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54results about How to "Good physical and chemical compatibility" patented technology

Preparation method of inorganic composite coating on the surface of quartz fiber reinforced quartz matrix composite material

The invention which belongs to the technical field of special functional ceramic materials relates to a preparation method of an inorganic composite coating on the surface of a silica fiber-reinforced silica-based composite material. The preparation method comprises procedures of surface treatment, coating slurry preparation, spray, thermal treatment, and coating with a material for modification,wherein the temperature of the thermal treatment is 500-650DEG C. According to the invention, a solid phase reaction is carried out on three substances of lithium carbonate, aluminum hydroxide, and silica when being calcined, and a low expansion ceramic material is prepared by controlling the ratio among the three substances; a borate or a phosphate and the like are simultaneously introduced to prepare a low temperature flux to reduce the melting temperature of the integral body of the low expansion ceramic material; and a solidification hydrolysis reaction is finally carried out on an inorganic silicone resin to form a compact protection layer on the surface of a transition layer to reach effects of modification and double layer protection. The preparation method of the invention is scientific and reasonable, and is easy to implement, the material of the inorganic composite coating obtained with the preparation method has a good moistureproof performance, and has a good physicochemical match with the silica fiber-reinforced silica-based composite material, and simultaneously can improve dielectric properties of the silica fiber-reinforced silica-based composite material.
Owner:ZHONGCAI HIGH NEW MATERIAL +1

Super-light functional master batch, plastic product based on super-light functional master batch and method for preparing plastic product through rotational molding

The invention discloses a super-light functional master batch, which is prepared from the following components in ratio: 20-70 parts of resin, 10-50 parts of fillers, 5-20 parts of a viscosity adjusting auxiliary, 5-50 parts of a functional auxiliary, 0.1-1 part of a processing thermal stabilizer and 0.1-2 parts of a processing lubricant, wherein the resin is PP, ABS or PA; the fillers are hollow glass beads or phenolic beads; the invention further discloses a plastic product prepared from 40-60 parts of matrix plastic and 20-30 parts of super-light functional master batch; the invention further discloses a method for preparing the functional plastic through rotational molding after the matrix plastic and the functional master batch are heated to a molten/half molten state. According to the invention, after the matrix plastic and the functional master batch are heated to a certain temperature and the rotational molding is carried out, and under the effect of the centrifugal force, the matrix plastic moves towards an outer layer, so that the selective distribution of the functional auxiliary is achieved; the dosage of the functional auxiliary can be reduced and the performance of the products is improved.
Owner:重庆科聚孚新材料有限责任公司 +1

Repairing agent and repairing method for surface damage of silicon carbide ceramic matrix composite material

The invention relates to a repairing agent and a repairing method for surface damage of a silicon carbide ceramic matrix composite material. According to the invention, solid polycarbosilane, dimethylbenzene, zirconium carbide powder, silicon carbide powder and silicon carbide whiskers in a reasonable ratio form a liquid substance with moderate viscosity. The chemical components of the repairing agent can quickly form a repairing layer having good physical and chemical compatibility with the silicon carbide ceramic matrix composite material in a natural environment. The preparation and construction processes of the repairing agent can be operated on line on the site of a damaged component. After the repairing agent is used for repairing surface damage, a repairing layer having good physical and chemical compatibility with a silicon carbide ceramic matrix composite body can be formed in a damaged area, and the repairing agent is high in bonding strength and high in temperature resistance. Through reasonable repair process parameters and matching of solid polycarbosilane, xylene, zirconium carbide powder, silicon carbide powder and silicon carbide whiskers in the reasonable ratio, the use temperature range of the repairing layer is -120 to 1400 DEG C, and the use temperature can reach 1650 DEG C in a short time.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Method for preparing carbon/carbon composite material nanometer silicon carbide-mullite composite external coating

InactiveCN101838157BImprove high temperature oxidation resistanceImprove oxidation protection abilityCarbon compositesThermal dilatation
The invention provides a method for preparing carbon / carbon composite material nanometer silicon carbide-mullite composite external coating. The method comprises the following steps: adding mullite powder and nanometer silicon carbide powder into isopropanol for ultrasonic oscillation, adding iodine into the mixture for another ultrasonic oscillation, and placing the mixture in a hydrothermal reaction kettle; clamping the carbon / carbon composite material test sample with SiC internal coating on a cathode clip in the hydrothermal kettle for hydrothermal electrophoresis reaction, taking out anddrying the test sample to obtain the carbon / carbon composite material nanometer silicon carbide-mullite composite external coating. The mullite adopted as the C / C-SiC external coating has higher thermal stability and oxidation resistance, and has melting point more than 1,800 DEG C. The coefficient of thermal expansion of the mullite is close to that of the SiC, so the mullite cannot generate thermal stress at high temperature. The mullite can generate SiO2 and Al2O3 with low penetration and excellent high-temperature stability with oxygen at high temperature, additionally; nanometer silicon carbide particles can effectively overcome microcrack and other defects of the SiC internal coating, so that the high-temperature oxidation resistance of the coating can be greatly improved.
Owner:SHAANXI UNIV OF SCI & TECH

