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106results about How to "With thermal shock resistance" patented technology

Ceramic coating used for heating furnace

The invention relates to ceramic coating used for a heating furnace. The ceramic coating comprises the following components: ceramic micro powder, an inorganic bonding agent and a linear thermal expansivity regulator. The invention also provides a method for preparing the ceramic coating for the heating furnace. The ceramic coating has the characteristics of having improved radiance and thermal shock resistance, being efficient and energy-saving, prolonging the service life of furnace linings and furnace tubes, improving temperature uniformity and the like, as defined below: (1) the energy consumption is reduced, the energy is saved by more than 3 percent and pollutant discharge is reduced; (2) the temperature uniformity in the heating furnace is improved: (3) the metallurgy stability of the furnace tube of the heating furnace is improved, the coking and scaling of the furnace tub are delayed, and the absorbing capacity of the furnace tube can be maximized; (4) the emissivity of the surface of the refractory lining layer can be maximized so as to increase the secondary radiation of radiant heat (energy) and increase the efficiency of the radiant section; and (5) the outer wall temperature and the exhaust gas temperature of the heating furnace can be reduced by more than 5 percent.
Owner:北京安泰恒业科技有限公司

Anti-erosion iron runner castable for large blast furnace

The invention relates to an anti-erosion iron runner castable for a large blast furnace. The material comprises, according to weight percentage, 58-64 parts of compact brown fused alumina particles, 2-5 parts of white corundum particles, 16-23 parts of silicon carbide, 5-7 parts of aluminum oxide micro-powder, 2-3 parts of pure calcium aluminate cement, 2-3 parts of silicon dioxide micro-powder, 1.5-2.5 parts of spherical asphalt particles, 0.5-1.2 parts of carbon black powder, 1.5-3.5 parts of metal silicon powder, 0.2-0.6 part of boron carbide, 0.1-0.2 part of metal aluminum powder, 0.15-0.2part of a water reducing agent, 0.6-1 part of an anti-erosion agent and 0.05-0.08 part of explosion-proof fibers. According to the castable, the service life of a primary runner of a main runner is prolonged, and the stability of safe operation of an iron runner is improved. It is verified that the requirements for rapid baking without cracking, erosion resistance, oxidation resistance, slag adhesion resistance and iron flux can be met, the iron flux can reach 180000 tons or above without repairing, and good application prospects are achieved.
Owner:TANGSHAN GUOLIANG SPEICAL REFRACTORY MATERIAL

Preparation method of hollow aluminum oxide ceramic microsphere modified polyurethane coating

The invention relates to a preparation method of a hollow aluminum oxide ceramic microsphere modified polyurethane coating. The preparation method comprises the following steps: preparing hollow aluminum oxide ceramic microspheres, namely treating aluminum nitrate and monosaccharide raw materials by virtue of steps of ultrasound, magnetic stirring, hydrothermal treatment, heat treatment and the like to obtain the hollow aluminum oxide ceramic microspheres with uniform particle size; and blending the obtained ceramic microspheres with waterborne polyurethane, and carrying out high-speed dispersion, ultrasound, spin coating and curing to obtain a composite coating. The preparation method provided by the invention has the advantages that nontoxic and easily available raw materials are adopted, a preparation process is simple, technology is controllable, cost is low, repeatability is good, and the hollow aluminum oxide ceramic microspheres are uniformly distributed. The prepared composite coating has the characteristics of environmental friendliness, light weight, high strength, high hardness, high wave transmission, low thermal conductivity, low infrared emissivity, excellent wear resistance, excellent weather resistance and the like and can be applied to the fields of heat insulation coatings, infrared stealth and the like.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

High-temperature nano radiation coating for heating furnace and preparation process thereof

The invention provides a high-temperature nano radiation coating for a heating furnace and a preparation process thereof. The coating comprises radiation function powder particles, an inorganic adhesive and an expansion coefficient regulator. The preparation process comprises the following steps: preparing the radiation function powder particles, preparing the expansion coefficient regulator, synthesizing the inorganic adhesive, mixing the radiation function powder particles, the inorganic adhesive and the expansion coefficient regulator, and filtering and grinding the obtained mixture so as to obtain the high-temperature nano radiation coating for the heating furnace. The high-temperature-resistant nano radiation coating disclosed by the invention has the characteristics of capability of increasing the radiance and the thermal shock stability, energy conservation and environmental friendliness, corrosion resistance, and capability of prolonging the service life of the heating furnace and raising the temperature uniformity, and the like. The technical indexes of the products provided by the invention are as follows: a temperature of 1800 DEG C can be resisted, the radiance epsilon is greater than or equal to 0.92, the thermal shock resistance (1300 DEG C) is greater than or equal to 5 times, the thickness of the coating is 0.1-0.2 mm, and the service life is greater than or equal to 6 years.
Owner:BDES BEIJING ENERGY SAVING TECH SERVICE

