113results about How to "Play a pinning role" patented technology

The invention discloses a preparation method of a graphene alloy nanocomposite and an SLM (Selective Laser Melting) forming process. According to the preparation method, turbid liquid is prepared through the ultrasonic vibration of anhydrous ethanol, so that the graphene is uniformly dispersed in the anhydrous ethanol, the graphene is uniformly dispersed, then after the graphene anhydrous ethanolturbid liquid is mixed with high-temperature alloy in proportion, the graphene and partial residue are distributed in the grain boundary and crystals by participating in the interfacial reaction, so that the strength and toughness of a formed part are improved, and the hot cracking tendency is reduced; the addition of graphene changes the organization form of the material; and in the SLM forming process, the graphene in the graphene high temperature alloy nanocomposite is used as a heterogeneous nucleating agent, and increases the nucleation rate in the solidification crystallization process.The graphene high temperature alloy nanocomposite is prepared by the dielectric barrier discharge plasma-assisted ball milling technique. The plasma enhances the activity of powder, so that columnar crystals preferentially growing change to isometric crystals, grains are refined and the performances are improved.

The invention relates to a high-strength Cu-Ni-Si alloy and preparation method thereof. The alloy comprises 2.0-6.0% of Ni, 0.5-1.5% Si, 0.5-1.0% of Ti, 0.5-1.0% of Mn, 0.5-1.0% of Ag and the balance of copper and unavoidable impurity elements. The preparation method sequentially comprises the following steps of smelting; casting; homogenization treatment; hot rolling and solution treatment; pre-cold rolling and aging treatment; and cold-rolling deformation. A Ni2Si non-oxide reinforcing phase is generated in the alloy disclosed by the invention; after the rolling is carried out repeatedly, the nucleation positions of precipitated phases can be increased, the more the broken grains, the more grain boundaries, the more nucleation positions of the precipitated phases and the more the precipitated phases; and under the condition that aging treatment is carried out repeatedly, the more precipitated phases are precipitated and thus the comprehensive performance of the alloy is dramatically increased, the strength, the elongation property at a high temperature and the electric conductivity are improved and the bending workability of the alloy is also improved.

The invention relates to a pipeline steel, especially to a pipeline steel with resistance against carbon dioxide and hydrogen sulfide corrosion, and also relates to a preparation method thereof, and belongs to the field of pipeline steel manufacturing technology. The pipeline steel with resistance against carbon dioxide and hydrogen sulfide corrosion comprises following chemical compositions in mass percent, C 0.02 to 0.08%, Si 0.10 to 0.50%, Mn 0.10 to 0.50%, V 0.01 to 0.20%, Al 0.01 to 0.05%, Cu 0.10 to 0.50%, Cr 2.0 to 6.0%, Ni 0.3% or less, Nb 0.3% or less, Ti 0.3% or less, P 0.02% or less, and S 0.005% or less, with the balance being Fe or impurity elements which are unavoidable. The pipeline steel is resistant against both carbon dioxide and hydrogen sulfide corrosion, and can be used in an environment with both of the two corrosive gases, and the resistance against carbon dioxide and hydrogen sulfide corrosion of the pipeline steel is 2 times or more of that of currently used carbon steel.

The invention discloses a copper steel composite material, an arc additive preparing method and application of the copper steel composite material and a tin bronze alloy. The composite material is composed of a copper alloy layer and a steel layer. The copper alloy layer is novel tin bronze and comprises the following components including, by weight percent, 5%-10% of Sn, 0.15%-0.35% of Al, 0.05%-0.2% of Si, smaller than 0.01% of Pb, smaller than 0.01% of Ni and the balance Cu. A preparing technology of the composite material includes the steps that firstly, casting of a novel tin bronze alloybar is conducted; secondly, the alloy bar is subjected to extruding and drawing technologies, and a wire with the diameter being 0.8 mm to 1.6 mm is prepared; and thirdly, the wire is arranged on thesurface of a steel plate in an arc additive manner, and the copper/steel composite material is obtained. The copper steel composite material is high in combination strength and has dendrite tissue which is compact, uniform and fine, and the wear reducing and resisting performance and the bearing performance are high.

The invention discloses a crystalline grain control method for a GH690 alloy shear cover of an explosion valve and belongs to the technical field of material machining. The method aims to solve the problems that the structure of a forge piece of the GH690 alloy material shear cover of the explosion valve is not even, and crystalline grains abnormally grow up. A heat treatment machining is organically combined with a forging machining, and the machining method that large deformation free forging is implemented at a high temperature (1020 DEG C to 1150 DEG C), small deformation foetal die forging is implemented at a medium temperature (710 DEG C to 850 DEG C), and the inhibition function of carbide second-phase particles on moving of a grain boundary is used for restraining the abnormal growth of the crystalline grains in forging machining of the shear cover in an auxiliary mode is provided. According to the crystalline grain control method for the GH690 alloy shear cover of the explosion valve, the forging piece forming and crystalline grain refinement are conducted synchronously, and the shear cover forge piece is obtained through heating twice; the machining limitation that a forging piece with the simple structure is subjected to high-temperature multiple-time hierarchical forging machining at present is overcome; the forging heating number is reduced; the follow-up heating treatment of the forging piece of the GH690 nickel-based alloy sheer cover is avoided. The structure with even carbides and refined crystalline grains of the GH690 alloy shear cover of the explosion valve forged through the method can be obtained.

