Method for preparing chopped carbon fiber reinforced amorphous composite material and a device thereof

A technology of amorphous composite material and chopped carbon fiber, which is applied in the field of preparation of chopped carbon fiber reinforced amorphous composite material, can solve the problems of fast cooling speed, poor wettability, low cooling rate, etc., and achieves small negative damage and improved Wetting property, effect of improving wettability

A technology of amorphous composite material and chopped carbon fiber, which is applied in the field of preparation of chopped carbon fiber reinforced amorphous composite material, can solve the problems of fast cooling speed, poor wettability, low cooling rate, etc., and achieves small negative damage and improved Wetting property, effect of improving wettability

CN112553546AActive Publication Date: 2021-03-26HEBEI UNIV OF TECH

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  • Method for preparing chopped carbon fiber reinforced amorphous composite material and a device thereof
  • Method for preparing chopped carbon fiber reinforced amorphous composite material and a device thereof
  • Method for preparing chopped carbon fiber reinforced amorphous composite material and a device thereof

Examples

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Effect test

preparation example Construction

[0043] figure 1The illustrated embodiment shows that the components of the device used in the preparation method of the chopped carbon fiber reinforced amorphous composite material include: an air inlet 1, a closed high vacuum induction heating spray casting furnace body 2, a thick tube with a A quartz tube with a diameter of 0.5 mm to 2 mm nozzle 3, a water-cooled induction heating coil 4, high-temperature cement 6, a split copper mold with an inner cavity diameter of 2 mm to 30 mm 8, and a closed furnace body 2. The outlet is connected to the valve 9 of the vacuum system; the connection mode of each component of the device is: the split copper mold 8 is placed in the center of the closed furnace body 2, and the water-cooled induction heating coil 4 is arranged on the thick tube of the quartz tube 3 Around the part, the spout part of the quartz tube 3 is in contact with the inner cavity of the split copper mold 8 from the top of the split copper mold 8 and is sealed with high...

Embodiment 1

[0051] The components of the device used in the preparation method of chopped carbon fiber reinforced amorphous composite materials include: air inlet 1, a closed high vacuum induction heating spray casting furnace body 2, and a thick tube with a diameter of 0.5mm~ Quartz tube with 2mm spout 3, water-cooled induction heating coil 4, high-temperature cement 6, split copper mold with an inner cavity diameter of 2mm to 30mm 8, a closed furnace body 2 with a vacuum system connected to the gas outlet on the lower side Valve 9; the connection mode of each component of the device is: the split copper mold 8 is placed in the central position of the closed body of furnace 2, the water-cooled induction heating coil 4 is arranged around the thick tube part of the quartz tube 3, and the quartz tube The spout part of 3 is in contact with the inner cavity of the split copper mold 8 from the top of the split copper mold 8 and is sealed with high temperature cement 6 to avoid air leakage. The ...

Embodiment 2

[0056] The first step, chopped carbon fiber electroless plating:

[0057] Commercial T800 carbon fiber is used for shearing, and then sieved with a 400-mesh sieve, and the chopped carbon fiber under the sieve is taken to obtain a chopped carbon fiber with a length of 30 μm, and the chopped carbon fiber is subjected to electroless copper plating. The process includes: Pretreatment →Sensitization, activation→reduction→plating, in which the pretreatment uses the burning method and organic solvent immersion, the specific process is 1h in a heating furnace at 420°C, then soaked in acetone for 1h, then ultrasonically cleaned with alcohol for 15min, and dried Then use concentrated nitric acid to soak for 1 hour to roughen, then rinse repeatedly with clean water until all residual nitric acid is removed, and then dehydrate and dry with alcohol; for sensitization and activation, put the roughened carbon fiber into the sensitization-activation solution and mechanically stir for 15 minute...

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Abstract

The invention discloses a method for preparing a chopped carbon fiber reinforced amorphous composite material and a device thereof, and relates to the technical field of forming an amorphous compositematerial by contacting fibers with molten metal and performing rapid solidification. The method adopts a chemical plating method to improve the wettability of the carbon fibers, a carbon fiber preform is prepared through a copper mold, furthermore, the chopped carbon fiber reinforced amorphous composite material is prepared by using a vacuum low-pressure casting method, namely a spray casting method, and the defects that in the prior art, the fiber agglomeration phenomenon caused by non-uniform dispersion of reinforced fibers in a matrix or an interface structure with brittleness equal to that generated by the carbon fibers and the matrix at an interface, the method is only suitable for a traditional magnesium alloy matrix, a high cooling speed cannot be achieved, an amorphous matrix cannot be obtained, and the amorphous composite material cannot be prepared for various amorphous alloy matrixes needing vacuum melting are overcome.

Description

technical field [0001] The technical solution of the present invention relates to the technical field of forming amorphous composite materials through rapid solidification by contacting fibers with molten metal, in particular to the preparation method and device of chopped carbon fiber reinforced amorphous composite materials. Background technique [0002] Due to its high specific strength, high specific modulus and good high temperature performance, carbon fiber reinforced metal matrix composites have attracted widespread attention in many high-tech fields such as automobiles, aviation and aerospace. With the rapid development of aviation technology, the proportion of various carbon fiber composite materials used in the manufacture of new passenger aircraft is increasing, showing attractive development prospects. Traditional carbon fiber reinforced metal matrix composites are mainly based on alloys such as aluminum alloys and magnesium alloys with low density and good plast...

Claims

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Application Information

Patent Timeline
26 Mar 2021
Publication
CN112553546A
IPC
C22C45/10; C22C45/00; C22C49/11; C22C49/10; C22C49/04; C22C49/14; C22C47/04; C22C47/06; C22C47/16; C22C47/18; B22D18/06; B22D18/04; C22C101/10; C22C121/02
CPC
C22C45/10; C22C45/005; C22C49/11; C22C49/10; C22C49/04; C22C49/14; C22C47/04; C22C47/06
Inventors
王新; 尹海龙