Fiber composite and manufacturing method thereof
A technology of fiber composite materials and fibers, which is applied in the field of fiber composite materials with vibration-controlling properties and its manufacturing method, and can solve the problems of overall material rigidity and strength reduction, insufficient vibration-control reduction ratio, etc.
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Embodiment 1
[0050] The preparation procedures and conditions of Embodiment 1 of the present invention (numbering: 4V) are as follows, and each material is described as follows, fiber: carbon fiber (Toray, T700SC, 12K); first / second resin: epoxy resin (Dow Chemical, Epon 828); multilayer carbon nanotubes: A-MWCNT1020, Xinyun Enterprise (accounting for 5wt% of composite resin layer); modified functional group: amine group (according to J.Mater.Chem.,2011,21,7337-7342 Methods). Preparation of a round tubular hollow body Taking the length 450mm X diameter 20mm and thickness 4.0mm as an example, first place 4 strip-shaped composite resin layers (thickness 70±2μm) on the fiber prepreg horizontally at an angle of 0° (θ°) On the cloth layer (thickness 80±2μm) (similar figure 1 shown, but the included angle is 0 degrees), the width L of the strip-shaped composite resin layer 1 The distance L from the plurality of strip-shaped composite resin layers 2 The ratio is 1:4. Then wrap the above-menti...
Embodiment 2
[0052] Embodiment 2 of the present invention (code number: 2V) preparation method and conditions are as described in Embodiment 1, change the width L of the composite resin layer of this strip 1 The distance L from the plurality of strip-shaped composite resin layers 2 The ratio is 1:2.
Embodiment 3
[0054] Embodiment 3 of the present invention (number: 3V) preparation method and condition are as described in embodiment 1, change the width L of the composite resin layer of this strip 1 The distance L from the plurality of strip-shaped composite resin layers 2 The ratio is 1:3.
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