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122results about How to "High strength retention" patented technology

High-adhesive one-component deoximation type room-temperature vulcanized silicone rubber sealant and preparation method thereof

The invention discloses a high-adhesive one-component deoximation type room-temperature vulcanized silicone rubber sealant comprising the following components from (A) to (F) in parts by weight: 100 parts of modified alpha, omega-dihydroxylpolydimethylsiloxane (A), 10-30 parts of dimethyl silicon oil (B), 7-12 parts of deketoxime crosslinking agent (C), 1-5 parts of silane coupling agent (D), 50-150 parts of reinforcing filler (E) and 0.1-1 part of catalyst (F). Compared with the traditional deoximation type sealant, the sealant has excellent adhesive property particularly for some substrates such as plastics, modified resin and the like which are difficultly adhered by using an organic silicon adhesive and can be widely applied to adhesion and sealing of industries such as electronics, automobiles, household appliances and the like. Modified polydimethylsiloxane is used as a basic polymer in deoximation type silicon rubber, so that the sealant has relatively proper surface drying time, provides more reasonable operation time and meets the production takt requirement under different working conditions; in addition, due to the adoption of the modified polydimethylsiloxane, the sealant has excellent waterproofness and is relatively high in strength retention rate under high temperature and high humidity conditions.
Owner:富乐(苏州)新材料有限公司

High-temperature-tolerance frequency selection wave-transmitting structure and preparation method thereof

The invention discloses a high-temperature-tolerance frequency selection wave-transmitting structure. The high-temperature-tolerance frequency selection wave-transmitting structure successively comprises a wave-transmitting layer, a modification bonding layer and a frequency selection layer from inside to outside, wherein the wave-transmitting layer is made of a continuous fiber reinforced ceramic-based wave-transmitting composite material; the modification bonding layer is made of a low-dielectric-constant material; the frequency selection layer is a noble metal physical plating layer or a noble metal glass conductor coating with periodic structure patterns. The high-temperature-tolerance frequency selection wave-transmitting structure can tolerate high temperature of 700 DEG C or more, and has excellent high temperature tolerance. The invention also provides a production method of the high-temperature-tolerance frequency selection wave-transmitting structure; the modification bonding layer is produced by using a plasma spraying process; the thermal damage to the substrate can be avoided, so that the substrate has high strength retention rate; the size accuracy of the frequency selection layer produced by a laser processing process can be higher than 20 microns; the frequency selection layer has high size accuracy.
Owner:NAT UNIV OF DEFENSE TECH +1

Method for preparing carbon/carbon/silicon carbide composite material

The invention relates to a preparation method of a carbon / carbon / silicon carbide composite material. The preparation method is characterized in that: chemical gas phase permeation technology is adopted to prepare reactive carbon atom and provide protection for carbon fiber, and is combined with the resin liquid phase dipping carbonizing technology to prepare carbon / carbon composite material through adopting a pore adjusting method of a composite material blank; moreover, the density of the obtained carbon / carbon composite material is between 1.0g / cm<3> and 1.90g / cm<3>; a method according to which the gaseous atom generated through the evaporation of solid silicon and the carbon atom in the carbon / carbon composite material are formed into SiC through chemical reaction under high temperature ranging from 1,650 DEG C to 2,200 DEG C is adopted to carry out the rapid preparation of the carbon / carbon / silicon carbide composite material. Compared with body carbon / carbon composite material, the mechanical property of the carbon / carbon / silicon carbide composite material is substantially increased to an equivalent degree and has outstanding antioxidation. Moreover, the preparation method is an engineered method which can realize the efficient preparation of a small-scale thin-wall special-shaped high-performance carbon / carbon / silicon carbide composite material.
Owner:XIAN AEROSPACE COMPOSITE MATERIALS INST

Process for producing spunlaced composite high-performance polyphenylene sulfide fiber filtering material

The invention relates to a process for producing spunlaced composite high-performance polyphenylene sulfide fiber filtering material, belongs to the fibrous raw material textile production technology field. The process uses polyphenylene sulfide fiber as raw material, has the following steps: processing raw material by checking, weighing, feeding, feeding into long certain, mixing cotton and fine loosing; layering and carding respectively by a first carding machine and a second carding machine; putting respectively into mesh placing machine for placing mesh; debatching, congruent, superposing and prewetting; spunlacing by a plurality of spunlacing machine, dewatering, drying and reeling. The advantages of the invention is that: the invention adopts polyphenylene sulfide high-performance fiber as raw material, the raw material is adapted to high efficient high speed carding production for its self physical and chemical properties, structure and adaptability to meshing and reinforcing process; improves spunlacing entanglement effect to fiber; improves the mechanical strength of spunlaced composite filtering material significantly, and ensures the end product to achieve excellent mechanical properties, filtering quality and chemical resistance property.
Owner:SHAOXING RONGLIDA TEXTILE TECH