The invention relates to pre-hardening plastic die steel. The preparation method comprises the following steps: adding 0.05-0.15%V of microalloying elements into 4Cr2NiMnMo; after pleiotropic deformation, carrying out fine treatment and pre-hardening treatment, wherein the pleiotropic deformation comprises radial and axial forging deformation of the die steel and transverse and vertical pleiotropic deformation with the forging ratio greater than or equal to 8; the fine treatment comprises the following step: by taking the temperature of the forged die steel with the product thickness as a starting point, heating to 880+/-10 DEG C; and after insulating at a speed of 3min/mm, discharging and air-cooling to 70 DEG C for spheroidizing annealing, wherein the specific process comprises the following steps: quickly heating to 780+/-10 DEG C*3min/mm; and then cooling to 550 DEG C for discharging and air cooling at a speed less than or equal to 30 DEG C/h; the pre-hardening treatment comprises the following steps: heating the die steel with the product thickness from 70 DEG C to 350+/-10 DEG C; insulating at the speed of 3min/mm; then heating to 880+/-10 DEG C; then, insulating at the speed of 3min/mm; and then air-cooling to 70 DEG C and tempering.

The invention relates to the field of materials, specifically relates to a preparation method of a graphene ceramic material. The preparation method comprises the following steps: (1) taking graphene to prepare a graphene impregnation liquid; (2) carrying out glue discharge treatment on zirconia ceramic; (3) carrying out vacuum pressing impregnation on the graphene impregnation liquid obtained in the first step and the zirconia ceramic after glue discharge obtained in the second step so as to obtain a graphene-zirconia ceramic composite material perform; (4) carrying out microwave sintering on the graphene-zirconia ceramic composite material perform so as to obtain a graphene-zirconia ceramic composite material. Compared with the prior art, the bending strength, breaking tenacity and hardness of the prepared graphene-zirconia ceramic composite material are obviously improved by 37.68%, 35.89% and 18.34% respectively when being compared with those of a relatively common ceramic material, and the macro-mechanical properties are obviously increased; compared with that of a common ceramic material, the electrical conductivity is obviously improved, and the graphene is free of dispersed distribution in a ceramic base body but is of a network-like compact simple-substance structure.

The invention discloses a normal-pressure solid-phase sintered silicon carbide ceramic profiled part and a manufacture method thereof. A compact silicon carbide ceramic profiled part product is obtained by material preparation, material mixing through ball milling, high pressure grouting, drying in shade and low temperature drying and high temperature sintering. Through optimized matching of silicon carbide particles at different levels and effective design of channels of a resin die, micrometer powder is introduced to overcome obstruction of die channels, thereby obviously prolonging the service life of the die. The micrometer powder is large in size and small in specific surface area, thereby preventing loss of components, and through matching of particles with different size, sub-micrometer powder is uniformly dispersed in micrometer powder, thereby overcoming low grouting efficiency and nonuniform components. The density of a blank obtained from matching of particles with different size is obviously increased, so that the contraction is reduced and the blank is beneficial for preventing sintering deformation and cracking of a solid-phase sintered silicon carbide ceramic profiled part. Boric acid or/and diboron trioxide is adopted as a sintering aid and is dissolved in a thick liquid, so that the sintering aid is uniformly dispersed, and the density distribution of high-temperature-sintered silicon carbide ceramic profiled part is uniform.

The invention discloses a TiCp/EPS lost foam manufacturing technology and a steel matrix composite casting technology by means of a TiCp/EPS lost foam and relates to the technical field of composite lost foam casting in the metal forming field. The casting technology comprises manufacturing of a TiCp/EPS composite lost foam pattern, pattern coating material smearing, drying, a steel matrix composite lost foam negative pressure casting technology process, a pouring technology, a heat treatment technology and the like. TiC particles and a matrix are firmly combined, the TiC particles are evenlydispersed, the comprehensive mechanical property of a product is improved, and large-sized TiC reinforced steel matrix composite part in complicated shapes can be manufactured by means of lost foam casting.

