This capability limit of components is a question that designers of carbon fiber sandwich structures need to consider. Laminate structure Laminate structure is the key to the design of carbon fiber sandwich structure. The mechanical properties of a single-layer material composed of a matrix and a reinforcing material are determined by the mechanical properties of the component materials, the phase geometry (the shape, distribution, and content of each phase material) and the properties of the interface zone.
Fatigue and impact damage. Compared with metal materials, the fatigue of composite materials must consider factors such as temperature, humidity, and impact damage. Mechanical connection is suitable for situations where the thickness of the connecting piece is large, the reliability requirements are high, and the large concentrated load is transmitted.Five major structural design points of carbon fiber composite materials: Carbon fiber sandwich structure composite materials replace traditional metal materials, especially in the manufacture of important structural components.
Hybrid connection is a combination of cementation and mechanical connection, which can improve anti-peeling, impact resistance, fatigue resistance, creep resistance and other properties. In most cases, impact damage covers fatigue issues in the structural design. Under the action of external load, the components have the ability to resist deformation and damage, but this ability is limited. For some frame structural parts, if the layer is not uniform, it will also cause warpage instability, so pay special attention in the manufacturing process. polymethacrylimide Suppliers The mechanical properties of a laminated body made of single-layer materials are determined by the mechanical properties of the single-layer materials and the layering geometry (the thickness of each single layer, the laying direction, and the layering sequence).
If the connection between the parts is required, the connection form needs to be designed. However, the factors that determine the strength and rigidity of composite materials are not only related to the types of fibers and resins, but also related to the layering direction of carbon fibers and the combination of layers. Gluing is mainly the use of adhesives to connect parts into an inseparable whole. Therefore, when designing carbon fiber sandwich structural components, the mechanical properties of the three-level structure need to be considered. How to transfer the excellent performance of single-layer structure to composite structural components, and the layer structure plays a role in connecting the past and the next.