Wind Turbine Blade Shell with Low Shear Modulus Regions

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Solution Overview

Problem

Wind turbine blades have high torsional stiffness near the root, limiting the amount of twist that can be induced by aerodynamically generated bending moments, which restricts performance improvements.

Innovation Solution

Incorporating regions of lower modulus materials or structures, such as thinner layers or slip joints, between shell sections to reduce torsional stiffness, particularly near the root, allowing increased twist response and aerodynamic performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the blade shell uses uniform thick material throughout, then the blade has high strength and rigidity, but the torsional stiffness is too high which limits twist response

Engineering Contradiction:
Improveblade strengthVSAvoidtorsional stiffness
Core Design Contradiction:
StrengthVSStability of the object's composition

Solution Approach 1:

The blade shell transitions from uniform thickness to variable thickness, with thicker sections at the root for strength and thinner sections toward the tip for reduced torsional stiffness. This local differentiation allows the blade to maintain structural integrity while enabling greater twist response in the outer regions.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The blade shell is divided into multiple sections with different thickness characteristics. The root region maintains thick construction for strength, while intermediate and tip regions use progressively thinner sections, creating segmented stiffness zones that allow controlled twist propagation along the blade length.

Inventive Principle:
Principle #1Segmentation

2Strength

If the blade root is made very thick for strength, then the blade has high structural integrity, but the sweep response and twist capability are reduced

Engineering Contradiction:
Improvestructural integrityVSAvoidtwist capability
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The blade employs local quality differentiation where the root section maintains thick construction for structural integrity and strength, while intermediate and outer sections use progressively thinner material. This allows the thick root to provide anchoring strength while the thinner outer sections provide the flexibility needed for sweep response and twist capability.

Inventive Principle:
Principle #3Local quality

3Stability of the object's composition

If regions of lower modulus material are introduced to reduce torsional stiffness, then twist response increases, but the overall structural rigidity may be compromised

Engineering Contradiction:
Improvetorsional stiffnessVSAvoidstructural rigidity
Core Design Contradiction:
Stability of the object's compositionVSStrength

Solution Approach 1:

The blade shell uses material with lower modulus of rigidity in specific regions (particularly intermediate and outer sections) while maintaining higher modulus material in the root section. This localized material property differentiation reduces torsional stiffness where flexibility is needed while preserving structural rigidity where strength is critical.

Inventive Principle:
Principle #3Local quality

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 reduction in torsional stiffness enhances the twist response of the blade, improving overall performance by allowing greater aerodynamic flexibility and efficiency.

Implementation Method 1

the intermediate shell section includes a material having a lower modulus of rigidity than the first shell section and the second shell section

Methodology Applied
Scientific EffectModulus of rigidity: Elasticity

Implementation Method 2

at least a portion of an edge of the first shell panel is configured to slidably interact with at least a portion of an edge of the second shell panel to reduce the torsional stiffness of the blade shell

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentUS8075278B2Shell structure of wind turbine blade having regions of low shear modulus
Publication Date: 2011.12.13 ZUTECK MICHAEL D
  • US8075278B2 patent drawing
  • US8075278B2 patent drawing
  • US8075278B2 patent drawing

AI summary

The torsional rigidity of a wind turbine blade affects the twist response of the blade induced by bending moments within the blade. By including regions having a lower modulus of rigidity than the remainder of the blade shell, the torsional rigidity of the blade shell can be decreased, and the twist response thereby increased. In blades having a single shear web, this twist response may be more pronounced. The regions of low modulus may comprise additional shell panels, or thick regions of low modulus joining material.