Preparation method of carbon fiber composite hollow blade
A hollow blade and composite material technology, applied in the field of parts processing, can solve problems such as low efficiency, poor corrosion resistance, and high cost
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[0030] The invention provides a method for preparing a carbon fiber composite hollow blade, comprising the following steps:
[0031] (1) Wrap thermoplastic material on the surface of the resin-based composite material to prepare the core mold of the hollow blade mold to be processed, and lay the carbon fiber fabric prepreg on the surface of the core mold to form the first layer; the carbon fiber fabric prepreg Lay on the base mold of the hollow blade mold to be processed to form the second layer; lay the carbon fiber fabric prepreg on the upper cover mold of the hollow blade mold to be processed to form the third layer; lay the first layer The mandrel is positioned on the base mold with the second ply in contact with one side of the first ply; a sealing ring is placed along the edge of the base mold, after which the third ply will be laid The upper cover plate mold is reversed and assembled on the base mold with the second laying layer, and the third laying layer is in contact...
Embodiment 1
[0052] refer to Figure 6 The process shown to prepare carbon fiber composite hollow blades includes the following steps:
[0053] Step S102: The hollow blade mold to be processed includes an upper cover mold 40, a base mold 20, a core mold 10 disposed between the upper cover mold 40 and the base mold 20, and an end cap disposed at one end of the core mold 10 11; wherein, the core mold 10 is formed by wrapping a thermoplastic material on the surface of a resin-based composite material, and the resin-based composite material is a composite material of Toray T300 carbon fiber and modified epoxy resin (TG temperature<100°C), The thermoplastic material is polyphenylene sulfide (PPS); the materials of the upper cover mold 40, the base mold 20 and the end cap 11 are all stainless steel;
[0054] Lay 20 layers of carbon fiber fabric prepreg (Toray T300 carbon fiber prepreg, the TG temperature of the epoxy resin contained therein is 135° C.) laminated on the surface of the core mold ...
Embodiment 2
[0062] refer to Figure 8 The process shown to prepare carbon fiber composite hollow blades differs from that of Example 1 in that step S102 includes the following sub-steps:
[0063] Sub-step S1021: cleaning the surface of the core mold 10 of the hollow blade mold to be processed, and then laying a release cloth (specifically tetrafluoroethylene release cloth); the base mold 20 and the upper cover mold 40 of the hollow blade mold to be processed Cleaning, followed by application of release agent;
[0064] Sub-step S1022: use a laser projector to lay carbon fiber fabric prepreg on the surface of the core mold 10 to form a first layer; place the core mold 10 with the first layer in a vacuum bag, and then extract the vacuum bag gas to degas the first ply and compact the first ply;
[0065] Sub-step S1023: use a laser projector to lay carbon fiber fabric prepreg on the base mold 20 to form a second layup; place the base mold 20 with the second layup in a vacuum bag, and then ex...
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