Wind Turbine Blade Trailing Edge Tab Design

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Solution Overview

Problem

Wind turbine blade designs with thick flat-back trailing edges enhance structural strength and lift but suffer from noise, drag, and manufacturing complexities due to vortex shedding and sharp contours, while solutions like splitter plates reduce noise but not manufacturing issues.

Innovation Solution

A tab extending from the pressure side near the trailing edge, particularly in the aft 10% of the chord, increases lift by slowing airflow and directing it downward, with varying tab heights and shapes to optimize lift and reduce drag, and can be integrated or attached as an add-on with turbulators for enhanced performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a thick flat-back trailing edge is used, then structural strength and lift are improved, but noise and drag increase due to vortex shedding

Engineering Contradiction:
Improvestructural strengthVSAvoidvortex shedding noise and drag
Core Design Contradiction:
StrengthVSObject-generated harmful factors

Solution Approach 1:

The patent applies curvature by replacing the sharp flat-back trailing edge with a rounded trailing edge. This curvature modification eliminates the sharp contours that cause vortex shedding, thereby reducing noise and drag while maintaining structural strength through the rounded geometry

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Force

If a thick flat-back trailing edge is used, then lift is improved, but manufacturing complexity increases due to sharp contours

Engineering Contradiction:
ImproveliftVSAvoidblade molding
Core Design Contradiction:
ForceVSEase of manufacture

Solution Approach 1:

The rounded trailing edge replaces difficult-to-mold sharp contours with smooth curved surfaces that are easier to manufacture. This curvature transformation maintains the lift-enhancing thickness while eliminating molding problems associated with sharp edges

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Object-generated harmful factors

If a splitter plate is added to reduce vortex shedding, then noise is reduced, but device complexity increases

Engineering Contradiction:
Improvevortex shedding noiseVSAvoidblade structure
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The patent extracts and eliminates the source of vortex shedding by removing sharp contours from the trailing edge design. Instead of adding a splitter plate to mitigate the problem, the solution extracts the harmful sharp edges and replaces them with rounded contours, thereby reducing noise without adding device complexity

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

By applying curvature to the trailing edge, the patent fundamentally changes the geometry to prevent vortex shedding at its source, eliminating the need for additional components like splitter plates and thereby reducing device complexity

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 tab design enhances lift and structural strength while minimizing drag and manufacturing complexities, offering improved aerodynamic performance and practical molding capabilities.

Implementation Method 1

a tab extending into the boundary layer on the pressure side of a wind turbine blade near the trailing edge to increase lift

Methodology Applied
Scientific EffectBoundary layer: Boundary Layer

Data Source

PatentEP3329117B1Wind turbine blade with trailing edge tab
Publication Date: 2021.02.17 SIEMENS GAMESA RENEWABLE ENERGY AS
  • EP3329117B1 patent drawingFigure 1~2
  • EP3329117B1 patent drawingFigure 3~5
  • EP3329117B1 patent drawingFigure 6~11

AI summary

A wind turbine blade (20B-C) with a rounded trailing edge (42A-E) and an elongated tab (44A-J) extending from the pressure side (PS) within the aft 10% of the local chord (C) and generally parallel to the trailing edge to increase lift. The tab may have a height (H) that is greatest on the radially inboard end to maximize lift, and lower on the outboard end to minimize drag. It may have a base with a length of at least 60% of its height.