The invention provides a heat processing technology for improving the impact energy of 20CrNiMo alloy steel. The technology includes the following steps: I, performing carburizing treatment to the 20CrNiMo alloy steel until the depth of a carburizing layer reaches 1.4 mm to 1.7 mm; II, performing primary quenching; III, performing primary tempering, V, performing secondary quenching; IV, performing secondary tempering. According to the invention, through improving the heat processing technology of the 20CrNiMo alloy steel, the problem that other excellent performances of the 20CrNiMo alloy steel cannot be fully exerted due to lower impact energy is solved, the material usability is better, and the application range is wider.

The invention discloses a preparation method of a high-strength and high-toughness high-entropy alloy, and relates to the technical field of alloy material production. The preparation method comprises the following specific steps that high-entropy alloy powder prepared from the components in atomic percent: 27%-30% of Mn, 8%-12% of Co, 8%-12% of Cr, 0.4%-1.3% of C and the balance of Fe is prepared; the high-entropy alloy powder is subjected to ball milling treatment and then pre-pressed, the pressure ranges from 300 MPa to 500 MPa, the pressure is maintained for 200 seconds to 300 seconds, and a pre-pressed block of the high-entropy alloy is obtained; the pre-pressing block is subjected to vacuum annealing, vacuum hot pressing sintering and cold rolling deformation; and the high-entropy alloy sheet subjected to cold rolling deformation is subjected to constraint carbon distribution treatment at the temperature of 400-550 DEG C, and free carbon elements are diffused. The C-containing unequal-atom FeMnCoCrC high-entropy alloy prepared through the method has excellent strength and plasticity combination, and meanwhile, the problems that a high-entropy alloy prepared through a traditional technology is uneven in component and unstable in structure are solved.

The invention relates to a ceramic fiber toughened CVD silicon carbide (SiC) composite and a preparation method and application thereof. The ceramic fiber toughened CVD SiC composite adopts a C/SiC composite as a substrate, SiC fibers are generated on the substrate in situ, SiC is deposited on the peripheries of the SiC fibers generated in situ, and a SiC layer toughened by the SiC fibers is formed; the SiC layer toughened by the SiC fibers is further internally provided with metal M and/or a carbide of the metal M and/or a silicide of the metal M; and M is selected from one or more of iron, cobalt and nickel. The preparation method of the ceramic fiber toughened CVD SiC composite comprises the steps: pyrolytic carbon is deposited on a carbon fiber perform firstly; then silicon melting andsiliconizing are conducted; then a catalyst, namely the metal M is introduced in a plated mode; SiC whiskers are prepared through vapor deposition; and finally, the SiC layer is prepared. The designed and prepared composite is particularly suitable for a reflector of a space camera.

A CO2 and Cl<-> corrosion resistant high-strength 15Cr oil pipe for high-temperature high-pressure wells comprises the following compositions in percent by weight: carbon, <=0.03 wt%; silicon, 0.2-0.5 wt%; manganese, 0.2-0.6 wt%; phosphorus, <= 0.02 wt%; sulfur, <= 0.005 wt%; chromium, 14.5-15.3 wt%; molybdenum, 1.7-2.4 wt%; copper, 0.6-1.0 wt%; nickel, 6.5-7.5 wt%; tungsten, 0.4-0.7 wt%; titanium, 0.002-0.007 wt%; boron, 0.001-0.005 wt%; niobium, 0.04-0.09 wt%; vanadium, 0.03-0.07 wt%; nitrogen, 0.01-0.1%; oxygen, <= 0.001 wt%; hydrogen, <= 0.000005 wt%; controlled compositions: arsenic, <=0.03 wt%; antimony, <=0.03 wt%; and antimony, <=0.03 wt%; and the balance iron. According to the 15Cr oil pipe, the minimum yield strength is 925 MPa (125ksi steel grade), the critical usage temperature is 210 DEG C, the CO2 partial pressure can be 10 MPa or more, the Cl<-> concentration can be 120000 mg/L, the 15Cr oil pipe has certain H2S stress corrosion cracking resistant performance, and compared with a super II type 13Cr martensite stainless steel oil pipe material, the increased cost is not large.

The invention relates to a silicon-based negative electrode material containing a silicate framework, a negative plate and a lithium battery. The silicon-based negative electrode material comprises amodified silicon monoxide material in which a silicate material is dispersedly distributed, the general formula of the modified silicon monoxide material with the silicate material dispersed inside isMxSiOy, X is larger than or equal to 1 and smaller than 6, y is larger than or equal to 3 and smaller than 6, and the element M comprises one or more of Mg, Ni, Cu, Zn, Al, Na, Ca, K, Li, Fe and Co.wherein the grain size is 0.5 nm to 100 nm; in the modified silicon monoxide material, the content of the silicate material accounts for 5%-60% of the total mass of the modified silicon monoxide material; the dispersedly distributed silicate material forms a framework structure of the silicon-based negative electrode material, does not generate a physicochemical reaction along with lithium removaland lithium intercalation of the silicon-based negative electrode material in the circulation process, and keeps the original structure unchanged after multiple times of circulation.

