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94results about How to "Control microstructure" patented technology

Production method for optimizing drawing performance of steel wire rod for carbon steel welding wire

The invention relates to a production method for optimizing the drawing performance of a steel wire rod for a carbon steel welding wire, belonging to the technical field of steel production. The technology path comprises the following steps of billet chemical composition control and inspection, heating of a walking heating furnace, rough rolling, top cutting by a flying shear, middle rolling, precision rolling in advance, high-speed precision rolling, sending and clamping, as well as spinning, temperature controlling, and disperse coil cooling, collecting coils, and steel wire rod inspection. The method is characterized in that through optimizing the technology parameters of operation key points, the effective control to microstructure of the steel wire rod for the carbon steel welding wire on a high-speed wire rod production line short of slow cooling capability is realized, and the frequent brittleness problem caused by the common structure reason in the drawing process, especially the high-speed drawing process of the steel wire rod for the carbon steel welding wire on produced on the production line is solved. The method has the advantages that the effective control of the steel wire rod structure for the carbon steel wire on the traditional high-speed line material production line can be realized without prolonging the length of slow cooling, and the generation of the low-temperature hard phase structure is avoided, thus the drawing performance of the steel wire rod is changed, and the requirement of drawing use of the type of the steel wire rod is met.
Owner:SHOUGANG CORPORATION

Silicon carbide reinforced metal matrix composite with micro orientated structure and preparation method thereof

The invention relates to a silicon carbide reinforced metal matrix composite with a micro orientated structure and a preparation method thereof. The composite consists of silicon carbide with a volumefraction of 5-90% and metal, and has the micro orientated structure which is expressed as oriented arrangement of the silicon car bide in a metal matrix. The preparation method of the composite comprises the following steps of: firstly preparing water-based slurry containing silicon carbide powder; processing the slurry by utilizing freeze casting and vacuum freeze drying to obtain a green body with an orientated porous structure; compressing the green body and removing organic matters in the green body; carrying out sintering to obtain an oriented porous skeleton of silicon carbide; and finally infiltrating the skeleton by utilizing liquid metal bath, and carrying out solidification and cooling to obtain the silicon carbide reinforced metal matrix composite with the micro orientated structure. The composite has excellent properties such as light mass, high intensity, wear resistance and high-temperature creep resistance, the micro structures and properties of the composite can be effectively controlled through adjusting the preparation process, and the composite has considerable application prospect when serving as a structural material.
Owner:INST OF METAL RESEARCH - CHINESE ACAD OF SCI

Wide-temperature range and high-efficiency soft ferrite material, magnetic core preparation method and application

The invention provides a wide-temperature range and high-efficiency soft ferrite material, a magnetic core preparation method and the application. Through optimized selection of a main formula and effective doping, the wide-temperature range and high-efficiency soft ferrite material is developed; by a multi-stage equilibrium atmosphere sintering method, the density, the crystal grain size and theporosity of the ferrite material and distribution of the ferrite material inside and between crystal grains are controlled, so that the microstructure of the ferrite material is more effectively controlled, and main characteristic parameters of the material are guaranteed to be harmonious and unified; ui of a final product can reach 3400, the core loss at 25-120 DEG C is 350mW, the core loss at 100 DEG C is 250mW, the L value stably reaches +3.5% in the temperature range of -40 DEG C to 85 DEG C, and the overall loss level is reduced by 8-13.8% in a relatively wide temperature range; the hightemperature Bs of the final product is also greatly improved, the final product has excellent inductance stability under a wide-temperature range condition, and the production cost is reduced by 20% or above.
Owner:湖北华磁电子科技有限公司

Multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating and preparation method thereof

ActiveCN103722849AImproves antioxidant propertiesMitigates differences in coefficient of thermal expansionLayered productsOxidation resistantMicrostructure
The invention discloses a multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating and a preparation method thereof. The multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating is formed by laminating SiC layers, Ta layers and C layers, and is characterized in that the laminating sequence is the SiC layer, the Ta layer, the C layer, the Ta layer and the SiC layer, or SiC layer, the Ta layer, the C layer, the Ta layer, the SiC layer, SiC layer, the Ta layer, the C layer, the Ta layer, and the SiC layer, or SiC layer, the Ta layer, the C layer, the Ta layer, the SiC layer, SiC layer, the Ta layer, the C layer, the Ta layer, the SiC layer, SiC layer, the Ta layer, the C layer, the Ta layer and the SiC layer; both sides of the C layer are Ta layers; the innermost layer and the outermost layer are SiC layers; and the Ta layer, the C layer, the Ta layer and the SiC layer are sequentially deposited on the prepared SiC layer with a chemical vapor deposition method so as to obtain the multilayer antioxidant high-temperature-resistant SiC/Ta/C/Ta/SiC coating. According to the coating and the preparation method thereof, the outer SiC layer forms a layer of SiO2 film in a high-temperature aerobic environment, so that diffusion of oxygen atoms can be prevented effectively, and meanwhile, a TaC layer can be formed on a contact surface of the Ta layer and the C layer to further improve the antioxidation performance. Alternate deposition of coatings can effectively relieve differences of coefficients of thermal expansion of the coatings and improve the thermal shock performance of the coatings remarkably, the thickness and lay number of a matrix can be controlled by controlling deposition time and deposition times, and the microstructure of the composite coating can be controlled.
Owner:TAICANG PAIOU TECH CONSULTING SERVICE

