Curled C-Shape Wind Turbine Blade Winglet Design

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Solution Overview

Problem

Existing wind turbine blade winglets face limitations in reducing tip vortex losses and thrust loads, leading to sub-optimal aerodynamic performance and potential tower-strike issues, with traditional L-shaped structures being either ineffective or limited by weight and drag penalties.

Innovation Solution

A compact curled winglet structure is introduced, extending spanwise from the tip towards the center of rotation to form a C-shape or open P-shape, which can be smoothly curved, boxy planar, or a combination thereof, on both the pressure and suction sides, reducing out-of-plane thrust and enhancing aerodynamic efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If traditional L-shaped winglet structures are used, then the blade tip vortex suppression is improved, but the tower-strike margin is reduced

Engineering Contradiction:
Improvetip vortexVSAvoidtower-strike margin
Core Design Contradiction:
Object-affected harmful factorsVSLength of stationary object

Solution Approach 1:

The patent applies curvature by transitioning from straight L-shaped winglet segments to a continuously curved C-shaped or open P-shaped winglet structure. The winglet features a curved spanwise extension that smoothly transitions from the blade tip toward the center of rotation, creating a more aerodynamic profile that reduces tip vortices while maintaining adequate tower clearance through the curved geometry.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The patent moves beyond the traditional two-dimensional L-shaped winglet configuration by introducing a three-dimensional C-shaped or open P-shaped structure with curved spanwise and chordwise extensions. This dimensional transformation allows the winglet to effectively suppress tip vortices while maintaining sufficient distance from the tower through spatial optimization.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Productivity

If larger winglet structures are used to reduce tip vortex losses, then aerodynamic performance is improved, but weight and drag penalties increase

Engineering Contradiction:
Improveaerodynamic performanceVSAvoidwinglet weight
Core Design Contradiction:
ProductivityVSWeight of moving object

Solution Approach 1:

The curved C-shaped or open P-shaped winglet structure creates a more aerodynamic profile that reduces drag compared to traditional L-shaped designs. The smooth curvature minimizes flow separation and turbulence, allowing for effective tip vortex suppression with reduced structural weight requirements.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The patent optimizes the winglet geometry by changing key parameters including the curvature radius, spanwise extension length, and chordwise distribution. These parameter adjustments enable the winglet to achieve optimal aerodynamic performance while minimizing weight and drag penalties through precise geometric tuning.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If passive winglet devices are used, then manufacturing simplicity is improved, but adaptability to different operating conditions deteriorates

Engineering Contradiction:
Improvewinglet manufacturingVSAvoidoperating condition adaptability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The continuously curved C-shaped or open P-shaped winglet structure provides superior adaptability across different operating conditions compared to segmented L-shaped designs. The smooth curvature allows the winglet to effectively suppress tip vortices across a broader range of wind speeds and blade pitch angles, enhancing versatility while remaining manufacturable as a single-piece composite structure.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 curled winglet structure effectively minimizes tip vortex losses and thrust loads, improving aerodynamic performance while maintaining sufficient tower clearance, thus enhancing energy production and reducing structural weight and noise.

Implementation Method 1

winglets can be employed to improve the overall efficiency and performance of a wind turbine. For example, a winglet may decrease the amount of spanwise flow generated at the tip of a rotor blade and, thereby, reduce drag on the rotor blade

Methodology Applied
Scientific EffectVortex formation: Vortex Ring

Implementation Method 2

winglets may decrease the amount of spanwise flow generated at the tip of a rotor blade and, thereby, reduce drag on the rotor blade

Methodology Applied
Scientific EffectDrag reduction: Drag

Implementation Method 3

The rotor blades capture kinetic energy from wind using known airfoil principles and transmit the kinetic energy through rotational energy

Methodology Applied
Scientific EffectAirfoil principles: Aerofoil

Implementation Method 4

winglets may also be installed on rotor blades to reduce the overall diameter of the wind turbine as well as to reduce noise emitted by the blades

Methodology Applied
Scientific EffectNoise reduction: Sound

Data Source

PatentUS9086053B2Enhanced wind turbine blade
Publication Date: 2015.07.21 GE INFRASTRUCTURE TECH LLC
  • US9086053B2 patent drawing
  • US9086053B2 patent drawing
  • US9086053B2 patent drawing

AI summary

A wind turbine blade includes a root portion, a tip and a body extending between the root portion and the tip. The body has a pressure side and a suction side. The body further has at least one winglet. Each winglet has a spanwise extension towards the root portion of the rotor blade and that ends at the tip to form a winglet having a substantially C-shaped or substantially open P-shaped geometry.