Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia...

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Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA

Transcript of Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia...

Page 1: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Opportunities and Challenges for Textile Reinforced Composites

Christopher M. Pastore

Philadelphia University

Philadelphia, Pennsylvania, USA

Page 2: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Textile Reinforced Composites

Fiber reinforced composites whose repeating volume element (RVE) is characterized by more than one fiber orientation.

Formed with hierarchical textile processes that manipulate individual fibers or yarn bundles to create an integral structure.

It is possible to join various sub-assemblies together to form even more complex structures.

Page 3: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Hierarchy of Textile Materials

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Perceived Benefits

Textiles are considered to have significant cost savings compared to tape lay-up. Individual layer of fabric is much thicker than tape. Fewer lay-up steps are necessary to create the final structure. Formed from dry fiber and infiltrated with resin in a secondary

operation. Handling and storage requirements of the material are reduced

compared to prepreg. A single product is suitable for a variety of matrix materials,

reducing inventory and manufacturing costs.

Page 5: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

2D and 3D Textiles

Textiles are frequently classified as either 2D or 3D. Clearly all fabrics are 3D, but 2-D implies that the

fabric is fundamentally thin. That is, the thickness of the fabric is formed by only 2 or 3 yarns in

the thickness direction.

A 3-D fabric can have substantial thickness, limited only by the machine, not some fundamental physical phenomenon.

Page 6: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Types of Textiles

Direct-formed fabrics are those made directly from fibers.

Woven, knitted, and braided fabrics are made from manipulation of yarns.

These four classes represent the vast majority of fabrics used in composite materials. woven fabrics are formed by inter-lacing yarns, knitted by inter-looping yarns, braided by inter-twining yarns, and direct formed fabrics by inter-locking fibers.

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Direct Formed Fabrics

Created directly from fibers without a yarn processing step involved.

No interlacing, intertwining, or interlooping of fibers within the structure.

These fabrics are called nonwovens in much of the literature, despite the obvious inadequacy of this term.

Page 8: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Direct Formed Fabrics

Generally there are 2 steps First a web is constructed of fibers. This sets the distribution of in-

plane fiber orientation. Next the web is densified. This typically involves through thickness

entanglement or bonding.

Page 9: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Web formation

Opening process: mechanically separates the fibers. Deposit fiber mass onto a belt, creating a continuous roll of low-

density material width of roughly 1-meter and a thickness 10-20 cm called a picker lap.

The fibers have a virtually uniform, random orientation in the plane, with substantial out of plane orientation.

To thin the picker lap, it may be passed through a card. Individual fibers are mostly oriented in the direction of material flow

through the machine. This orientation allows the fibers to pack closer than previously resulting in a

thickness reduction, increased density, and a preferred distribution of fiber orientations in the machine direction.

The resulting material is called a carded web.

Page 10: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Densification of web

The carded web may be used as input to the needle punch, or it may be cross-lapped first. The cross-lapper places carded web transverse to the machine

direction allowing the preferred fiber orientation to be in the cross direction.

Needle punch creates mechanical interlocking through barbed needles

Bonding can be done to chemically adhere the fibers Adhesive application Thermal bonding (sacrificial low melt fibers are pre-included in the

web)

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XYZ Orthogonal Nonwoven

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Knitted Fabrics

There are two basic types of knitting - weft knitting and warp knitting.

They are distinguished by the direction in which the loops are formed. Weft knitting, the most common type of knitting in the apparel

industry, forms loops when yarns are moving in the weft direction, or perpendicular to the direction of fabric formation.

Warp knitting differs from weft knitting in that multiple yarns are interlooped simultaneously. A set of yarns are supplied from a creel or warp beam and interlooped in the cross (course) direction.

Page 13: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Jersey Knits The simplest weft knit structure is

the jersey. Inherently bulky due to curvature

of the yarn. The “natural” thickness of a jersey

knit fabric is roughly three times the thickness of the yarns, resulting in maximum yarn packing factors of 20-25%, and thus Vf around 15%.

High extensibility (up to 100% strain to failure) which allows complex shape formation capabilities.

Page 14: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Rib Knits In a rib knit structure it is possible to incorporate large yarns in the weft

to create a weft inserted rib knit. In such a way a “unidirectional” preform can be constructed. However

it is difficult to achieve fiber volume fractions greater than 30% in these structures due to the inherent bulkiness of the fabric.

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Conformable Rib Knit

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Warp Knits In the WIWK, the load bearing yarns are locked into

the structure through the knitting process

Page 17: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Braiding

Biaxial braided fabrics may incorporate a longitudinal yarn creating a triaxial braid.

