Ceramic-based composite material screw, and preparation method thereof
A composite material and ceramic-based technology, applied in the direction of screws, mechanical equipment, threaded fasteners, etc., can solve the problems of polycarbosilane production process complexity, long production cycle, short production cycle, etc., to achieve easy synthesis and collection, equipment Low cost, low cost effect
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[0023] The present invention proposes a method for preparing a ceramic matrix composite screw, such as figure 1 shown, including the following steps:
[0024] (1) Using carbon fiber cloth as a reinforcement, vacuum pretreatment is carried out on the carbon fiber cloth to remove the organic glue on the surface of the carbon fiber;
[0025] Preferably, in the step (1), the temperature for the vacuum pretreatment of the carbon fiber cloth is 1000-1600° C., and the time is 0.5-2 hours;
[0026] Preferably, the thickness of the carbon fiber cloth is 0.20-1.0 mm; the temperature of the vacuum pretreatment is preferably 1400° C., which facilitates the removal of the organic glue on the surface of the carbon fiber.
[0027] (2) The pretreated carbon fiber cloth is laminated to several layers, and the carbon fiber prefabricated part is obtained by needle punching and sewing; the number of layers of carbon fiber cloth can be selected according to actual needs, so that it can be used in...
Embodiment 1
[0042] This embodiment provides a method for preparing a ceramic matrix composite screw, comprising the following steps:
[0043] (1) Use T300-1K carbon fiber cloth as the reinforcement, the thickness of the carbon fiber cloth is 0.200mm, vacuum pretreatment, the pretreatment temperature is 1000 ℃, heat preservation for 1h;
[0044] (2) Laminate the carbon fiber cloth to a predetermined thickness of 10 mm, and suture it with needle punching, and the suture density is 5 mm;
[0045] (3) Using polyoxysilane as a precursor, the carbon fiber preform was vacuum impregnated and cracked in an inert atmosphere. The impregnation time was 6 hours, the cracking temperature was 1000°C, and the dipping and cracking was repeated 6 times to obtain the green body;
[0046] (4) Process the blank into a round bar, and use a diamond grinding wheel for thread processing to form a screw semi-finished product;
[0047] (5) The processed screw semi-finished products are subjected to several vacuum im...
Embodiment 2
[0050] This embodiment provides a method for preparing a ceramic matrix composite screw, comprising the following steps:
[0051] (1) Use T300-3K carbon fiber cloth as reinforcement, the thickness of carbon fiber cloth is 0.25mm, vacuum pretreatment, pretreatment temperature is 1200 ℃, heat preservation 0.5h;
[0052] (2) Laminate the carbon fiber cloth to a predetermined thickness of 8mm, and suture it with needle punching, and the suture density is 10mm;
[0053] (3) Using polyoxysilane as a precursor, the carbon fiber preform was vacuum impregnated and cracked in an inert atmosphere. The dipping time was 4 hours, the cracking temperature was 800°C, and the dipping and cracking was repeated 6 times to obtain the green body;
[0054] (4) Process the blank into a round bar, and use a diamond grinding wheel for thread processing to form a screw semi-finished product;
[0055] (5) The processed screw semi-finished products are subjected to several vacuum impregnation and inert ...
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