Segmented Wing Wind Turbine for Low Speed Efficiency

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Solution Overview

Problem

Conventional wind energy systems face inefficiencies in low wind conditions and are cumbersome in construction and maintenance, lacking scalability and flexibility in power distribution for various applications.

Innovation Solution

The design incorporates a support structure, hub assembly, and a wing structure with full-length and segmental wings, allowing for rotational efficiency and adaptable power distribution, featuring a cylindrical annular rim to enhance torque generation and aerodynamic lift, enabling efficient energy conversion across different wind conditions and scalable sizes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If conventional wind turbine designs are used, then结构简单性 is maintained, but efficiency in low wind conditions deteriorates

Engineering Contradiction:
Improveefficiency in low wind conditionsVSAvoidstructure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The wind turbine is divided into multiple independent wing structures (first plurality and second plurality) with different radial lengths, allowing each segment to operate optimally in low wind conditions while maintaining overall structural efficiency

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The wing structures are designed to be adjustable in angle and configuration, allowing the system to dynamically adapt to varying wind conditions, particularly optimizing performance in low wind scenarios

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If traditional wind energy systems are used, then manufacturing simplicity is maintained, but scalability and adaptability deteriorate

Engineering Contradiction:
Improvescalability and flexibilityVSAvoidconstruction and maintenance complexity
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The system uses modular wing structures that can be independently manufactured and assembled, enabling scalable deployment from small to large configurations while simplifying construction and maintenance operations

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The wing structures are designed with universal mounting configurations that allow the same basic components to be used across different scale implementations, enhancing scalability while maintaining manufacturing simplicity

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

3Adaptability or versatility

If uniform wing structures are used, then manufacturing simplicity is maintained, but power distribution flexibility deteriorates

Engineering Contradiction:
Improvepower distribution flexibilityVSAvoidwing structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

Different wing structures are assigned different radial lengths (first plurality extending to first radius, second plurality extending to second radius), allowing each local segment to optimize power capture for specific applications while maintaining overall system flexibility

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The wing structure is segmented into multiple independent units with varying radii, enabling flexible power distribution to multiple applications simultaneously while managing structural complexity through modular design

Inventive Principle:
Principle #1Segmentation

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 system achieves high efficiency in various wind conditions, simplifies construction and maintenance, and allows flexible power distribution to suit diverse applications, from small to large scales, including simultaneous operation with multiple energy systems.

Implementation Method 1

a plurality of full-length wings extending from near the hub assembly to near the outer periphery

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Implementation Method 2

a plurality of segmental wings that are radially shorter than the full-length wings

Methodology Applied
Scientific EffectAerodynamic drag: Drag

Implementation Method 3

cylindrical annular rim extending around an outer periphery of the wing structure

Methodology Applied
Scientific EffectTorque generation: Torque

Data Source

PatentUS11220992B2Wind energy systems
Publication Date: 2022.01.11 JMCC WING LLC
  • US11220992B2 patent drawing
  • US11220992B2 patent drawing
  • US11220992B2 patent drawing

AI summary

Systems can be used to harness energy from winds. For example, this document describes scalable systems having multiple wing-like blades that can efficiently convert wind power into electricity and other types of energy.