Choosing fiberglass multiaxial fabric affects the laminate design, structural weight, and production efficiency of composite components. Different fiber orientations serve different reinforcement needs, while areal weight, layer construction, and manufacturing processes also influence material performance. The selection process should start with the load requirements of the finished component, followed by the appropriate fabric structure and specifications.
Multiaxial fabric combines layers of fiberglass oriented in different directions and stitches them together into an integrated structure. Common types differ mainly in fiber orientation and layer construction.
If a component primarily carries tensile loads in one direction, prioritize the fiber configuration aligned with that direction. When reinforcement is needed in both longitudinal and transverse directions, a 0°/90° structure may be suitable. For components subject to significant shear or torsional loads, ±45° layers may also be worth evaluating.
▶ In practice, multiple layer orientations are often combined to meet structural requirements. Fiber orientation alone does not determine final performance; the stacking sequence, fiber content, resin system, and component design must also be considered.
Areal weight, expressed in g/m², indicates the mass of fabric per unit area. However, two multiaxial fabrics with the same total areal weight may have different fiber distributions and layer constructions, so they should not automatically be treated as interchangeable.
A higher areal weight does not necessarily mean a better choice. It may reduce the number of plies needed to achieve a target fiber weight, but it can also increase the component's overall weight. The final specification should be consistent with the laminate design and manufacturing requirements.
The performance of a fabric can vary depending on the manufacturing process. In addition to reinforcement requirements, consider how well the resin can impregnate the fibers, how easily the fabric conforms to the mold, and whether the layers remain stable during processing.
Vacuum infusion
Pay attention to resin flow, fiber wet-out, and air removal throughout the laminate.
Resin transfer molding (RTM)
Evaluate fabric permeability, preform stability, and compatibility with the mold.
Hand lay-up
Consider drapability, conformity to complex surfaces, and resin impregnation during manual processing.
The final result also depends on resin viscosity, stacking sequence, compaction, mold design, and process parameters. For complex components or applications with demanding load requirements, trial production or relevant testing can help verify material suitability.
When requesting a quotation or confirming a product grade, providing clear requirements makes it easier to identify a suitable material. The following details should be checked:
▶ For composite structures such as wind turbine blades, marine hulls, and industrial components, fabric specifications should also align with the design loads and laminate calculations. If standard products do not meet the requirements, customized fiber configurations, areal weights, and widths may be considered.