The braided fabric is characterized mainly by the braid angle, , (10° - 80°).

Braids are tubular and frequently compared with filament winding. They have been shown to be cost competitive.

The braided fabric is flexible before formation, and thus the fabric can conform to various shapes. The braided fabric may be formed around a mandrel, and rather complex shapes can be formed.

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Braiding

Braids are formed by a circular “maypole” pattern of yarn carrier motions

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Types of 2D Braids

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3D Braiding Machine

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Woven Fabrics

Generally characterized by two sets of perpendicular yarns systems

One set is raised and lowered to make “sheds” (these are warp yarns)

The other set is passed through these sheds, perpendicular to the warp yarns (these are fill, or pick or weft yarns)

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Elements of a loom

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Woven Fabrics

The structure of the woven fabric is the pattern of interlacing between the warp and weft yarns

Yarns can “float”, or not interlace for some distance within a woven fabric

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Basic weave structures

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Crimp in Weaves

The crimp is defined as one less than the ratio of the yarn's actual length to the length of fabric it traverses.

Crimp levels influence fiber volume fraction, thickness of fabric, and mechanical performance of fabric.

High crimp leads to Reduced tensile and compressive properties Increased shear modulus in the dry fabric and the resulting

composite Fewer regions for localized delamination between individual yarns.

Page 26: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Applications of Weaves

Weaves can be formed into composites with fiber volume fractions as high as 65%.

High harness count satins – 8 and 12 –serve the role previously held by 0/90 tape lay-ups.

There is a significant cost benefit to using the fabrics in that much fewer layers need be applied because the woven fabric is usually many times thicker than the tape (depending on the yarns used in the fabric).

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3D Weaves

Layer-to-layer Through thickness

XYZ

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Doubly Stiffened Woven Panel

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Variations in Weave Design

If large yarns are used in the warp direction and small yarns are infrequently spaced in the weft direction, the resulting fabric resembles a unidirectional material.

Weaves can be formed with gradients in a single or double axis by changing yarn size across the width or length

Complex shapes can be achieved through “floating” and cutting yarns to reduce total number of yarns in some section of the part

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Gradations through yarn size

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Shape through floats

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Issues with shaping woven fabrics

Tailoring the cross-section of a woven fabric will generally result in a change in weave angle, a change in the distribution of longitudinal, weaver, and fill, and a change in fiber volume fraction in consequence to the change in

thickness.

Some fiber volume fraction effects can be controlled by tooling. The tailoring occurs in a discrete manner, using individual yarns, whereas most tooling will be approximately continuous.

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Example of single taper weave

Consider a tapered panel where gradation in thickness is achieved by changing yarn size/count across the width

Page 34: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Design of tapered woven panel

Pick count is constant, warps and wefts per dent are modified to taper

Z yarn path changes to accommodate the weave.

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

16

17

18

1 3 5 7 9 11 13 15 17 19 21 23 25 27 29 31

Dent

Number

Pick Columns per inch Picks per column

Warp per dent

Page 35: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

40%

42%

44%

46%

48%

50%

52%

54%

56%

58%

60%

0.000 0.500 1.000 1.500 2.000 2.500

Distance from Thin Edge (in)

FiberVolumeFraction

Calculated

Target

Variation in Fiber Volume Fraction

This variation in yarn packing results in variations in Vf for the resulting composite.

Page 36: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Variation in weave angle

The weave angle will also change throughout the width of the part due to varying warp yarn count and part thickness.

25 °

30 °

35 °

40 °

45 °

50 °

55 °

0.0 0.5 1.0 1.5 2.0 2.5

Distance from Thin Edge (in)

WeaveAngle

Calculated

Target

Page 37: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Yarn Distributions

The distribution of warp, weft, and Z yarn will also vary throughout the part.

15%

20%

25%

30%

35%

40%

45%

50%

55%

60%

0.0 0.5 1.0 1.5 2.0 2.5Distance from Thin Edge (in)

YarnDistribution % Z % Warp % Fill

Page 38: Opportunities and Challenges for Textile Reinforced Composites Christopher M. Pastore Philadelphia University Philadelphia, Pennsylvania, USA.

Variations in Modulus

All mechanical properties will vary throughout the part

0

2

4

6

8

10

12

14

0.0 0.5 1.0 1.5 2.0 2.5

Distance from Thin Edge (in)

TensileModulus(Msi)

E11 E22 E33