Metal ceramic alloy free of core-ring structure and preparation method thereof

ActiveCN109338193ASmall expansion coefficientRealize microcrystallization interfacial bonding methodMaterials preparationAlloy
The invention relates to the technical field of metal ceramic material preparation, and relates to a metal ceramic alloy free of a core-ring structure and a preparation method thereof. The metal ceramic alloy free of the core-ring structure comprises the following components of, in percentage by weight, 10-55% of Ti (C, N) micron powder, 10-55% of (Ti, M) (C, N) micron powder, 10-55% of Ti (C, N)sub-micron or / and nano powder, 10-55% of (Ti, M) (C, N) sub-micron or / and nano powder, 5-20% of WC, 0-30% of TiC, 0-30% of TiN, 0-20% of Co, 0-20% of Ni, 0-10% of Cr, 0-15% of Mo2C, 0-10% of TaC / NbC,0-2. 5% of VC, 0-5% of Cr2C3, and 0-1.2% of carbon black; the components are prepared into a mixture according to a certain ratio, the mixture is subjected to ball milling, sieving and mould pressingto prepare a blank, and the blank is subjected to sintering and cooling to prepare a metal ceramic material free of the core-ring structure. According to the method, a powder metallurgy method is adopted to prepare the metal ceramic alloy free of the core-ring structure, and the technological difficulty of being not easy to control the thickness of a microcosmic core-ring structure in the preparation process a traditional metal ceramic with core-ring structures is solved.
Owner:ZIGONG CEMENTED CARBIDE CORP

Preparation method of fine-grain TA15 titanium alloy foil

The invention discloses a preparation method of fine-grain TA15 titanium alloy foil. The preparation method specifically comprises the following steps of (1) heating a TA15 titanium alloy cast ingot at 1000-1100 DEG C, and then carrying out cogging forging to obtain a plate blank; (2) carrying out heat preservation at 900-960 DEG C, and then carrying out rolling; (3) carrying out heat treatment at 30-50 DEG C above a beta phase transformation point, and then carrying out water quenching cooling; (4) carrying out heating at 900-940 DEG C, and then carrying out rolling; (5) carrying out assembly welding on the obtained blank to obtain a cladding ply-rolling pack; (6) carrying out heating at 900-940 DEG C, and then carrying out rolling for the fourth time; (7) opening the ply-rolling pack, and then carrying out assembly welding on the blank to obtain a cladding ply-rolling pack; (8) carrying out heating at 920-940 DEG C, and then carrying out rolling in a direction perpendicular to the previous rolling direction; (9) carrying out annealing, creep correction, alkali pickling and sanding on the blank to obtain a plate with the thickness of 0.6 mm; (10) shearing the plate, and then carrying out cold rolling multiple times to obtain rolled foil with the thickness ranging from 0.1 mm to 0.2 mm; and (11) carrying out vacuum annealing heat treatment to obtain the finished foil with the thickness ranging from 0.1 mm to 0.2 mm.
Owner:INST OF METAL RESEARCH - CHINESE ACAD OF SCI

Organization control method of large-size pre-hardening type plastic die steel module

The invention relates to an organization control method of a large-size pre-hardening type plastic die steel module for manufacturing plastic products, belonging to the technical field of metallographical organization structure control of alloy steel heat treatment. Aiming at multiple large-size pre-hardening type plastic die steel containing carbon, chromium, manganese and molybdenum or the large-size pre-hardening type plastic die steel containing a small amount of elements of copper, nickel, aluminum, boron, and the like, after steel ingots are forged into a module, cooling is controlled according to the phase change characteristics of the steel, and then heat is preserved in a low-temperature furnace to ensure that the austenite of the module is sufficiently converted; the module is heated again at a proper speed, and after complete austenite, the cooling is controlled; after the temperature of the surface of the module is reduced to 350-200 DEG C, slow cooling is carried out to obtain a bainite or bainite and martensite mixed organization, and the grain size is 5-8 grades; and finally, tempering is carried out within a temperature range of 300-600 DEG C, the hardness is adjusted into a range of 28-38 HRC, and the section hardness difference is smaller than +/-2HRC.
Owner:SHANGHAI UNIV

