In the design of carbon fiber composite tubular graphite heat exchangers, mechanical factors are the core elements determining their performance and reliability. Carbon fiber composites, with their lightweight, high strength, corrosion resistance, and controllable thermal conductivity, are ideal reinforcing materials for carbon fiber composite tubular graphite heat exchangers. However, their anisotropy, interfacial bonding state, and differences in molding processes require comprehensive consideration of multiple mechanical factors during the design process.
The alignment of carbon fibers directly affects the mechanical properties of the composite material. Carbon fiber composites are typical anisotropic materials; their tensile strength along the fiber axis can reach 6-12 times that of steel, while the strength perpendicular to the fiber direction is significantly reduced. In carbon fiber composite tubular graphite heat exchangers, if the fiber direction is inconsistent with the fluid flow direction, it may lead to localized stress concentration and microcrack propagation. For example, when the fluid impact force is perpendicular to the fiber direction, the interlaminar shear strength is low (typically only 50%-70% of the matrix resin strength), easily causing interfacial debonding. Therefore, during the design phase, the fiber layup direction needs to be optimized based on fluid dynamics analysis. For example, circumferential winding can be used in the inner layer of the pipe wall to enhance resistance to internal pressure, while axial winding can be used in the outer layer to improve bending stiffness.
Interfacial bonding strength is crucial to the mechanical properties of composite materials. The interfacial bonding state between carbon fiber and the graphite matrix directly affects stress transfer efficiency. If the interfacial bonding is weak, the fiber and matrix are prone to slippage under external loads, leading to a decrease in the overall strength of the composite material. For example, in high-temperature or corrosive media environments, the interface may weaken due to thermal stress or chemical erosion, resulting in delamination failure. During the design phase, surface treatment techniques (such as plasma treatment and silane coupling agent coating) should be used to enhance the chemical bonding between the fiber and the matrix, while optimizing molding process parameters (such as temperature and pressure) to reduce interfacial defects.
The molding process has a decisive influence on the mechanical properties of composite materials. Different molding methods (such as winding, compression molding, and pultrusion) will lead to differences in fiber volume fraction, porosity, and residual stress distribution. For example, in the filament winding process, improper fiber tension control may lead to localized fiber accumulation or loosening, resulting in uneven strength; in the compression molding process, uneven pressure distribution can easily cause warping and deformation of the product. Strict parameter control standards must be established in conjunction with the process characteristics during the design phase. For example, fiber tension can be adjusted in real time through an online monitoring system, or a segmented temperature-curing process can be used to reduce residual stress.
The dynamic influence of ambient temperature and load conditions on the mechanical properties of composite materials cannot be ignored. Carbon fiber composites may experience matrix softening at high temperatures, leading to a decrease in shear modulus; while in low-temperature environments, matrix brittleness increases, weakening impact resistance. Furthermore, dynamic loads (such as fluid pulsation and vibration) may induce fatigue damage, especially at interfaces, which are prone to becoming fatigue crack initiation sites. During the design phase, thermodynamic simulation analysis should be used to evaluate the performance degradation law of the material at different temperatures, and fatigue life prediction models should be used to optimize the structural thickness and layup sequence.
The coupling effect of fluid dynamics and structure must be incorporated into the design considerations. In tubular heat exchangers, the pressure distribution, turbulence intensity, and vibration frequency generated by fluid flow will dynamically interact with the tube wall structure. For example, high-speed fluids may create turbulent vortices locally on the pipe wall, causing vibration acceleration to exceed the fatigue limit of the composite material; while fluid pressure fluctuations may trigger pipe wall buckling instability. During design, fluid-structure interaction simulations should be used to optimize the pipe diameter-to-wall thickness ratio, and flow guiding devices should be added to reduce turbulence intensity.
Performance degradation mechanisms under long-term service conditions need to be prevented in advance. Carbon fiber composites may experience matrix aging, fiber oxidation, and interface weakening under long-term thermo-mechanical coupling. For example, oxidizing media may corrode the carbon fiber surface, leading to a decrease in strength; while ultraviolet radiation may cause yellowing and embrittlement of the matrix resin. Weather-resistant matrix materials (such as bisphenol A epoxy resin) should be selected during design, and surface coating technology should be used to isolate environmental corrosion.
The design of carbon fiber composite tubular graphite heat exchangers should focus on mechanical properties, constructing a complete mechanical protection system covering materials, structure, process, and environment through fiber orientation optimization, interface strengthening, process control, environmental adaptability design, and fluid-structure interaction analysis. This process requires not only a deep understanding of the multi-scale mechanical behavior of composite materials, but also customized design based on specific operating conditions, ultimately achieving long-term stable operation of the heat exchanger in complex service environments.