Large-sized special-shaped composite magnesium aluminate spinel product and technique for producing the same

The invention relates to large or specific compound magnesium-aluminum spinel products with the formula of 48 to 56 percent of 5-1mm magnesium-aluminum spinel, 12 to 22 percent of 1-0.088mm magnesium-aluminum spinel, 16 to 25 percent of magnesium-aluminum spinel with d90 less than 0.088mm, 3 to 6 percent of magnesium-aluminum spinel with d90 less than 0.010mm, 3 to 15 percent of beta alumina powder with d95 less than 0.020mm, 2 to 6 percent of hydratable alumina, 1 to 5 percent of magnesium promoter, 0.05 to 0.4 percent of external efficient water reducing agents (polycarboxylic acid plus sulfonation naphthaldehyde polymer plus sulfonation melamine polymer), 1 to 6 percent of latex of the system of external polyacrylic acid and 1 to 6 percent of external water. The magnesium-aluminum spinel composite combined refractory has the following chemical compositions: 72 to 87 percent of Al2O3, 12 to 27 percent of MgO, 0.2 to 1.5 percent of Na2O and 0.1 to 0.5 percent of SiO2. The raw materials are weighed according to the ratios, and are mixed, molded and maintained to make billets, and then are subjected to the processes of drying, firing at the temperature of 1430 to 1650 DEG C and inspection and the like so as to make products of large or specific compound magnesium-aluminum spinel refractory. The magnesium-aluminum spinel product has excellent manufacturing performance and excellent performances of high-temperature resistance, erosion resistance and creep resistance. As the products are casted and moulded, large and specific products can be produced.
Owner:青岛中瑞泰旭催化剂有限公司

Preparation method of tundish air brick

InactiveCN103787670AHigh Durability Thermal Shock ResistantExcellent thermal shock resistanceAzodicarbonamideCorundum
The invention discloses a preparation method of a tundish air brick. The preparation method comprises the following steps of: (1) placing 45-55 parts by weight of tabular corundum granules, 10-14 parts by weight of mullite granules and 5-8 parts by weight of chromic oxide granules into a mixer, and mixing for 5-8 minutes; (2) placing 4-6 parts by weight of white corundum fine powder, 2-3 parts by weight of alpha-Al2O3 fine powder and 1.5-3.5 parts by weight of silica micropowder into the mixer, and mixing for 10-15 minutes; (3) adding a mixture prepared from the step (1) to the mixer used in the step (2), mixing for 10-15 minute again, adding 0.4-0.6 part by weight of sodium hexametaphosphate, 0.3-0.5 part by weight of yellow dextrin, 0.1-0.3 part by weight of azodicarbonamide, 0.2-0.4 part by weight of boric acid and 0.1-0.3 part by weight of aluminum fluoride, and then mixing for 10-15 minutes again; (4) ageing for 1-2 hours, pressing for forming by using a press machine, and drying into a drying kiln at 200 DEG C for 24 hours; (5) firing under the condition of 1250-1350 DEG C for 2-3 hours.
Owner:WUXI CHENGBO SCI & TECH DEV

Preparation method of refractory high-entropy alloy skeleton-copper spontaneous perspiration composite structure

The invention discloses a preparation method of a refractory high-entropy alloy skeleton-copper spontaneous perspiration composite structure. The method comprises the following steps of: smelting a refractory high-entropy alloy raw material to obtain an alloy ingot, and preparing refractory high-entropy alloy powder from the alloy ingot by using a plasma rotating electrode atomization method; forming the refractory high-entropy alloy powder into a preset porous skeleton structure through an electron beam or selective laser melting additive manufacturing process; and infiltrating metal copper into the porous skeleton structure by adopting an infiltration process, thereby obtaining the refractory high-entropy alloy skeleton-copper spontaneous perspiration composite structure. The structure has the characteristic of spontaneous perspiration, and is suitable for high-temperature parts such as rocket engine nozzle throat inserts, thrust chamber injector panels, missile warhead nose cones and electromagnetic gun tracks. The prepared composite structure has the advantages that the forming process is simple, the porosity can be conveniently designed and adjusted according to actual requirements, the mechanical property is good, high temperature resistance and thermal shock resistance can be achieved, and high practical value is achieved.
Owner:JIANGSU UNIV OF SCI & TECH +2

