Wind Turbine Spar Cap Segmentation for Shape and Strength
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Solution Overview
Problem
The existing methods for manufacturing wind turbine blades with spar caps are limited by the difficulty in bending or twisting the spar caps to match the blade shape, which restricts the blade design and can lead to reduced strength due to pore formation in the spar caps.
Innovation Solution
A method of manufacturing wind turbine blades that involves forming first-type spar caps by stacking support plates with reinforcing fibers and second-type spar caps by impregnating reinforcing fiber sheets with resin, and then injecting resin between the spar caps and core panels to form the blade shells, which are subsequently assembled.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Shape
If traditional spar caps are used, then the blade structure is simple, but it is difficult to bend or twist the spar cap to match the blade shape
Solution Approach 1:
The spar cap is divided into multiple segments or layers that can be independently formed and then assembled. This segmentation allows each segment to be manufactured separately with standard materials, and then joined together to create the complex three-dimensional curved shape required by the blade design.
Solution Approach 2:
Multiple spar cap layers are nested within each other, with each layer contributing to the overall complex geometry. The nested structure allows inner layers to form the base shape while outer layers add additional curvature and complexity, enabling the spar cap to match the blade's three-dimensional shape.
2Adaptability or versatility
If spar caps are forced to match blade shape, then the blade design flexibility increases, but pores may form in the spar cap reducing strength
Solution Approach 1:
The spar cap segments are pre-formed to match the required blade shape before final assembly. By preparing the segments in advance with proper geometry and bonding surfaces, the final assembly process becomes simpler and less likely to introduce defects such as pores, while maintaining design flexibility.
Solution Approach 2:
The manufacturing process parameters are optimized to prevent pore formation during spar cap fabrication and assembly. This includes controlling resin viscosity, injection pressure, and curing conditions to ensure complete wetting of fiber layers without trapping air, thereby maintaining high strength while achieving complex shapes.
3Productivity
If complex blade shapes are designed, then aerodynamic performance improves, but the manufacturing difficulty of spar caps increases
Solution Approach 1:
The complex spar cap structure is segmented into multiple manageable layers and sections that can be manufactured using standard processes. Each segment maintains the required aerodynamic contour while being producible with conventional materials and equipment, thereby achieving high aerodynamic performance without excessive manufacturing complexity.
Solution Approach 2:
The spar cap utilizes composite material construction with multiple fiber orientations and material properties in different layers. This composite structure allows the spar cap to conform to complex aerodynamic shapes while maintaining structural efficiency and manufacturability through standardized composite fabrication techniques.
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
This method allows for easier manufacturing of wind turbine blades while enhancing structural strength by enabling more flexible design and preventing pore formation in the spar caps.
Implementation Method 1
injecting a resin in a state in which a vacuum pressure is applied to a space between the cover and the main mold
Data Source
AI summary
A method of manufacturing a wind turbine blade capable of being easily manufactured and improving structural strength. The method of manufacturing the wind turbine blade includes performing spar cap formation in which a first-type spar cap having a structure in which support plates including reinforcing fibers are stacked and a second-type spar cap including reinforcing fiber sheets are formed, performing shell formation in which a pressure side shell and a suction side shell are formed by injecting a resin in a state in which the first-type spar cap, the second-type spar cap, and a core panel are disposed between an inner skin and an outer skin, and performing shell assembly in which the pressure side shell is joined to the suction side shell.


