Wind Turbine Rotor Blade Joint Segmentation

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Solution Overview

Problem

Existing wind turbine rotor blade assembly methods face challenges such as alignment difficulties, complex inspection processes, and inability to disassemble segments for maintenance or upgrades, particularly in larger turbines, which increase manufacturing, transportation, and assembly costs while compromising structural integrity and energy efficiency.

Innovation Solution

A blade segment design featuring a shell segment with a joint portion projecting from the tip or root end, allowing for span-wise joining with adjacent segments, enabling accurate assembly and disassembly, and facilitating the use of mechanical fasteners or bonding materials for secure connection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If rotor blades are manufactured in blade segments to reduce transportation and assembly costs, then manufacturing and transportation costs are reduced, but alignment difficulties and assembly complexity increase

Engineering Contradiction:
Improvemanufacturing costVSAvoidassembly complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The rotor blade is divided into multiple blade segments that can be manufactured separately and transported independently. Each segment includes joint portions with joining surfaces that enable modular assembly, reducing transportation costs while maintaining structural integrity through the segmented design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The joint portion with joining surfaces acts as an intermediary element between adjacent blade segments. This intermediary structure facilitates precise alignment and secure connection during assembly, reducing assembly complexity while enabling modular manufacturing and transportation.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Power

If blade segments are joined together to form large rotor blades, then energy production and aerodynamic performance are improved, but inspection and maintenance difficulty increase

Engineering Contradiction:
Improveenergy productionVSAvoidinspection difficulty
Core Design Contradiction:
PowerVSEase of repair

Solution Approach 1:

The rotor blade is segmented into modular sections that can be independently inspected and maintained. The joint portions provide accessible interfaces for inspection, allowing technicians to examine connection integrity without disassembling the entire blade structure, thus facilitating maintenance while maintaining large blade power generation capabilities.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The modular segment design allows individual blade segments to be replaced or upgraded without replacing the entire rotor blade. This enables selective maintenance and recovery of functional segments, reducing inspection difficulty and maintenance costs while preserving the high power output of large rotor blades.

Inventive Principle:
Principle #34Discarding and recovering

3Power

If rotor blade size is increased to improve energy efficiency, then energy production increases, but manufacturing and transportation costs increase

Engineering Contradiction:
Improveenergy productionVSAvoidmanufacturing cost
Core Design Contradiction:
PowerVSEase of manufacture

Solution Approach 1:

Large rotor blades are divided into smaller manageable segments that can be manufactured using standard facilities and equipment. This segmentation enables production of large-scale high-power blades without requiring specialized manufacturing infrastructure, reducing manufacturing costs while maintaining the energy production benefits of large blade size.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The segmented blade design allows smaller segments to be assembled into a larger complete blade structure. This nested approach enables transportation of smaller, more manageable segments through standard infrastructure while ultimately achieving the large rotor blade configuration needed for high energy production.

Inventive Principle:
Principle #7Nested doll (Nesting)

4Strength

If blade segments are designed for permanent assembly to ensure structural integrity, then structural strength is improved, but adaptability for maintenance and upgrades is reduced

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

Solution Approach 1:

The joint portions are designed with dynamic characteristics that provide rigid connection during operation to ensure structural integrity, while allowing for controlled disassembly when needed. The joining surfaces and fastening mechanisms maintain strong structural connection under load but can be systematically disconnected for maintenance or upgrades, providing both strength and adaptability.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The joint portion design serves multiple functions: providing structural connection for integrity during operation, enabling precise alignment during assembly, and allowing controlled disassembly for maintenance. This multi-functional design achieves both structural strength and adaptability without compromise.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Data Source

PatentUS7997874B2Wind turbine rotor blade joint
Publication Date: 2011.08.16 GE INFRASTRUCTURE TECH LLC
  • US7997874B2 patent drawing
  • US7997874B2 patent drawing
  • US7997874B2 patent drawing

AI summary

A blade segment is disclosed for a rotor blade formed from a plurality of blade segments, the blade segment having a span and a chord. The blade segment includes a shell segment having a pressure side and a suction side extending between a leading edge and a trailing edge, the shell segment further having a tip end and a root end. The blade segment further includes at least one joint portion projecting from the shell segment at one of the tip end or the root end and defining a generally span-wise extending joining surface. The joint portion allows the blade segment to be coupled to an adjacent blade segment with a mating joint portion.