75results about How to "Play a role in diffusion strengthening" patented technology

A high-temp self-lubricating non-Pb Cu-base composition has a chemical formula: Ni+C+Sn+Zn+MX+Fe+Cu, where MX is chosen from BN, Si3N4, SiC, Al2O3, TiN, TiC and Cr3 C2 and C is graphite and carbon fibres. It has anti-oxidizing, anti-corrosion and high-temp anti-wear characteristics.

The invention discloses a high-strength steel plate for ocean engineering and a production method thereof. The production method comprises the working procedures of smelting, continuous casting, heating, rolling, heat stacking and heat treatment, wherein the molten steel obtained in the smelting procedure comprises the following chemical ingredients with contents in percentage by mass: 0.05-0.09% of C, 0.10-0.30% of Si, 1.1-1.35% of Mn, not greater than 0.010% of P, not greater than 0.003% of S, 0.15-0.4% of Ni, 0.15-0.35% of Cr, 0.10-0.30% of Mo, 0.020-0.050% of Nb, 0.03-0.05% of V, 0.020-0.050% of TAl, and balance Fe and inevitable impurities; a quenching and tempering process is adopted in the heat treatment procedure; during the quenching process, a heating temperature is 880-910 DEG C, and a total heating time is PLC +(20-40) minutes; and during the tempering process, a heating temperature is 580-620 DEG C, a total heating time is 1.5-2 minutes per millimetre, and air cooling is carried out after discharge. According to the method disclosed by the invention, through adjustment and optimization for the proportion of alloy elements in the steel plate, and quenching and low-temperature short-time tempering, good mechanical properties of the steel plate can be guaranteed under a low-carbon-equivalent condition, and the steel plate is enabled to have good structure, comprehensive property and welding property.

The invention discloses a manufacturing method for an aviation 625 MPa grade large-size aluminum alloy pre-stretching plate and relates to the field of manufacturing methods for aluminum alloy pre-stretching plates. Through the manufacturing method, the technical problem that mechanical properties of existing aluminum alloy plates cannot reach the requirements of application to specific wing wallboards is solved. The manufacturing method for the aviation 625 MPa grade large-size aluminum alloy pre-stretching plate comprises the steps that raw materials are weighed according to the mass percentof elements, and the plate is obtained after smelting, casting, homogenizing annealing, hot rolling, solution treatment, pre-stretching and three-level aging treatment. The ultrahigh-strength alloy large-size wide plate prepared with the manufacturing method is the large-size pre-stretching plate which is flat in plate face, uniform in thickness, good in surface and stable in performance. The aviation 625 MPa grade large-size aluminum alloy pre-stretching plate prepared with the manufacturing method is widely applied to the fields of spaceflight, aviation and military and civil large aircrafts.

The invention discloses a special steel for a hardware tool and a preparation method thereof. The steel comprises the following chemical components in percentage by weight: 0.50-0.60% of C, 0.17-0.37% of Si, 0.20-0.50% of Mn, 0.008-0.020% of P, 0.001-0.005% of S, 0.25-0.60% of Cr, 0.20-0.35% of Ni, 0.07-0.25% of Cu, 0.010-0.030% of Ti, and the rest amount of iron and inevitable impurities. The preparation method is performed by a general clean steel process, and comprises the steps of steel smelting, LF furnace refining, continuous casting, casting blank heating, rolling, cooling and reeling. All alloy element components in the steel are designed to properly increase the carbon content and decrease the content of such noble metals as Ni and Cr; the process of smelting and rolling is controlled to obtain the special steel for the hardware tool with high-hardness surface and low-hardness-toughness heart material matrix; and the steel can satisfy the performance needed by the hardware tool and the target of optical economic benefit.

The invention discloses a FeCoNiCrMn high-entropy alloy and a method for preparing a wear-resisting coating through the alloy. Elements Fe, Co, Ni, Cr and Mn are adopted as main elements, and an alloysystem is formed according to the equal atomic ratio or the approximate equal atomic ratio. The preparation method of the wear-resisting coating of the FeCoNiCrMn high-entropy alloy is provided. FeCoNiCrMn spherical high-entropy alloy powder is prepared through a gas atomization method, and the wear-resisting coating is prepared on the surface of a stainless steel matrix through an atmosphere plasma spraying process. Spraying parameters are adjusted, the microstructure of the coating is optimized to the largest degree, and the spraying parameters with the optimal coating wear resistance are obtained. The prepared FeCoNiCrMn high-entropy alloy is good in coating combination, compact in structure and extremely good in wear resistance.