Silicon carbide reinforced carbon matrix composite material and preparation method

The invention discloses a silicon carbide reinforced carbon matrix composite material and a preparation method. Mesocarbon microbeads are adopted as the matrix, and silicon carbide ceramic is adoptedas the reinforcement phase and is evenly distributed among the carbon microbeads so as to form a three-dimensional network silicon carbide skeleton reinforced isotropic structure. Technically, siliconpowder particles and the mesocarbon microbeads are taken as the raw materials to prepare uniform and thickness controllable silicon carbide coating coated mesocarbon microbead powder by molten salt method, after pre-press molding, discharge plasma sintering is carried out at 1600-1900DEG C to form a uniform three-dimensional network silicon carbide ceramic skeleton, while the strength, ablation resistance, oxidation resistance and thermal shock resistance of the carbon matrix are improved, the thermal conductivity of the matrix is also improved, therefore the isotropic carbon matrix compositematerial characterized by low cost, low density and excellent mechanical properties, sintering properties, thermal shock resistance, ablation resistance and thermal conductivity can be formed. Because of the excellent comprehensive performance, the silicon carbide reinforced carbon matrix composite material can be widely applied to aerospace, national defense, electronic packaging and other fields, and has broad application prospects.
Owner:XI AN JIAOTONG UNIV

Quartz glass tube silicon chip bracket component

The invention provides a quartz glass tube silicon chip bracket component for a mesh belt-free silicon chip sintering furnace. The component comprises a quartz glass tube, metal sleeves, support legs and limiting screws, wherein the support legs are fixed on the metal sleeves; the metal sleeves are provided with threaded holes and are fixed on the quartz glass tube at equal intervals through the limiting screws; the support legs are made of steel wires; and the surfaces of the steel wires are coated with ceramic coatings. The quartz glass tube has the advantages of high intensity, high temperature resistance, low expansion coefficient, thermal shock resistance, acid resistance, chemical stability, high electrical insulating property, small heat absorption capacity and the like and is very suitable to be taken as a silicon chip bracket. The support legs are made of steel wires and the surfaces of the steel wires are coated with ceramic coatings, so that the requirements on intensity, high temperature resistance and wearing resistance of the support leg are met and metal ion pollution of a silicon chip caused by metal contact in a sintering process is reduced. Each metal sleeve is provided with an opening and a threaded hole, so that the metal sleeve is convenient to fix on the quartz glass tube.
Owner:EGING PHOTOVOLTAIC TECHNOLOGY CO LTD

Dispersion strengthened ceramic composite material and preparation method thereof

ActiveCN106747545AWith stomata control, fromThermally conductiveChemical industryCeramic composite
The invention discloses a dispersion strengthened ceramic composite material and a preparation method thereof and belongs to the field of composite materials and engineering ceramic materials. The composite material is formed by compounding silicon carbide of different forms, calcium sulfate whiskers, metal fibers and a composite adhesive, wherein the silicon carbide of different forms, the calcium sulfate whiskers, the metal fibers and the composite adhesive are interweaved and distributed. The preparation method comprises the following steps: 1) uniformly mixing the silicon carbide, the calcium sulfate whiskers, the metal fibers and the composite adhesive under vacuum conditions so as to prepare slurry; 2) vibrating and casting the slurry in a mold under vacuum; and 3) curing the mold and cast slurry, thereby obtaining the dispersion strengthened ceramic composite material. According to the method disclosed by the invention, the problems of wear and corrosion of highly corrosive solid-liquid media on pump materials during transport are effectively solved, and the prepared composite material has the characteristics of high metal matrix adhesion force, high hardness, wear resistance, corrosion resistance, oxidation resistance, thermal shock resistance and the like and is applied to the fields of chemical industry, pharmacy, papermaking and the like.
Owner:NORTHEASTERN UNIV +1
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