Needle-Punched Fibrous Preform for Controlled Z-Axis Fibre Alignment

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Solution Overview

Problem

Current methods for producing carbon fibre preforms for braking systems, such as carbon/carbon (C/C) brake discs, fail to distribute fibres in a controlled manner both on the main plane and orthogonal to it without causing fibre damage, leading to inadequate mechanical and thermal properties.

Innovation Solution

A method involving the superposition of carbon fibre layers, followed by needle-punching with a device equipped with barbs to orient fibres parallel to a predefined axis, using non-woven layers to protect woven layers and control fibre distribution, allowing for controlled fibre arrangement without damage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If needle-punching is used to arrange fibres parallel to the superposition axis, then fibres are distributed homogeneously on the axis Z, but fibres are forced damaged reducing mechanical features

Engineering Contradiction:
Improvefibre distribution homogeneityVSAvoidmechanical strength
Core Design Contradiction:
Manufacturing precisionVSStrength

Solution Approach 1:

The invention separates fibre placement into two distinct mechanisms: non-woven layers provide homogeneous orthogonal distribution through needle-punching, while woven layers preserve fibre integrity for in-plane strength. This segmentation allows homogeneous distribution without the harmful effects of forced fibre arrangement

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The non-woven layer acts as an intermediary that enables homogeneous fibre distribution along the axis Z without directly damaging the more critical woven fibres. The non-woven fibres serve as a sacrificial medium that achieves distribution homogeneity while protecting the structural integrity of the woven fibre system

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of manufacture

If impregnation and moulding of short fibres is used, then production cost and simplicity are reduced, but fibres along the axis Z are almost totally absent resulting in poor technical features

Engineering Contradiction:
Improveproduction simplicityVSAvoidcompression strength along axis Z
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

The invention performs preliminary arrangement of fibres in specific configurations (woven and non-woven layers) before the impregnation and moulding process. This preliminary structuring ensures that fibres are already positioned to provide both in-plane and orthogonal strength, eliminating the need for complex post-processing while maintaining simple production methods

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention uses a composite structure combining woven and non-woven fibre layers, each contributing different properties. The woven layers provide in-plane strength while the non-woven layers provide orthogonal fibre distribution, achieving superior technical features while maintaining the simplicity of impregnation and moulding processes

Inventive Principle:
Principle #40Composite materials

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 enables controlled fibre distribution, enhancing mechanical strength and thermal conductivity of C/C brake discs by ensuring fibres are aligned appropriately, improving the overall performance of braking systems while maintaining fibre integrity.

Implementation Method 1

a step b) of needle-punching by means of least one first needle-punching device the multilayer body in a needle-punching direction substantially parallel to the superposition axis to arrange at least part of the fibres parallel to the superposition axis

Methodology Applied
Scientific EffectMechanical Force: Mechanical Force

Implementation Method 2

using non-woven layers to protect woven layers and control fibre distribution, allowing for controlled fibre arrangement without damage

Methodology Applied
Scientific EffectPhysical Protection: Physical Containment

Data Source

PatentUS20240051256A1Method of making a fibrous preform and a fibrous preform thus obtained
Publication Date: 2024.02.15 FRENI BREMBO SPA
  • US20240051256A1 patent drawing
  • US20240051256A1 patent drawing
  • US20240051256A1 patent drawing

AI summary

A method of making a fibrous preform in carbon and/or fibres of a carbon precursor may include superposing at least two layers of carbon fibres and/or fibres of a carbon precursor according to a predefined superposition axis Z so as to form a multilayer body. The method may also include needle-punching via least one first needle-punching device the multilayer body in a needle-punching direction substantially parallel to the superposition axis Z to arrange at least part of the fibres parallel to the superposition axis Z, so as to obtain a needle-punched multilayer body. An optional step may include superposing with each other according to the superposition axis Z two or more of the needle-punched multilayer bodies, obtained separately by applying the above steps.