The invention discloses a nickel electrode slurry which comprises the following components in parts by weight: 40.05-70 parts of a coated nickel powder, 0.01-5 parts of barium titanate particles, 0-8 parts of an adhesive, 0.5-3 parts of a dispersing agent, 10-40 parts of a solvent and 0-15 parts of a diluent. The coated nickel powder comprises a nickel powder and a barium titanate coating layer coated on the surface of the nickel powder. According to the formula, the coated nickel powder with the barium titanate coating layer and the barium titanate particles doped in the coated nickel powder are selected at the same time, sintering shrinkage of the nickel powder is inhibited through the combined action of the barium titanate with the two structural relations, and the effect is greatly improved; and according to the process, the slurry is dispersed in a manner of combining squeezing and cavitation blasting so that the dispersion effect is enhanced, the mechanical grinding time is shortened, excessive grinding is prevented, the surface characteristics of the nickel powder are kept, and the oxidation resistance of the nickel powder is excellent.

The invention provides a magnesium-based spherical quasicrystal master alloy and a preparation method thereof, which relates to a magnesium-based alloy taking zinc as a secondary main component. The alloy is a Mg-Zn-Y-C quaternary magnesium-based icosahedral spherical quasicrystal master alloy comprising the following chemical components: 55.0 to 65.0 percent of Mg, 30.0 to 40.0 percent of Zn, 2.5 to 5.5 percent of Y, and 0.1 to 0.5 percent of C, wherein the diameter of spherical quasicrystals is 3 to 7 mu m; the average diameter of the spherical quasicrystals is 6 mu m; and the volume of the spherical quasicrystals accounts for 40 to 48 percent of the total volume of the alloy. The preparation method is characterized by adopting control over solidification rate, namely pouring molten alloy into a casting mold with cooling rate controllable and controlling the solidification rate in a range between 68.4 and 84.8 K/s. The alloy can improve the mechanical properties of alloy material better when a magnesium alloy matrix is reinforced, and has the advantages of simple process, not high demand for equipment, extensive sources of raw materials, convenience for realizing industrialized production and resource conservation.

The invention discloses a method for improving long-term oxidation resistance of a high-niobium titanium-aluminum alloy through adding yttrium at high temperature, belonging to the high temperature oxidization field of the metal material. The invention is characterized in that Y is added in a Ti 45Aa17Nb alloy or a Ti 45Al 8Nb alloy, a tiny yttrium doping high-niobium titanium-aluminum alloy complete lamellar structure is obtained after using vacuum melting and homogenization treatments; the alloy comprises the following components by atomic percent: 46.4-47.9% of Ti, 45% of Al, 7-8% of Nb and 0.1-0.8% of Y; and the homogenization treatment process comprises the following steps: heat insulation is carried out at a temperature of 1320 DEG C for 12h, a converter is insulated for 30 minutes at a temperature of 900 DEG C and then taken out for air cooling. The invention has the advantages that adding proper amount of Y increases the proportion of Al2O3 in an oxide film, reduces the thickness of the oxide film, refines particles producing the oxide, facilitates plastic deformation of the oxide film and reduces cracking of the film; and by epoxidation experiments, after all alloys containing Y go through 1000 cycle periods, no obvious shedding phenomenon occurs in the oxide film, and addition of Y improves the adhesion of the alloy oxide film and raises the use temperature of the high-niobium titanium-aluminum alloy to the temperature of more than 900 DEG C.

The invention relates to a nickel-based alloy with high grain-boundary strength and a preparation method thereof. The nickel-based alloy consists of the chemical components in percentage by weight; 20-25 percent of chromium, 0.2-0.7 percent of copper, 0.01-0.2 percent of carbon, 8.0-10.0 percent of molybdenum, 10-15 percent of cobalt, 0.5-1.5 percent of aluminum, 0.2-0.6 percent of titanium, 0.01-0.02 percent of boron, 0.01-0.03 percent of tungsten, 0.01-0.3 percent of tantalum, 0.02-0.06 percent of rare earth and the balance of nickel and other unavoidable trace impurity elements. The preparation method for the nickel-based alloy with high grain-boundary strength comprises the following steps of (1) preparing raw materials: preparing a proper amount of Incone1617 main material and a small amount of Re, B, Ta and W for component adjustment; and (2) feeding the materials for smelting: putting the materials Cr, Mo, Ta and W which have high smelting points to the bottom of a crucible, then adding the Incone1617 furnace material, sequentially adding the rest of the raw materials, covering the materials with a slag removal agent, and smelting the materials in a vacuum smelting furnace. By the adding of B, Ta and the rare earth elements, the nickel-based alloy is low in environment sensitivity and can achieve effects of purifying the grain boundary and effectively improving the grain-boundary bonding strength.