Wind Turbine Blade Root Assembly Staggered Bolt Configuration

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Solution Overview

Problem

Wind turbine blades with longer lengths experience increased loads, requiring stronger root assemblies. However, the limited space on the root portion's circumference for bolts and bushings restricts the root capacity, leading to high strain and potential failure, especially with staggered bolt configurations.

Innovation Solution

The root assembly features a staggered configuration of T-bolts with adjacent bushings offset axially, creating a quotient between the axial distance and bushing diameter of 2.5 or greater. This configuration allows for increased root capacity without expanding the circumferential spacing, and by optimizing the axial distance and bushing diameter, the strain in the laminate can be reduced.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a large number of bolts and bushings are provided in the root assembly to resist high loads, then the root capacity increases, but the space on the common circumference of the root portion is limited, making it difficult to accommodate more bolts

Engineering Contradiction:
Improveroot capacityVSAvoidcircumferential space
Core Design Contradiction:
StrengthVSArea of stationary object

Solution Approach 1:

The patent transitions from a single-plane circumferential arrangement of bolts to a three-dimensional staggered configuration where bolts are distributed across multiple axial planes. This dimensional change allows more bolts to be accommodated within the limited circumferential space by utilizing the axial dimension, thereby increasing root capacity without requiring additional circumferential area.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The staggered configuration effectively nests multiple rows of bolts within the radial and axial boundaries of the root portion. By offsetting adjacent bolts axially and radially, the design creates a compact nested arrangement that maximizes the number of bolts that can fit within the constrained root geometry, similar to how nested dolls occupy space efficiently.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Strength

If a staggered configuration of bolts is used to increase root capacity, then more bolts can be accommodated, but the root portions experience large strain and are susceptible to failure

Engineering Contradiction:
Improveroot capacityVSAvoidservice life
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent applies local quality by creating non-uniform spacing patterns in the staggered bolt configuration. Adjacent bolts are offset axially by distances specifically optimized to be at least 2.5 times the bushing diameter, creating zones of reduced strain concentration between adjacent bolts while maintaining overall load distribution. This localized optimization of spacing prevents excessive strain in critical areas while preserving the increased root capacity provided by the staggered arrangement.

Inventive Principle:
Principle #3Local quality

3Reliability

If the axial distance between adjacent bushings is increased to reduce strain, then the service life increases, but the root capacity decreases due to fewer bolts that can be accommodated

Engineering Contradiction:
Improveservice lifeVSAvoidroot capacity
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent systematically varies the axial distance parameter between adjacent bushings according to a specific criterion (at least 2.5 times the bushing diameter). This parameter optimization balances two competing requirements: sufficient axial spacing to reduce strain concentrations and extend service life, while maintaining enough compactness to accommodate the necessary number of bolts for adequate root capacity. The parameter change transforms the design from arbitrary spacing to an optimized configuration.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS12292028B2Root assembly of a wind turbine blade for a wind turbine, wind turbine blade and wind turbine
Publication Date: 2025.05.06 SIEMENS GAMESA RENEWABLE ENERGY AS
  • US12292028B2 patent drawing
  • US12292028B2 patent drawing
  • US12292028B2 patent drawing

AI summary

The following relates to a root assembly of a wind turbine blade for a wind turbine. The following further relates to a wind turbine blade including the root assembly and a wind turbine including the wind turbine blade.