Segmented Stiffening Structure for Wind Turbine Rotor Blade Twist

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Solution Overview

Problem

Existing rotor blade constructions for wind turbines are cumbersome and costly in creating an inherent twist or torque under external loads, which is necessary to reduce mechanical loads and weight.

Innovation Solution

The rotor blade features an axially segmented stiffening structure with segments having different positions and orientations relative to each other and the longitudinal axis, allowing for localized adjustments in mechanical behavior to generate twist or torque, thereby reducing the angle of attack and load on the blade.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a rotor blade construction uses more material to withstand high mechanical loads, then the strength and stability are improved, but the weight of the rotor blade increases

Engineering Contradiction:
Improvemechanical load resistanceVSAvoidrotor blade weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The stiffening structure is divided into multiple axially adjacent segments (first stiffening structure segment, second stiffening structure segment, etc.) that can independently deform. This segmentation allows the rotor blade to create inherent twist through differential segment deformation, reducing mechanical loads without requiring additional material, thus resolving the contradiction between strength and weight.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The stiffening structure segments are designed with different positions and orientations relative to the longitudinal axis, enabling dynamic twist creation under external loads. This dynamic response allows the rotor blade to automatically adjust its geometry to reduce loads, maintaining strength while minimizing weight.

Inventive Principle:
Principle #15Dynamics

2Ease of manufacture

If the stiffening structure is made as a single continuous piece, then the manufacturing process is simpler, but the ability to create inherent twist is reduced

Engineering Contradiction:
Improvestiffening structure fabricationVSAvoidtwist creation capability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The stiffening structure is segmented into multiple axially adjacent segments with different positions and orientations. Each segment can be manufactured separately and then assembled, which maintains manufacturing simplicity while enabling the creation of inherent twist through the differential arrangement of segments, thus resolving the contradiction between ease of manufacture and adaptability.

Inventive Principle:
Principle #1Segmentation

3Stability of the object's composition

If the stiffening structure segments are all oriented the same way, then the structural symmetry is maintained, but the inherent twist creation capability is lost

Engineering Contradiction:
Improvestructural symmetryVSAvoidtwist generation ability
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The stiffening structure segments are deliberately arranged with different positions and orientations relative to the longitudinal axis of the base body. This asymmetric arrangement allows the structure to create inherent twist under external loads while maintaining overall structural stability, resolving the contradiction between symmetry and adaptability.

Inventive Principle:
Principle #4Asymmetry

4Strength

If axially adjacent stiffening structure segments overlap each other, then the structural connection is strengthened, but the complexity of assembly increases

Engineering Contradiction:
Improvesegment connection strengthVSAvoidassembly complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

Axially adjacent stiffening structure segments are designed to overlap each other, merging their structural functions to create stronger connections. This overlap design strengthens the segmental structure while the standardized segment interfaces keep assembly complexity manageable, resolving the contradiction between connection strength and assembly complexity.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP2587050B1Rotor blade
Publication Date: 2019.06.19 SIEMENS GAMESA RENEWABLE ENERGY AS
  • EP2587050B1 patent drawingFigure 1~2
  • EP2587050B1 patent drawingFigure 3~6
  • EP2587050B1 patent drawingFigure 7~10

AI summary

Rotor blade (4) for a wind turbine (1), comprising a longitudinal rotor blade base body (5), whereby a stiffening structure (6) is disposed within the base body (5), wherein the stiffening structure (6) is divided in at least two, axially adjacently disposed stiffening structure segments (6a, 6b), whereby at least one first stiffening structure segment (6a) is disposed with a different position and/or orientation relative to at least one further stiffening structure segment (6b) and/or relative to the longitudinal axis (A) of the base body (5).