Axial-Cavity-Free Pen-Type Bushing Securing for Wind Blades

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Solution Overview

Problem

Existing methods are not suitable for securing pen-type bushings in the blade root of a wind turbine blade, as they require additional axial cavities that are not compatible with this type of bushing.

Innovation Solution

A method involving a rod placement in the inner bushing channel, filling the space with a bonding compound, and using a sealing element to secure the bushing without an axial cavity, along with a cap to facilitate compound distribution and sealing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If an additional axial cavity is used to secure a bushing in a blade root, then the bushing can be accommodated, but the method is not suitable for pen-type bushings and requires additional structural complexity

Engineering Contradiction:
Improvesuitability for pen-type bushing installationVSAvoidaxial cavity structure
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The rod is placed inside the inner bushing channel, and the bonding compound flows through this nested structure. The rod acts as a temporary core around which the bonding compound is deposited, enabling the bushing to be secured without requiring an additional axial cavity in the blade root.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

Instead of using an axial cavity (one-dimensional approach), the invention utilizes the inner bushing channel (already present in the bushing structure) and flows bonding compound through it. This transforms the problem from requiring additional blade root modification to utilizing the existing bushing internal geometry.

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

2Ease of operation

If the inner bushing channel is left open, then the bonding compound can flow through, but the inner thread is exposed and vulnerable to damage

Engineering Contradiction:
Improvebonding compound flowVSAvoidinner thread protection
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The sealing element is installed in the inner bushing channel before the bonding compound is introduced. This preliminary action protects the inner thread from damage by the bonding compound while still allowing the compound to flow through the channel via the through-hole in the sealing element.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The sealing element acts as an intermediary component between the bonding compound and the inner thread. It has a through-hole that allows the bonding compound to pass through while preventing direct contact between the compound and the vulnerable inner thread, thus protecting it from damage.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of manufacture

If the bonding compound is applied without pressure, then the application is simple, but the bonding compound may not fill the entire space between the cavity and the bushing

Engineering Contradiction:
Improvebonding compound applicationVSAvoidcomplete space filling
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

A pressure difference is applied to the bonding compound during insertion, causing it to flow through the inner rod channel and fill the entire space between the cavity and the bushing. This pneumatic/hydraulic approach ensures complete filling without requiring complex manual application procedures.

Inventive Principle:
Principle #29Pneumatics and hydraulics

4Stability of the object's composition

If the rod remains in the bushing during curing, then the bushing is held in position, but the rod occupies space needed for bonding compound flow

Engineering Contradiction:
Improvebushing alignment during curingVSAvoidinner rod channel occupancy
Core Design Contradiction:
Stability of the object's compositionVSVolume of stationary object

Solution Approach 1:

The sealing element is divided into two functional parts: a first section that seals the inner bushing channel, and a second section with a through-hole that allows bonding compound to pass through. This segmentation enables the sealing function while maintaining flow path openness.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The rod is temporarily placed in the inner bushing channel during bonding compound application, then removed after the compound has been introduced. This extraction of the rod after serving its purpose as a flow guide and temporary support allows complete bonding without permanent occupation of the channel space.

Inventive Principle:
Principle #2Taking out (Extraction)

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

Enables secure placement and replacement of pen-type bushings in the blade root without axial cavities, ensuring effective bonding and alignment during curing.

Implementation Method 1

filling the space between the cavity and the bushing with a bonding compound to secure the bushing in the cavity thereby letting the bonding compound flow through the inner rod channel

Methodology Applied
Scientific EffectFluid flow:

Implementation Method 2

allowing the compound to cure until the bushing is secured in the cavity

Methodology Applied
Scientific EffectCuring:

Implementation Method 3

selecting and placing a sealing element in the inner bushing channel near the second outer end of the bushing for sealing off the inner bushing channel

Methodology Applied
Scientific EffectSealing:

Data Source

PatentUS12442355B2Method for securing a bushing in a blade root of a wind turbine blade and cap for use in said method
Publication Date: 2025.10.14 VIVENTUS HLDG
  • US12442355B2 patent drawing
  • US12442355B2 patent drawing
  • US12442355B2 patent drawing

AI summary

The invention relates to a method for securing a bushing in a blade root of a wind turbine blade according to the preamble of claim 1. The method is known in the state of the art. The known method uses an additional cavity in axial direction of the blade root. The cavities in axial and radial direction are used for accommodation of a T-bolt type bushing. The known method is not suitable for pen-type bushing. The invention has for its purpose to provide a method, which is suitable for securing a pen-type bushing in the blade root, which method can also be used to replace an existing pen-type bushing in a blade root.