrengthVSProductivity

Solution Approach 1:

Each blade is designed with non-uniform properties along its length, including variable pitch angles and optimized cross-sectional shapes. This local optimization allows each blade to extract maximum power from the wind while maintaining sufficient structural strength, reducing the need for additional blades.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The propeller blades are constructed using composite materials that provide high strength-to-weight ratios, enabling thinner, lighter blades that maintain structural integrity while reducing drag and improving aerodynamic efficiency. This allows for fewer blades to achieve the same power extraction.

Inventive Principle:
Principle #40Composite materials

3Strength

If blade thickness is increased, then structural strength is improved, but aerodynamic drag increases and lift/drag ratio decreases

Engineering Contradiction:
Improveblade structural strengthVSAvoidaerodynamic drag
Core Design Contradiction:
StrengthVSObject-generated harmful factors

Solution Approach 1:

Advanced composite materials are used to construct blades with optimized thickness distributions. These materials provide the necessary structural strength with minimal material usage, allowing blades to be thinner and lighter, thereby reducing aerodynamic drag while maintaining adequate strength.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The blade cross-sections are designed with optimized curved geometries that reduce flow separation and minimize drag. The curved airfoil shapes and optimized leading/trailing edges improve the lift-to-drag ratio while maintaining structural integrity through careful curvature design.

Inventive Principle:
Principle #14Spheroidality (Curvature)

4Productivity

If the propeller operates at high angles of attack to maximize lift, then power capture increases, but drag increases dramatically and blade stall occurs

Engineering Contradiction:
Improvepower captureVSAvoiddrag and stall
Core Design Contradiction:
ProductivityVSObject-generated harmful factors

Solution Approach 1:

The variable pitch angle design allows different blade sections to operate at optimal angles for their local conditions. The pitch can be adjusted dynamically to respond to changing wind speeds and turbulence, maintaining high lift while avoiding excessive drag and stall conditions.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention optimizes the angle of attack parameter along the blade length and adjusts it dynamically based on operating conditions. This controlled parameter variation maximizes lift generation while keeping drag manageable and preventing stall, thereby optimizing power capture efficiency.

Inventive Principle:
Principle #35Parameter changes

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

The vortex-shaped propeller design improves wind energy capture by focusing energy flow towards the rotor center, increasing efficiency and reducing mechanical stress, while allowing for adaptability to different wind profiles, potentially exceeding the 59% power capture limit set by Betz's limit.

Implementation Method 1

Just like the wing of an airplane, wind turbine blades work by generating lift due to their shape. The more curved side generates low air pressures while high pressure air pushes on the other side of the airfoil. The net result is a lift force perpendicular to the direction of flow of the air.

Methodology Applied
Scientific EffectLift force generation: Aerofoil

Implementation Method 2

There is, unfortunately, also a retarding force on the blade: the drag. This is the force parallel to the wind flow which also increases with angle of attack. In an appropriately shaped airfoil, the lift force is much bigger than the drag.

Methodology Applied
Scientific EffectDrag reduction: Drag

Data Source

PatentUS8905706B2Vortex propeller
Publication Date: 2014.12.09 BILLS CHRIS
  • US8905706B2 patent drawing
  • US8905706B2 patent drawing
  • US8905706B2 patent drawing

AI summary

The invention discloses at least one blade extending away from a beginning point and longitudinally along a central axis and approximating the shape of a spiral about said central axis. The blade comprises a beginning point disposed a first lateral distance away from the central axis and a terminating point disposed a second lateral distance away from the central axis, the second distance being greater than the first distance.