The invention provides a high-thermal-conductivity die-casting aluminum alloy. The high-thermal-conductivity die-casting aluminum alloy comprises, by mass percentage, 0.05%-1.0% of silicon, 0.3%-1. 3% of iron, 0.2%-2.0% of nickel, 0.1%-1.2% of magnesium, 0.001%-0.15% of strontium and the balance aluminum and inevitable impurities, wherein the mass percentage of the impurities is smaller than 0.2%. The invention further provides a preparing method of the high-thermal-conductivity die-casting aluminum alloy. The preparing method comprises the steps that at different heating temperatures, the aluminum and magnesium, an aluminum silicon intermediate alloy, a ferro-aluminium intermediate alloy, a nickel-aluminum intermediate alloy and an aluminum strontium intermediate alloy are sequentially fused to obtain aluminum, silicon, iron, nickel, magnesium and strontium fusion; then refined treatment and slag removal treatment are carried out to obtain an aluminum alloy solution; and the temperature of the aluminum alloy solution is adjusted to be 680 DEG C to 720 DEG C, and then casting can be carried out. The high-thermal-conductivity die-casting aluminum alloy has the excellent casting performance and has the higher heat conductivity coefficient.

The invention discloses a wear-resisting and high-hardness flux core wire. The wear-resisting and high-hardness flux core wire is composed of a flux core and a low-carbon cold-rolling steel tape sheath wrapped on the outer side of the flux core. The flux core comprises, by weight, 20-25 parts of low-carbon ferrochromium, 1.5-3 parts of titanium powder, 1-2 parts of nickel powder, 5-8 parts of calcium-silicon alloys, 2-4 parts of magnesium-aluminum alloys, 3-5 parts of electrolytic manganese, 1-2 parts of ferromolybdenum, 2.5-4 parts of ferroniobium, 1-2 parts of ferrovanadium, 3-5 parts of rare earth iron alloys, 3-5 parts of carbonate, 3-4 parts of graphite, 120-150 parts of iron powder, 0.5-1.5 parts of tungsten powder and 2-4 parts of calcium fluoride. The wear-resisting and high-hardness flux core wire has good welding performance, deposited metal tissue is compact, air holes and cracks are avoided, combination with base metal is good, performance is stable, and deposited metal has good wear resistance, corrosion resistance, high hardness and other performance.

The invention discloses a high-strength and heat-resistant aluminum alloy wire and a preparation method thereof. The aluminum alloy wire comprises the composition by the mass percentage: 0.6-1.2% of Mg, 0.4-0.8% of Si, 3.0-7.0% of W, and the balance Al. The preparation method of the aluminum alloy wire comprises the following steps: preparing an aluminum alloy liquid, atomizing the aluminum alloy liquid into a powder, screening the aluminum alloy powder, mixing a tungsten powder with the particle size of not more than 3 microns with the aluminum alloy powder, carrying out cold isostatic pressing on the mixed powder into a prefabricated blank, carrying out vacuum degassing, heating, hot-extruding into an aluminum alloy round rod, drawing into an aluminum alloy wire, and carrying out solid solution and aging treatment to obtain the high-strength and heat-resistant aluminum alloy wire. Tungsten is uniformly added into the aluminum alloy wire by adopting a powder hot extrusion method, the strength of the aluminum alloy wire is strengthened, the aluminum alloy wire has excellent room-temperature tensile mechanical properties, electrical conductivity and heat resistance, the room-temperature tensile strength is more than 320 MPa, the elongation rate is more than 9%, the electrical conductivity is more than 56%IACS, and after heat preservation for 1 h at the temperature of 250 DEG C, the tensile strength is more than 290 MPa and the tensile strength survival rate is more than 91%.

