Turbine Blade Segmentation for Remote Assembly

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Solution Overview

Problem

Shipping large turbine blades for applications like wind turbines is inconvenient and expensive due to their size, necessitating a method to join sections together at a remote location without excessive complexity and expense.

Innovation Solution

A method involving the integration of an integral bulkhead with a blade shell to form a blade, which is then separated into segments, allowing each segment to include a portion of the bulkhead and shell, enabling easier assembly and shipment, with the bulkhead being fabricated as a one-piece component or composite parts integrated using locking elements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If turbine blades are manufactured as large integral structures, then structural strength and integrity are improved, but shipping cost and convenience deteriorate

Engineering Contradiction:
Improvestructural strengthVSAvoidshipping cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The turbine blade is divided into multiple segments that can be manufactured separately and assembled at the installation site. The bulkhead is designed with integrated attachment features that enable mechanical connection between segments, maintaining structural integrity while allowing separate transportation of smaller components.

Inventive Principle:
Principle #1Segmentation

2Ease of manufacture

If turbine blades are divided into segments for shipping, then shipping cost and convenience are improved, but assembly complexity at remote location worsens

Engineering Contradiction:
Improveshipping convenienceVSAvoidassembly complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The bulkhead integrates multiple functions into a single component: it provides structural support, incorporates attachment features for joining blade segments, and includes mechanisms for securing the joint. This merging of functions reduces the number of separate parts and simplifies the assembly process at remote locations.

Inventive Principle:
Principle #5Merging (Combining)

3Manufacturing precision

If bulkhead is fabricated as one-piece component, then manufacturing precision and structural integrity are improved, but material usage and cost worsen

Engineering Contradiction:
Improvebulkhead precisionVSAvoidmaterial usage
Core Design Contradiction:
Manufacturing precisionVSQuantity of substance

Solution Approach 1:

The bulkhead is divided into multiple parts that can be manufactured separately using optimized material quantities for each section, then joined using locking elements. This segmentation allows for more efficient material usage while maintaining the structural integrity and precision of the complete bulkhead assembly.

Inventive Principle:
Principle #1Segmentation

4Adaptability or versatility

If blade is assembled from multiple parts, then adaptability for remote assembly is improved, but device complexity worsens

Engineering Contradiction:
Improveremote assembly capabilityVSAvoidnumber of parts
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The bulkhead combines multiple functional elements into integrated features, including attachment surfaces, locking mechanisms, and structural support elements. This reduces the total number of separate parts required while maintaining the adaptability for remote assembly of blade segments.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS8510947B2Turbine blade fabrication
Publication Date: 2013.08.20 GE INFRASTRUCTURE TECH LLC
  • US8510947B2 patent drawing
  • US8510947B2 patent drawing
  • US8510947B2 patent drawing

AI summary

A method includes joining an integral bulkhead and a blade shell to form a blade and separating the blade into two blade segments at a location including the integral bulkhead such that each blade segment comprises a portion of the integral bulkhead and a portion of the blade shell.