VectorUltraReinforcements – Increasing Shear and Torsional Properties with Carbon Fiber Double Bias Fabrics



C-BX material is manufactured on a LIBA MAX 5 machine.
 
After going through the stitch head, C-BX material is put into roll form.

Carbon fiber reinforced composites are being increasingly used in applications requiring low weight with high strength and stiffness.  In many widely adopted out-of-autoclave (OOA) processes such as vacuum infusion processing (VIP or VARTM) and resin transfer molding (RTM), carbon fiber fabrics are most commonly used for rapid laminate thickness build up.  Traditionally, these fabrics have been woven in nature, either plain, twill, or satin weaves depending on the level of drapeability and properties required for a given application.  However, woven fabrics do impose restrictions such as low composite mechanical properties due to fiber crimping, low stability, and lack of off axis reinforcing options.  In order to improve on these shortcomings, stitch-bonded multiaxial carbon fabrics were developed.

While stitch-bonded carbon fabrics are used successfully as direct replacements for traditional 0°/90° woven versions, this article will concentrate on their use in increasing in-plane off-axis (in this case ±45°) laminate properties.  Stitch-bonded fabrics are ideal for this type of reinforcement, as the “double bias” fabrics provide non-crimped, ±45° aligned fibers directly off of the roll with no skewing required.

Orienting fibers in the ±45° double bias directions are key to strengthening and stiffening laminates against in-plane shear stresses (beam shear webs, etc.) or torsional loading (as seen in driveshafts/torque tubes, etc.).  They are also required orientations for creating “quasi-isotropic” laminates (close to isotropic, meaning the same properties in all directions) which may be required when specific loading conditions are not known.  Below is a comparison of the in-plane shear modulus between 0°/90° glass and standard modulus carbon woven fabric laminates and ±45° double bias stitch-bonded fabrics:

Reinforcement
Type
Fabric Type Matrix Resin Fiber Volume
Ratio -V
(%)
In-Plane Shear
Modulus - Gxy
(Msi)*
E-Glass 7781 - 8-Harness
Satin Weave
5245C Epoxy 45% 0.77
E-Glass E-BX 1200 - ±45 Double
Bias Stitch-Bonded
INF114/210 Epoxy 45% 1.48
SM Carbon AGP370 - 5-Harness
Satin Weave
3501-6S Epoxy 62% 0.94
SM Carbon C-BX 1200 - ±45 Double Bias
Stitch-Bonded
INF114/210 Epoxy 54% 3.86

*Global coordinate system is set by the dry fabric roll dimensions: x - roll length, y - roll width
**Physical and mechanical data or woven composites taken from "Engineering Mechanics of Composite Materials"
I.M. Daniel & O. Ishai - 2nd Edition, Table A.5

As can been seen above, the shear modulus is increased by almost 2 times for the glass laminate when orienting the fibers at ±45°, and over 2.5 times that when switching to carbon fiber, even at slightly to moderately lower fiber volume fractions.

VectorUltra™ carbon fiber double bias reinforcement fabrics are available in a wide variety of areal weights (see table below for standard product listing) to meet any application.

Vector Ultra ™ Carbon Fiber Double Bias Products

Product Code Total Weight 90° ±45°/±60° CSM Veil/Core
Longitudinal Transverse Double Bias Weight Weight
oz/yd2 g/m2 oz/yd2 g/m2 oz/yd2 g/m2 oz/yd2 g/m2 oz/yd2 oz/yd2
C-BX 0300 2.94 100 n/a n/a n/a n/a 2.94 100 n/a n/a
C-BX 0450 4.46 151 n/a n/a n/a n/a 4.46 151 n/a n/a
C-BX 0600 5.94 201 n/a n/a n/a n/a 5.94 201 n/a n/a
C-BX 0900 8.91 302 n/a n/a n/a n/a 8.91 302 n/a n/a
C-BX 1200 11.80 400 n/a n/a n/a n/a 11.80 400 n/a n/a
C-BX 1800 18.37 623 n/a n/a n/a n/a 18.37 623 n/a n/a
C-BX 2400 24.11 818 n/a n/a n/a n/a 24.11 818 n/a n/a

For a complete listing of Vectorply standard products, please reference the standard product booklet or feel free to visit our website www.vectorply.com