Preparation method of 550-650 DEG C high-temperature titanium alloy foil

The invention relates to a preparation method of 550-650 DEG C high-temperature titanium alloy foil. The method specifically comprises the following steps of (1) heating a high-temperature titanium alloy cast ingot at 1100-1200 DEG C, and then carrying out forging to obtain a blank; (2) carrying out heating at 950-1000 DEG C, and then carrying out rolling; (3) carrying out heat treatment at 50-70 DEG C above a beta phase transformation point, and then carrying out water quenching cooling to room temperature to obtain a plate blank; (4) carrying out heating at 950-1000 DEG C, and then carrying out rolling; (5) carrying out assembly welding on the obtained blank to obtain a cladding ply-rolling pack; (6) heating the ply-rolling pack at 950-1000 DEG C, and then carrying out rolling; (7) opening the ply-rolling pack, and carrying out secondary assembly welding on the blank to obtain a cladding ply-rolling pack; (8) heating the ply-rolling pack at 900-950 DEG C, and then carrying out rolling in a direction perpendicular to the previous rolling direction; (9) carrying out annealing, creep correction, alkali pickling and sanding to obtain a plate with the thickness of 0.6 mm; (10) shearing the plate, and then carrying out cold rolling 7-25 times to obtain rolled foil with the thickness of 0.08-0.2 mm; and (11) carrying out vacuum annealing heat treatment to obtain the finished foil with the thickness ranging from 0.08 mm to 0.2 mm.
Owner:INST OF METAL RESEARCH - CHINESE ACAD OF SCI

arsenic-removing adsorbent with IB group metal nanoparticles loaded on zinc zirconium composite oxide and preparation method thereof

The invention discloses an arsenic-removing adsorbent with IB group metal nanoparticles loaded on a zinc zirconium composite oxide and a preparation method thereof. The method comprises the followingsteps: firstly, preparing an IB group metal salt solution, a zinc salt solution and a zirconium salt solution into a mixed metal salt solution; with the deionized water with pre-regulated pH value asa base solution, adding the mixed metal salt solution and a precipitant solution for co-precipitating and controlling an end point pH value within a range of 7-10; ending the dropwise adding, continuously stirring, heating and hydrolyzing the precipitate; centrifugally separating, thereby acquiring a hydrolysis product; washing, centrifuging, drying and baking, thus obtaining the arsenic-removingadsorbent. The arsenic-removing adsorbent prepared according to the invention is high in specific surface area and narrow in pore size distribution; the metal nanoparticles are highly dispersed and loaded onto an amorphous composite oxide carrier, so that the arsenic-removing adsorbent has the characteristics of high removal rate, high adsorption capacity, less dosage, high adsorption rate, and the like; the arsenic-removing adsorbent can be used for deeply treating the low-concentration arsenic pollutants in underground water and surface water and the low-concentration arsenic-bearing industrial wastewater.
Owner:FUZHOU UNIV

Preparation method for silicon dioxide block layer used for I-III-IV compound solar cell

The invention relates to the technical field of a solar cell and provides a preparation method for a silicon dioxide block layer used for an I-III-IV compound solar cell. The preparation method comprises the following steps that: acid catalysis solution of ortho-silicic acid alkyl ester is prepared; the acid catalysis solution of the ortho-silicic acid alkyl ester rests for 0.5-6h, and then NH4OH solution is added into the acid catalysis solution, so as to obtain silica sol; the silica sol is coated on a medium in an isopropanol atmosphere; the medium after being coated with the silica sol is aged continuously in the isopropanol atmosphere for 5-75min and then is soaked into isopropanol solution to be aged, so as to obtain an aged gel membrane; and the aged gel membrane is heated and dried, the heating rate is 10-180 DEG C/s, the aged gel membrane is kept for 10-75min after being heated to the temperature of 150-500 DEG C, so as to obtain the silicon dioxide block layer used for the I-III-IV compound solar cell. The preparation method is simple, thereby being suitable for batch production; moreover, the prepared silicon dioxide block layer used for the I-III-IV compound solar cell can effectively improve the efficiency of the solar cell.
Owner:徐东

Method for connecting Cf/LAS composite material via AgCuTi brazing filler metal

The invention discloses a method for connecting Cf/LAS composite material via an AgCuTi brazing filler metal. The method for connecting Cf/LAS composite material via the AgCuTi brazing filler metal comprises the following steps: step 1, machining the Cf/LAS composite material; step 2, processing the connection surface of the Cf/LAS composite material obtained in the step 1, placing the connection surface of the Cf/LAS composite material in the acetone solution and ultrasonic cleaning; step 3, placing the AgCuTi brazing filler metal between the connection surfaces of the Cf/LAS composite material to be connected, assembling the assembling piece with Cf/LAS composite material/AgCuTi brazing filler metal/Cf/LAS composite material overlapped in sequence; step 4, placing the assembling piece obtained in the step 3 in a vacuum heating furnace, pumping vacuum, electrically heating and cooling; the method for connecting Cf/LAS composite material via the AgCuTi brazing filler metal is mainly used for connecting the Cf/LAS composite material parts being smaller in size or simpler in shape together for obtaining the member being larger in size or complex in shape, the creep resistant property and thermal shock resistance of the high temperature structure can be improved and great application prospect can be achieved.
Owner:HARBIN INST OF TECH AT WEIHAI
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