Ceramic matrix composite turbine guide blade with turbulent flow structures and preparation method thereof

The invention discloses a ceramic matrix composite turbine guide blade with turbulent flow structures and a preparation method thereof. An inner cavity of the guide blade is provided with a plurality of columnar turbulent flow structures penetrating through a blade basin and a blade back, and the guide blade is made of a ceramic matrix composite. The invention further provides the preparation method of the blade. The preparation method comprises the following steps that a mold with vent holes is prepared firstly, then a fiber preform is prepared according to the mold, an interface layer and a ceramic matrix are sequentially deposited, after the mold is removed, the guide blade is machined to the design size, then through holes perpendicular to the blade profile are prepared in the turbulent flow column parts of a prepared blade body shell, then pins are inserted into the through holes, then a prepared assembly is connected in a homogeneous mode, and after machining and repairing, the ceramic matrix composite turbine guide blade with the turbulent flow structures is obtained. The temperature resistance of the guide blade prepared through the method is greatly improved, meanwhile, the structural weight is remarkably reduced, and the precision of the profile and the size and the cooling effect of the guide blade can be guaranteed.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Method for preparing high-entropy reinforced amorphous alloy composite material

The invention belongs to the technical field of amorphous alloy preparation, and relates to a method for preparing a high-entropy reinforced amorphous alloy composite material. The method comprises the following steps that amorphous alloy powder and high-melting-point high-entropy alloy powder with high toughness are evenly mixed according to a designed volume fraction, the mixed powder is conveyed out through airflow with supersonic speed, and the mixed powder and a laser focus are converged at a position 2-30mm above a deposition substrate; the amorphous alloy powder is heated to be in a molten state through laser suspension, meanwhile, the amorphous alloy powder is blown and cooled to be in a supercooled liquid state through supersonic airflow in the process of flying to the deposition substrate, an amorphous alloy matrix is deposited on the substrate, the high-entropy alloy powder is kept not molten all the time in the process, and finally, the high-entropy alloy powder is uniformly distributed in amorphous alloy formed by deposition in a reinforced phase form; the melting point of the high-entropy alloy powder is higher than that of the amorphous alloy powder; and an amorphous alloy composite material part without size constraint can be prepared, and the material has the performance advantages of high strength and high toughness.
Owner:AVIC BEIJING INST OF AERONAUTICAL MATERIALS

Preparation method of poly(3,4-ethylenedioxythiophene)/self-doped defect-rich tin oxide nano composite photocatalytic material

The invention relates to a preparation method of a poly(3,4-ethylenedioxythiophene)/self-doped defect-rich tin oxide nano composite photocatalytic material. A self-doped defect-rich tin oxide heterojunction material is loaded and dispersed on PETOT in a chemical bond complexing form to obtain the nano composite material; and the self-doped defect-rich tin oxide is selected from defect-rich tin oxide SnO2-x consisting of Sn-doped nonstoichiometric or mixed valent tin oxides. The electron-hole separation can be facilitated by utilizing the visible light responsive oxidation and reduction capacity of the self-doped defect-rich tin oxide heterojunction material, conductivity and hole transport capacity of PETOT as well as the chemical bonding heterojunction structure among different components, so that the excellent photocatalytic performance can be achieved. Meanwhile, the easy-to-mold characteristic of polypyrrole can effectively avoid the recycling difficulty of the powder material, sothat the poly(3,4-ethylenedioxythiophene)/self-doped defect-rich tin oxide heterojunction nano composite material is a novel environment-friendly photocatalytic material convenient to recycle.
Owner:PINGDINGSHAN UNIVERSITY

Preparation method of poly(3-hexylthiophene)/self-doped defect-riched tin oxide heterojunction nano composite photocatalytic material

The invention discloses a preparation method of poly(3-hexylthiophene)/self-doped defect-riched tin oxide heterojunction nano composite photocatalytic material. According to the method, a nano composite material is obtained by loading and dispersing a self-doped defect-riched tin oxide heterojunction material in P3HT in the form of chemical bond complexation; wherein the self-doped defect-riched tin oxide is selected from Sn-doped non-stoichiometric or defect-riched tin oxide SnO2-x composed of mixed valence state of tin oxide; according to the invention, the visible light photocatalytic redoxproperties of self-doped defect-riched tin oxide, the electrical conductivity of poly(3-hexylthiophene), the catalytic capacity of visible light and a heterojunction structure with chemical bonding among different components are utilized to fully inhibit photo-generated electrons-hole recombination of the nano composite photocatalytic material in a photocatalytic reaction, so that the improvements on the performance of photocatalytic redox degradation of pollutants and photocatalytic decomposition of hydrogen produced by water of the nano composite photocatalytic material are facilitated. Atthe same time, the characteristics of being easy to be molded of poly(3-hexylthiophene) can effectively avoid the problem of difficulty in recovery of powder materials.
Owner:PINGDINGSHAN UNIVERSITY
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