The invention relates to nitrogen containing martensitic stainless steel for a cutting tool and a manufacturing method of the nitrogen containing martensitic stainless steel. According to the technical scheme, chemical components of the nitrogen containing martensitic stainless steel for the cutting tool comprise 0.45wt%-0.70wt% of C, 13.0 wt%-17.0wt% of Cr, 0.10wt%-0.25wt% of N, 0.50wt%-0.80wt% of Si, 0.40wt%-1.0wt% of Mn, 0.0015wt%-0.0065wt% of Ca, not larger than 0.20wt% of V, not larger than 0.025wt% of Nb, not larger than 0.025wt% of Als, not larger than 0.03wt% of Mo, not larger than 0.008wt% of P, not larger than 0.005wt% of S and the balance Fe and inevitable elements. Meanwhile, the above chemical components meet the condition that C+N is 0.60-0.85wt%. The manufacturing method ofthe nitrogen containing martensitic stainless steel for the cutting tool comprises the steps of vacuum induction smelting, normal-pressure nitrogen increasing, casting, casting blank heating, rolling,quenching and tempering. The nitrogen containing martensitic stainless steel has the advantages that the alloy components are simple, the process is simple and convenient, the production cost is low,and large-scale production is easy. The manufactured nitrogen containing martensitic stainless steel for the cutting tool is high in hardness and good in toughness.

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 discloses a composite material tool electrode for electrolytic deposition and electric spark and a preparation method of the composite material tool electrode, and belongs to the technical field of electrical discharge machining of electric spark. The composite material tool electrode for electrolytic deposition and electric spark is characterized by comprising, by weight, 16-18% of SiC particles, 14-16% of TiB2 particles, and the balance copper as a base body, and the SiC particles and the TiB2 particles are embedded in the base body. Due to the fact that the SiC particles and the TiB2 particles are added to the copper base body, compared with the method that only the SiC particles are added in the initial research stage, on the premise of not changing the total adding amount, the specific heat capacity of the tool electrode is improved by 10%, the coefficient of thermal expansion is lowered by 3%, the hardness is improved by 5%, and therefore the loss of the electrode under same electrical discharge machining parameters is lowered by 7%, and the roughness of a machined surface is lowered by 2%.

The present invention is the technological process of adding aluminum and RE to produce high quality carbon steel ingot for high grade forging. During producing high quality carbon steel ingot, final deoxidizing agent of aluminum and RE is adopted and aluminum in 0.5-0.9 Kg and RE in 0.5-0.8 Kg for each ton of steel are added successively while smelting, and the steel ingot is demolded after 7-9 times the setting time. The high quality carbon steel ingot of the present invention may be used in producing high grade forging.

The invention provides a high-performance wrought magnesium alloy which can be extruded quickly and a preparation method thereof. The high-performance wrought magnesium alloy is prepared from, by mass, 1.0-3.0% of Al, 0.5-2.0% of Ca, 0.5-3.0% of Nd and/or Y, 0.1-1.0% of Ce and the balance magnesium and unavoidable impurities. Industrial pure Mg, industrial pure Al and middle alloys Mg-Ca, Mg-Nd, Mg-Y and Mg-Ce are adopted as raw materials and smelted to obtain an ingot casting; then, uniform thermal treatment, mechanical machining and plastic-deformation thermal machining are carried out to obtain a magnesium alloy material. The magnesium alloy material can be subjected to high-speed extrusion at the speed not lower than 15m/min. Moreover, the obtained material is excellent in mechanical performance, the yield strength and the tensile strength can reach 260 MPa and 290 MPa or above respectively, the specific elongation reaches 16% or above, and the application range of the magnesium alloy is further expanded.

The invention discloses an aluminum alloy plate strip for a lithium battery cover plate and a preparation method of the aluminum alloy plate strip. The aluminum alloy plate strip comprises the following components of, in percentage by mass, 1.18 wt%-1.8 wt% of Fe, Mn less than or equal to 0.395 wt% 0.03 wt%-0.08 wt% of Ca, 0.1 wt%-0.3 wt% of Si and the balance Al and inevitable impurities, wherein Fe + Mn is less than 2 wt%, Fe/Mn is more than or equal to 2.5, Mn + Si is less than 0.6 wt%, and (Fe + Mn + Ca)/Si is more than or equal to 2.5. According to the aluminum alloy plate strip for the lithium battery cover plate and the preparation method of the aluminum alloy plate strip, the alloy has good mechanical performance, forming performance and laser welding performance at the same time, especially the performance stability of a material can be improved, and a prepared explosion-proof valve has stable explosion pressure.