By Mark Harries, Bally Ribbon Mills
Three-dimensional (3-D) weaving of composite fabrics can produce complex, single-piece structures that are strong and lightweight. Compared to traditional two-dimensional (2-D) fabrics, 3-D weaving reduces weight, eliminates the delamination often experienced with 2-D fabrics, reduces crack risks, and lowers production time. 3-D fabrics also offer direct and indirect manufacturing and operational cost reductions.
What is 3-D weaving?
Most fabrics are woven in two dimensions – the X axis (length) and the Y axis (width). 3-D woven fabrics include weaving through the thickness, or the Z axis. This produces complex, single-piece structures.
Looms are the primary tool for weaving fabrics. Nearly as old as civilization itself, looms are ideal machines for weaving 2-D fabrics, including webbing, straps, belts, and tapes. However, they cannot weave 3-D fabrics without extensive tooling.
In 1991, Bally Ribbon Mills (BRM) received a research contract from the United States Air Force Research Laboratory that started the company on the path to developing the requisite technology for 3-D weaving. The experience gained from researching and ultimately building the first fully automated 3-D bias loom, gave BRM the knowledge and experience to develop other 3-D woven composites, including: orthogonal panels, thermal protection systems, near-net-shape, and complex net shape preforms for the aerospace, automotive, construction, military, and safety industries.
Benefits of 3-D weaving
3-D weaving is an emerging technology that offers a variety of benefits over both 2-D composite production and more traditional building materials, like steel and aluminum. The key benefits include weight reduction, elimination of delamination, reduced crack risk, lower production time, and cost reduction.
Weight reduction
3-D woven composites are drastically lighter than metal structures. This is particularly relevant to the aerospace industry. Every pound of weight saved from an aircraft is estimated to save the aircraft’s operator roughly $1 million in operating expenses, primarily fuel, over that aircraft’s lifetime. Smart utilization of 3-D woven composite structures in aircraft design can reduce the weight of an aircraft by up to 30 percent, resulting in considerable operational cost savings.
Elimination of delamination
Delamination occurs when two or more layers of a 2-D woven composite come apart, or delaminate, from each other. Delamination undermines the strength and reliability of the part, which must be replaced to prevent damage and severe safety issues. Delamination is the primary cause of damage to 2-D laminated composites.
3-D weaving produces near-net-shape composite structures that are fully interconnected by their yarn, as opposed to 2-D composites which include a number of different layers of materials artificially bonded together. This means there is no risk of delamination in 3-D woven composites, ensuring they retain strength and reliability.
Reduced crack risk
2-D laminated composites are prone to cracking, especially in structures with bends, such as T-shaped structures. Due to curvature limitations in the layers, many 2-D shapes have considerable gaps in joints and intersections. These spaces and pockets are often filled with resin, which can crack.
3-D woven composites, even in complex shapes, have no empty pockets, as their structural integrity extends along all three axes. Crack rates in 3-D woven composites are therefore far lower than in 2-D laminated composites.
Lower production times
2-D composite production is a long and precise process. Numerous layers of 2-D material are woven, either individually or in larger format and then cut to size. These layers are then pre-impregnated with certain resins, making them what are known as “prepreg” materials. These materials are then stacked and shaped into the requisite form in a process known as plying. Plying is often done by hand and is expensive and extremely time consuming. The layers are then laminated together in shape by infusion with additional resins – some processes and structures even require the material layers to be stitched together prior to lamination. Finally, the structure is set for a period of time, during which the resins cure.
After the structures are properly cured, further machining is required to form a finished product. Required secondary machining processes can include cutting, scraping, sanding, deburring, and drilling.
By contrast, 3-D weaving of composite structures is simpler, faster, and more cost efficient. Similar to 2-D looms, 3-D weaving looms weave weft and warp yarns along the X and Y axis. The difference in a 3-D loom is that instead of the fabric continuing along the Y axis, it builds upon itself vertically – weft and warp yarns are not only woven together on one plane, but one plane is woven together with the next.
Aside from designing a 3-D weave, which requires highly skilled design engineers, the 3-D weaving process is fully automated and results in net shape or near net shape parts. This dramatically reduces manufacturing time despite the increased complexity of the 3-D weaving process.
By weaving entire structures in 3-D, the slow and costly plying process – the longest and most costly portion of manufacturing a 2-D laminated composite structure – is completely eliminated, significantly speeding production and lowering cost.
Cost
Utilizing 3-D woven composite structures in place of traditional metal or 2-D laminated composites can provide cost savings through both the manufacturing process and the product’s operational lifetime. Automated 3-D weaving technology and near net shape capabilities reduce direct labor and secondary machining costs.
Indirect cost savings result from operational cost savings, for example reduced fuel. In addition, because 3-D woven composites are stronger, more resilient, and less prone to breakage than 2-D laminated composites, they can be replaced much less often, reducing replacement and maintenance costs.
Examples of 3-D weaving applications
Using polymer composites within aircraft engines has long been a challenge, thanks to the high temperatures and complex geometries involved in aircraft engine manufacture. Polymer composites are desirable, though, because as stated above, the aviation industry is constantly looking to reduce aircraft weight and increase fuel efficiency. Replacing traditional titanium components with carbon fiber composites in large engine parts serves to reduce weight, as these composite components are significantly lighter than comparable components in metal. In addition, composite engine parts reduce the noise level of an aircraft engine.
3D weaving has been particularly successful in advancing aviation heat shield technology. Thermal protection systems (TPS) are mission-critical components in space exploration vehicles. The ability to vary yarn types, density, thickness, and width, as well as resin type, allows for the creation of a fully customizable TPS to fit specific mission needs. Quartz compression pads, for example, have been woven by BRM for the Orion capsule in order to ensure structural strength during launch and heat resistance during re-entry. Additionally, NASA’s Heatshield for Extreme Entry Environment Technology (HEEET) program is developing a carbon TPS for extreme entries, intended to be capable of surviving the challenging environments of Saturn or Venus. Both these technologies are being developed through extensive additional research, but both rely on the basic principles and strengths of 3-D weaving.
Along with thick panels and engine parts, 3-D woven components also function well in joining two structures together. Because of the nature of the 3-D weave, strength and support is translated in all 3 dimensions, thus enabling the join to reinforce the strength along the load paths of the sub-structures being joined together. These 3-D woven shapes for joining can be tailored to suit the architecture of the structure itself, as well as the sub-components being joined.
Replacing traditional metal or 2-D composites provides benefits
Utilizing 3-D woven composite structures in place of traditional metal or 2-D laminated composites can provide cost savings through both the manufacturing process and a product’s operational lifetime.