Sliding plate brick added with compound aluminium oxide micropowder and carbon source and preparation method thereof

The invention discloses a sliding plate brick added with compound aluminium oxide micropowder and a carbon source and a preparation method thereof and relates to the technical field of refractory materials. The sliding plate brick is prepared from the following raw materials and components in percentage by weight: 40-50% of platy corundum granule, 10-20% of fused zirconia corundum granule, 5-10% of platy corundum fine powder, 5-10% of fused zirconia corundum fine powder, 10-15% of compound aluminium oxide micropowder, 0.5-3% of flake graphite, 0.5-3% of carbon black, 0.5-5% of metal aluminiumpowder, 0.5-5% of metal silicon powder and 1-4% of special additive, and the sum of the percents is 100%; in addition, 4-6% of phenolic resin is added. The finished sliding plate brick is obtained bythe processes of crushing and mixing of raw materials, mixing and rolling, forming, heat treatment, firing, digestion and carbonization, finish processing, inspection and packaging and the like. The sliding plate brick added with the compound aluminium oxide micropowder and the carbon source has the beneficial effects that by changing for the adjustment of the aluminium oxide micropowder, the heatshock resistance, washout resistance and erosion resistance of the sliding plate brick are improved and the service life is prolonged.
Owner:瑞泰马钢新材料科技有限公司

Glass fibrofelt laminated plate and preparation method thereof

The invention discloses a glass fibrofelt laminated plate and a preparation method thereof. The glass fibrofelt laminated plate and the preparation method thereof are characterized in that the glass fibrofelt laminated plate is a composite material prepared by performing hot-press molding on one layer or more than one layer overlapped high-strength tracking-resistant resin glass fibrofelt prepreg, and the tracking-resistant index is more than or equal to 600 V; the prepreg is a material formed by dipping or spray-coating a high-strength tracking-resistant resin adhesive on alkali-free glass fibrofelt and then roasting; and the high-strength tracking-resistant resin adhesive consists of 20 to 55 parts by weight of high-temperature-resistant epoxy resin, 15 to 60 parts by weight of modified phenolic resin, 10 to 35 parts by weight of a curing agent, 5 to 35 parts by weight of inorganic powder, 0.01 to 1 part by weight of an accelerant and 100 to 130 parts by weight of a solvent. The glass fibrofelt laminated plate provided by the invention is suitable for manufacturing of insulation structural components of large generator sets and nuclear power generators as well as manufacturing of high-temperature-resistant high-strength insulating composite materials for motors, transformers, military products and the like under the high-temperature working environment.
Owner:SICHUAN DONGFANG INSULATING MATERIAL

Moisture-resistant and heat-resistant high-strength silicone structural adhesive special for photovoltaic assemblies

The invention discloses a moisture-resistant and heat-resistant high-strength silicone structural adhesive special for photovoltaic assemblies. The moisture-resistant and heat-resistant high-strengthsilicone structural adhesive special for the photovoltaic assemblies consists of an A component and a B component according to a volume ratio of 10:1, wherein the A component consists of hydroxyl-terminated polydimethylsiloxane, a thixotropic agent, a reinforcing filler, a heat-resistant filler and a plasticizer; and the B component consists of methyl-terminated polydimethylsiloxane, pigment carbon black, a silane coupling agent, an active hydrogen blocking agent, a crosslinker , a catalyst, an antioxidant, a light stabilizer, and a deep curing agent. According to the moisture-resistant and heat-resistant high-strength silicone structural adhesive special for the photovoltaic assemblies, the problem that currently strength of a silicone structural adhesive decreases after damp-heat aging is solved; and the moisture-resistant and heat-resistant high-strength silicone structural adhesive special for the photovoltaic assemblies is applicable to the fields of structural bonding of double glass assembly back tracks, and between hanging buckles and glass, and bonding and sealing of photovoltaic assembly frames, and junction boxes, etc.; and the structural adhesive has high strength, excellent heat and humidity resistance and adhesion, and can play a structural adhesive role.
Owner:ZHEJIANG FORST NEW MATERIAL RES INST CO LTD

High-temperature brazing filler metal for soldering C/C and C/SiC composite materials and preparation methods thereof

