Modular Wind Turbine Rotor Blade Segmentation

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Solution Overview

Problem

Large wind turbine rotor blades are difficult to produce and transport due to their length and weight, and they are subjected to significant dynamic stresses, making them challenging to maintain and repair effectively.

Innovation Solution

A modular rotor blade design comprising multiple blade modules with detachable butt-joints and inlays made of fiber composite materials, allowing for easier assembly, transportation, and maintenance, with the ability to replace individual modules for aerodynamic optimization and repair.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If rotor blades are made as single large pieces to maintain structural integrity, then strength and reliability are improved, but production difficulty and transportation complexity increase

Engineering Contradiction:
Improvestructural integrityVSAvoidproduction difficulty
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The rotor blade is divided into multiple blade modules that can be produced separately and then assembled together. Each module maintains structural integrity through its own internal design, while the overall blade benefits from modular construction that simplifies production and transportation.

Inventive Principle:
Principle #1Segmentation

2Productivity

If rotor blades are made as single large pieces to ensure aerodynamic performance, then aerodynamic efficiency is improved, but transportation and assembly complexity increase

Engineering Contradiction:
Improveaerodynamic efficiencyVSAvoidassembly complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The blade is segmented into modules with standardized connection interfaces that maintain the overall aerodynamic profile. The segmentation allows for simplified transportation and assembly while preserving aerodynamic performance through careful design of the module connections and airfoil continuity.

Inventive Principle:
Principle #1Segmentation

3Strength

If rotor blades are made as single large pieces to maintain structural strength, then strength under dynamic stress is improved, but ease of repair and maintenance decrease

Engineering Contradiction:
Improvestrength under dynamic stressVSAvoidease of maintenance
Core Design Contradiction:
StrengthVSEase of repair

Solution Approach 1:

The rotor blade is divided into multiple replaceable modules connected by detachable joints. This allows individual damaged modules to be replaced without affecting the structural integrity of the entire blade, as the detachable connections maintain sufficient strength while enabling easy module replacement for maintenance and repair.

Inventive Principle:
Principle #1Segmentation

4Stability of the object's composition

If rotor blades are designed as fixed single pieces to ensure structural stability, then stability is improved, but adaptability for aerodynamic optimization decreases

Engineering Contradiction:
Improvestructural stabilityVSAvoidaerodynamic optimization
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The modular design enables dynamic reconfiguration of the rotor blade by allowing different module combinations. Modules with varying aerodynamic characteristics can be assembled to optimize performance for different operating conditions, while the standardized connection system maintains structural stability during operation.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP2199604B1A modular rotor blade and a method for assembling a modular rotor blade
Publication Date: 2016.07.13 GENERAL ELECTRIC CO
  • EP2199604B1 patent drawingFigure 1~2
  • EP2199604B1 patent drawingFigure 3~4
  • EP2199604B1 patent drawingFigure 5~6

AI summary

A blade module (100) of a modular rotor blade (5) comprising a hollow fiber composite body (150) which extends along a longitudinal blade axis and at least one inlay (10) located at or near a longitudinal end of the fiber composite body (150) is provided. The inlay (10) includes a receptacle (11) which is adapted to receive a threaded fastener (80) and an anchoring portion (12) anchored to the fiber composite body (150). Further, a modular wind turbine rotor blade (5) which includes at least two blade modules (100, 200) and a method for assembling a modular wind turbine rotor blade (5) are provided.