The product uses imported CYCOM 890RTM aviation-grade epoxy resin matrix, which perfectly infiltrates with T700 carbon fiber to ensure that the fiber-matrix interface bonding strength reaches level of the industry. The volatile content is controlled within 0.5%, avoiding air hole defects during the molding process. It has passed the AS9100 aerospace quality management system certification, strictly follows aviation material standards, and has stable batch consistency. It is suitable for mainstream aviation molding processes such as autoclave and RTM, and can be processed into high-precision components such as wing skins, fuselage frames and satellite structural components, greatly reducing the overall weight of components and improving structural strength and durability, solving the industry pain points of high density and long processing cycle of traditional aviation metal materials.
After curing, the tensile strength is 4900MPa and the tensile modulus is 230GPa. The thickness tolerance is controlled within ±0.01mm, with a standard width of 1000mm and custom special width available. The storage condition is -18℃ low-temperature frozen environment, with a valid storage period of 12 months. The curing process parameters are: preheating temperature 80℃, pressurization pressure 0.4-0.6MPa, curing temperature 120-180℃, holding time 60-90min. It has excellent chemical resistance and can resist most aviation fuel and hydraulic oil corrosion.
It is mainly used in scenarios such as aerospace wing skins, main fuselage load-bearing frames, satellite antenna brackets and military drone structural components. It can also be used for processing high-precision components of high-end sports competition equipment, meeting the strict quality requirements of aerospace materials and helping customers achieve lightweight and high-strength product design goals.
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