A high-temperature brazing filler metal for soldering C/C and C/SiC composite materials and preparation methods thereof relate to high-temperature soldering materials and preparation methods of the high-temperature soldering materials and mainly solve the problems of low high-temperature strength retention rate and poor performance of soldering joints in existing high-temperature solders for soldering the C/C and C/SiC composite materials. The high-temperature brazing filler metal for soldering the C/C and C/SiC composite materials is made from Ni and Zr or ZrH2. A method I comprises 1) weighing Ni and Zr or ZrH2, 2) performing smelting to obtain an alloy ingot and 3) performing foil fabrication. A method II comprises 1) weighing Ni and Zr or ZrH2, 2) performing ball milling to obtain a mixed powder and 3) pressing the mixed power to obtain foils and washing and drying the foils. The high-temperature brazing filler metal for soldering the C/C and C/SiC composite materials can provide a good wettability for the C/C and C/SiC composite materials and can mainly be formed into two structures during a soldering process, thereby guaranteeing the mechanical performance of the soldering joints. The components of the high-temperature brazing filler metal for soldering C/C and C/Sic composite materials do not contain precious metals, so that the cost is low; and the melting point of the component Zr is 1852 DEG C, so that the soldering joints can be guaranteed to have a high strength retention rate at 600 DEG C.
Owner:HARBIN INST OF TECH

Method for carrying out interface modification on alumina fiber three-dimensional fabric and modified alumina fiber three-dimensional fabric prepared by same

The invention relates to a method for carrying out interface modification on an alumina fiber three-dimensional fabric and a modified alumina fiber three-dimensional fabric prepared by the same. The method comprises the steps of: carrying out preprocessing on the alumina fiber three-dimensional fabric by adopting polyanion polymer solution to obtain a preprocessed alumina fiber three-dimensional fabric; preparing lanthanum phosphate precursor solution of which a temperature is not higher than 5 DEG C; under the conditions of vacuum and a temperature which is not higher than 10 DEG C, carryingout vacuum impregnation on the preprocessed alumina fiber three-dimensional fabric by adopting the lanthanum phosphate precursor solution; and carrying out microwave heating processing on the aluminafiber three-dimensional fabric subjected to vacuum impregnation, and then sequentially carrying out steps of cleaning, drying and high-temperature processing so as to complete interface modification on the alumina fiber three-dimensional fabric. The method is simple in process, does not require complex equipment and regents, and is high in utilization rate of a raw material and low in cost; and analumina fiber reinforced aluminum oxide composite material prepared by adopting the fiber three-dimensional fabric modified by the process disclosed by the invention still has high strength after long-time high-temperature processing.
Owner:AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH

Light or colorless polyamide composite material for laser welding

InactiveCN107083056AHigh strength retentionStrength beyondFiberAlkaline earth metal
The invention discloses a light or colorless polyamide composite material for laser welding. The light or colorless polyamide composite material for laser welding comprises a laser absorption part and a laser transmission part, wherein the laser absorption part comprises polyamide, a phosphate compound, a copper halide metal compound, a halogenated metal salt compound and glass fibers; the laser transmission part comprises polyamide, the copper halide metal compound, the halogenated metal salt compound and the glass fibers; halide ions in the copper halide metal compound are chloride ions, bromide ions or iodide ions; copper ions in the copper halide metal compound are Cu<+> or Cu<2+>; metal elements in the halogenated metal salt compound are alkali or alkaline-earth metal elements; the diameters of the glass fibers are 5-20mu m; and the number average lengths of the glass fibers are 0.05-30mm; and compared with a body material without a welded conjunction surface, the composite material disclosed by the invention is relatively high in strength retention rate or even exceeds that of the body material, the property retention rate of the composite material is even up to 95% or above, and the properties of the composite material are remarkably prior to those of welding materials of common short cut glass fibers.
Owner:JIANGSU KINGFA SCI & TECH ADVANCED MATERIALS CO LTD +1

Method for manufacturing ceramic matrix composite boron nitride interface coating

ActiveCN105463403AEasy to form stoichiometric ratioStoichiometric ratio is betterChemical vapor deposition coatingLow temperature depositionReaction temperature
The invention relates to a method for manufacturing a ceramic matrix composite boron nitride interface coating, in particular to manufacturing of boron nitride coatings on a fiber surface and a substrate surface and belongs to the technical field of ceramic matrix composite toughness improvement. According to the method, a single component NH3BH3 containing B and N at the same time is selected as a precursor of a BN interface, the precursor is free of toxin and pollution, unlikely to burn or explode and capable of easily forming BN at the stoichiometric ratio of B:N=1:1, it is guaranteed that the manufactured BN is good in stoichiometric ratio, the problem that B and N in a double-component precursor are disproportionate is avoided, and no corrosive gas is generated in the manufacturing process. The method can be used for manufacturing the coating at the reaction temperature from 400 DEG C to 900 DEG C through a low-temperature chemical vapor deposition method, the temperature from 700 DEG C to 900 DEG C is preferred to increase the yield of BN, and the content of the obtained deposition product BN is over 97%. The strength retention rate of fibers can be increased as much as possible through low-temperature deposition, the strength retention rate is over 90% after deposition, and the strength retention rate is over 70% after high-temperature thermal treatment.
Owner:AEROSPACE RES INST OF MATERIAL & PROCESSING TECH +1
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