| Composite part | A component made by combining two or more distinct materials that remain identifiable in the finished structure. | The combined materials provide properties that a single material may not achieve alone, such as high stiffness at relatively low weight. |
| Reinforcement | Continuous fibers, chopped fibers, fabrics, or other load-bearing elements. | Carries much of the mechanical load and strongly influences tensile strength, stiffness, and directional performance. |
| Matrix | A polymer, metal, or ceramic material that surrounds and supports the reinforcement. | Transfers loads between fibers, maintains the part shape, and protects the reinforcement from environmental damage. |
| Common reinforcement forms | Unidirectional tape, woven fabric, braided structures, chopped strands, and mats. | The form controls fiber alignment, drape, surface coverage, production speed, and the direction of strength. |
| Fiber orientation | Fibers may be aligned at 0°, 90°, or angled orientations such as ±45°. | Orientation determines how efficiently the part carries loads in different directions. A laminate with several angles can provide more balanced performance. |
| Fiber volume fraction | The percentage of the composite volume occupied by reinforcement. Many structural polymer composites use approximately 40%–65% fiber by volume, depending on the process and design. | Higher fiber content can improve stiffness and strength, but excessive content may make wet-out, consolidation, and quality control more difficult. |
| Layup | The planned sequence, orientation, and location of reinforcement layers in a laminate. | A carefully designed layup controls thickness, stiffness, strength, damage tolerance, and resistance to bending or twisting. |
| Mold or tool | A shaped surface or matched set of surfaces used to define the part geometry during forming and curing. | The tool determines dimensional accuracy, surface finish, repeatability, and the achievable production rate. |
| Wet-out or impregnation | The process of distributing matrix material throughout the reinforcement and removing areas that are not properly wetted. | Incomplete impregnation can create voids and weak areas, reducing strength and long-term durability. |
| Consolidation | The application of pressure, vacuum, rollers, or other methods to compact layers and reduce trapped air. | Good consolidation improves interlayer bonding, reduces void content, and helps achieve consistent thickness. |
| Curing or solidification | A chemical reaction or cooling stage that changes the matrix from a workable state into a solid structure. | The cure cycle affects final mechanical properties, dimensional stability, residual stress, and production time. |
| Vacuum bagging | A flexible sealed film is placed over the laminate, and air is removed to apply atmospheric pressure during processing. | It can improve consolidation and reduce trapped air without requiring a fully matched rigid mold. |
| Compression molding | A charge of reinforcement and matrix is placed in a heated mold and compressed until the part forms and cures. | It provides repeatable dimensions and is suitable for producing multiple parts with relatively short cycle times. |
| Resin transfer molding | Dry reinforcement is placed in a closed mold, and liquid resin is injected or drawn through the fibers before curing. | The process can produce complex shapes with controlled surfaces and more consistent resin distribution than many open-mold methods. |
| Filament winding | Resin-coated continuous fibers are wound around a rotating mandrel at controlled angles. | It is effective for cylindrical or rotational parts because fiber paths can be aligned with pressure and hoop loads. |
| Pultrusion | Continuous fibers are pulled through a resin bath and a heated forming die to create a constant cross-section. | It supports efficient continuous production of profiles such as rods, channels, beams, and flat sections. |
| Quality checks | Visual inspection, dimensional measurement, fiber and resin content checks, ultrasonic inspection, and mechanical testing. | Inspection helps identify delamination, porosity, dry areas, cracks, incorrect dimensions, and other defects before service. |
| Typical advantages | Low density, high specific strength, high specific stiffness, corrosion resistance, and design flexibility. | These advantages make composite parts useful where weight reduction, tailored performance, or resistance to harsh environments is important. |
| Typical limitations | Anisotropic behavior, sensitivity to manufacturing defects, more complex repair procedures, and challenges in recycling some thermoset systems. | Material selection and process control must be matched to the expected loads, temperature, moisture, impact, and service life. |