All composite parts are not flat – so why should all composite fabric be flat? At Textum we realize that composite parts take many different shapes and sizes. That’s why we have worked diligently over the years to develop specialty and 3D textiles in addition to our focus on flat fabrics. Textum holds exclusive rights to multiple US and foreign patents covering 3D and shaped fabrics. Our capabilities include helical fabrics, tubular fabrics, braided fabrics and preforms such as I-beams, T-shapes, X-shapes, etc. These fabrics can be manufactured with essentially any material that can be presented in yarn form; however, the most typical yarns used include carbon fiber, fiberglass and aramid.

Previously, when a manufacturer needed to produce circular textile patterns for reinforcing a disk shape they were limited to a couple of methods. One was to cut circular shapes from 0/90 broad fabric. The second was to cut wedge shaped patterns from broad fabric and lay up these segments (this second method was usually done with prepreg). In both methods the fabric waste can exceed 50% due to cutting losses. In the second method, there was the additional cost of excessive labor associated with the lay-up process. Textum’s technology allows for continuous helical fabrics thus overcoming both of these drawbacks with other benefits to include:

  • These fabrics can be produced in a continuous helix form with tailorable ID and OD dimensions. This allows for near net shape, circular fabrics resulting in a significant waste reduction.
  • Fiber orientations can include hoop yarns, radial yarns and yarns oriented in a plus/minus direction in the hoop – radial plane, e.g. +/- 45 degrees.
  • Fiber fractions in each of the directions selected can be tailored over a wide range and in such a manner as to maintain a constant relationship from ID to OD. This also creates a relatively constant ply thickness from ID to OD which is important if multiple turns of the helical fabric are required to form the desired disk thickness.
  • Current tooling can produce helix wall thicknesses up to 7 inches wide, (OD-ID)/2. With tooling and minor machine modifications this dimension is highly adjustable.
  • The resulting fiber architecture is non-crimp which is to say that the different fiber directions do not interlace as in traditional fabrics. This allows for better translation of fiber properties in the resulting composite structure.
  • The technology has been designed to be relatively high speed to allow for high volume production and low cost benefits.
Helical Fabric

Textum’s 3-D weaving technology allows for fabrics to be woven to a specific width, length and thickness with three directions of fiber orientation. Multiple designs are possible and they generally vary in the orientation of through thickness fibers, yarn spacing and the concentration of fiber in each weave direction. In most cases, the in-plane fibers do not interlace with each other but instead are layers of 0/90 fabric which are “stacked” on each other and held in place by through thickness (or Z direction) fibers.
These multi-layer fabrics are woven in such a way that the through thickness yarns can be used for inter-laminar property enhancement. These fabrics can be woven up to 130 inches wide. The number of fabric layers that are “stacked” on each other depends on the weave architecture selected but typically range from 3 to 18. These fabrics fall into three categories due to the manner in which the through thickness yarns are configured:



Through thickness yarns are generally at ~ 90 degree orientation to the in-plane fiber layers.

Angle Interlock

All warp direction yarns traverse fully from the top surface to the bottom surface in a repeating, sinusoidal fashion. The warp yarns form a +/- fiber architecture in the warp / through thickness plane.


Adjacent Ply Interlock

Selected yarns from each fabric layer periodically interlace with an adjacent fabric layer, above and or below. There will not be any through thickness yarns that fully traverse the thickness.

The fiber fraction in all fiber directions can be tailored with a wide degree of design flexibility. The ultimate thickness achievable will depend on the yarn denier used and the number of layers selected.

When designing and manufacturing composite components the less complicated the laminate schedule the better. Textum is an industry leader in manufacturing composite preforms and near net shape preforms by integrally weaving 3 dimensional structures. These shapes can be woven as integrated, single layer fabrics or as multi-layer fabrics. Shapes such as truss core structures, I-beams, T-beams, hat stiffeners and pi sections are examples of shapes that are possible. An example of this technology is Textum’s triangular cross section gap filler (see image to the right). Used when laminating 2-D fabrics into an I-beam or T-beam this component not only fills empty space to avoid resin rich pockets, it also helps transfer loads between the intersecting planes of fabric. Textum has significant experience with multiple yarn types and our engineers can work with your team to determine the ideal yarn spacing, yarn distribution and various design options that are optimal for your specific application.


Tubular fabrics have many applications.  Tubular fabrics are used in pipe repair, permanent bridge construction and repair, temporary bridges, temporary structures for military uses or civilian disaster relief as well as many other civil engineering applications.  Tubular fabrics are also used frequently in aerospace applications from structural components to gaskets.  The uses for tubular fabrics are about as limited as your imagination.

In the past, tubular fabrics have typically been produced using braiding machines. This is an acceptable method for some uses; however, braiding machines are typically limited to a fiber orientation of +/- 45 degrees or 60 degrees. Unlike braided fabrics, Textum’s unique woven tubular fabrics have fibers oriented 0/90 degrees offering exceptional hoop strength along the entire length of the fabric.

Additionally, these fabrics can be shaped on loom to accommodate our customer’s specific applications. A wide variety of shapes and sizes are possible. For example, a curved seamless tube can be woven to set inner and outer diameters. The tube can be constructed in such a way that it will conform to a selected diameter if inflated. Additionally, half tube or curved “U” shaped fabrics can be woven. An example application for this fabric would be a fan blade containment shroud on a jet engine. Textum’s unique tubular weaving technology allows for fabrics to be woven with specific predetermined shapes to their cross section allowing for a close fit to an irregular shaped mandrel.

Contact Textum today and let our engineers help you design a tubular fabric for your specific application.


Needle Punching

Textum specializes in designing and developing needle punched materials and needling processes for carbon fiber and certain ceramic fiber textile preforms. During this process, random or specifically oriented in-plane filaments throughout the preform are redirected through the preform thickness thus increasing the fiber volume in the through thickness (Z direction). The increase in Z direction fiber volume can aide in interlaminar preform mechanical properties, through thickness thermal conductivity and other fiber dominated properties. The Z direction fiber volume fraction can be controlled by the frequency of needling which is expressed as PPSI, penetrations per square inch. Contact us today to learn more about our needling capabilities.


Textum offers in-house sewing services and stitched products for 3-D reinforced composite applications and stitched laminations for flexible insulation products. In the case for composite applications, the stitches will provide improved through thickness reinforcement. Sewing is an excellent way to build near net shape preforms utilizing, for example, standard 2D fabrics in the in-plane directions. Textum has experience weaving a variety of materials including carbon fibers, ceramic fibers and various metal wires and virtually any material available in fiber form. Applications for stitched laminates include thermal insulations and blankets for applications up to 2000 degrees F and higher for short term exposures. Contact us today to learn more about our composite sewing capabilities.