Separate Tow Tensioning for Wrinkle-Free Composite Preforms

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Solution Overview

Problem

The formation of fabric preforms for composite components often results in distortions, wrinkles, and non-uniformity due to the difficulty in wrapping fabrics around forms without imperfections, leading to compromised structural integrity and mechanical properties in the final composite parts.

Innovation Solution

The method involves separately tensioning axial or hoop tows of the fabric during wrapping to reduce or eliminate imperfections, allowing for a more controlled and dense wrapping process, which can be achieved using tensioning mechanisms such as clutches or weights connected to the axial tows, enabling differential payout and slip, thereby improving the fiber architecture and mechanical properties of the composite material.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If conventional wrapping techniques are used to apply fabric around a form, then the process is simple and quick, but the fabric preform develops wrinkles, waviness, and distortion that compromise structural integrity

Engineering Contradiction:
Improvefabric preform qualityVSAvoidwrapping process complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The fabric is divided into separate axial tows that can be independently tensioned and controlled during wrapping. Each tow is paid out from its own dispenser, allowing individual adjustment of tension and payout rate to eliminate wrinkles and waviness while maintaining manufacturing feasibility

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The tension applied to each axial tow is independently controlled and adjusted during the wrapping process. By varying the tension parameters for different tows, the system eliminates fabric defects while managing the complexity through programmable control

Inventive Principle:
Principle #35Parameter changes

2Strength

If fabric is wrapped around a form without separate tensioning, then the equipment and process are simple, but the fiber architecture is poor and mechanical properties are reduced

Engineering Contradiction:
Improvemechanical properties of compositeVSAvoidtensioning mechanism complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

Multiple independent tensioning mechanisms are provided, with each mechanism controlling the tension of a specific axial tow. This segmentation allows precise control of fiber architecture to maximize mechanical properties while keeping each individual tensioning mechanism relatively simple

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Each tensioning mechanism serves multiple functions: it controls tow tension, regulates payout rate, and maintains proper fiber spacing. This multi-functionality reduces the need for additional separate systems, managing overall device complexity while improving mechanical properties

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 approach results in a higher fiber-to-resin ratio and improved mechanical properties of the composite components by reducing wrinkles and waviness, leading to a more consistent and stronger final product with enhanced structural integrity.

Implementation Method 1

friction between fibers or fiber bundles

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 2

separately tensioning each of the axial or hoop tows in the fabric

Methodology Applied
Scientific EffectTension: Tension

Data Source

PatentEP2794219B1Method and apparatus for forming a fabric preform for a composite material by separately tensioning tows
Publication Date: 2018.01.24 GKN AEROSPACE SERVICES STRUCTURES LLC
  • EP2794219B1 patent drawingFigure 1
  • EP2794219B1 patent drawingFigure 2
  • EP2794219B1 patent drawingFigure 3

AI summary

Disclosed are methods and devices for the formation of fabric preforms (20) that may be subsequently impregnated with a resin to form a composite component (18). One end of a fabric (44) is received on the form (54) such that the axial tows (46) of the fabric (44) extend in a direction generally perpendicular to a central axis (C-C) of the form (54). At least some of the plurality of axial tows (46) are separately tensioned on an end of the fabric (44) not attached to the form (54) and the fabric (44) is wrapped around the form (54) by rotating the fabric (44) and form (54) relative to one another about the central axis (C-C).