“…Traditional matrix resins used in composites, such as epoxy resins and bismaleimide resins, are limited to 150~250 °C, which severely limits the application of composites in high-temperature structures and their components [ 36 , 37 , 38 , 39 ]. Polyimide is one of the best high-temperature-resistant matrix materials in resin-based composites, and its multi-generation products can meet the temperature resistance requirement of 300~500 °C, which is currently mainly used in the advanced field of high-temperature-resistant structural components in aircraft [ 40 , 41 ]. The main difference between polyimide composites and traditional composites is that their interface is formed under high-temperature and high-pressure conditions (300~400 °C), which makes the interface formation mode between the polyimide resin matrix and carbon fiber, the interface bond strength, the stress distribution state between the carbon fiber and matrix, etc., significantly different from those of epoxy and bismaleimide resin matrix composites [ 41 , 42 ].…”