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69results about How to "High contact fatigue strength" patented technology

Heat treatment method for inlaid backup roll sleeve

The invention discloses a heat treatment method for an inlaid backup roll sleeve. The heat treatment method comprises the following steps: A, smelting a steel ingot, and then forging a roll sleeve blank, followed by rough machining and flaw detection; B, performing hardening and tempering on the roll sleeve blank, heating the roughed roll sleeve, and performing tempering on the roll sleeve; C, performing semi-finish turning machining and flaw detection on the roll sleeve; D, hoisting the semi-finish turning machined roll sleeve to a power-frequency quench machining tool, carrying out overall induction heating by using a dual-power frequency power source, adopting a water quenching method; subsequently, carrying out tempering; E, detecting metallographic structures of inner and outer surfaces of the roll sleeve, and detecting residual stress and hardness of the outer surface; F, performing finish machining on the roll sleeve; and G, assembling a roll shaft, and performing finish machining on the assembled roll. The heat treatment method for the inlaid backup roll sleeve of the present invention meets the requirements in structure, hardness and residual stress aspects, and meanwhile, such properties as abrasive resistance and contact fatigue strength of the roll sleeve also are improved.
Owner:SINOSTEEL XINGTAI MACHINERY & MILL ROLL

Steel ball special for large-sized offshore wind turbine generator bearing and manufacturing process of steel ball

ActiveCN102865301AIncrease the secondary stable tempering technologyAdd NDTFinal product manufactureBearing componentsSteel ballQuenching
The invention relates to a steel ball special for a large-sized offshore wind turbine generator bearing and a manufacturing process of the steel ball. The roundness of the steel ball is less than or equal to 0.8 mum, the hardness is 59-64 HRC, the single-grain hardness grain difference is less than or equal to 0.8 HRC, the batch hardness difference is less than or equal to 1.2 HRC, the core hardness is 54-60 HRC, the retained austenite is 8-13 percent, the metallographic structure is 2-3 grade, the surface roughness is less than or equal to 0.8 mum, and the crush load and the compression ratio of the steel ball are 1.2 times greater than international crush load and compression ratio. By selecting raw materials, adopting hot extrusion continuous forming during ball billet forming, adopting a water soluble quenching agent to perform multi-stage quenching during thermal treatment, increasing a secondary stable tempering technology, increasing various technologies such as eddy current nondestructive flaw detection in a process flow, the steel ball has the characteristics of good high contact fatigue strength, high wear resistance, high elastic limit, proper hardness, high impact toughness, good dimensional stability and the like.
Owner:JIANGSU LIXING GENERAL STEEL BALL

Nanoscale metal ceramization lubricant additive and preparation method therefor

InactiveCN103396862ARetain plasticityBoth super hard and super wear-resistantAdditivesChemical structurePhosphate
The invention provides a nanoscale ceramic metallization lubricant additive and a preparation method therefor, and aims to provide a nanoscale ceramic metal lubricant extreme pressure-antiwear additive which can improve the friction pair antiwear property and has self-lubricating functions. The invention is realized through the following technical scheme: quantification of raw materials is carried out according to the formula of the lubricant additive; nano ceramic powder is added into the raw materials; the above mixture is placed in a reactor wherein a coupling reaction is carried out under the atmosphere of hydrogen, nitrogen and helium; a coupling agent is added and the mixture is subjected to a coupling reaction to form ceramic primer gel with chemical covalent bonds, and one end of the coupling agent is a silicon-oxygen connection structure-Si[OEt]3 and the other end of the coupling agent is a chemical structure with molybdenum phosphate and boron nitride primer functional groups; the gel is added into a reactor through a metering pump, and is subjected to pressurization and carbon dioxide supercutical fluid solvent exchange, and the liquefied gel is converted into gasified gel; the gasified gel is then placed in a reactor atmosphere protection sintering furnace and sintered; the sintered ceramic coupling objects are placed in a stirring mixer and mixed with a surfactant additive, a dispersant, and a basic oil solvent to obtain finished products.
Owner:韩炳德

Thermal treatment method for reducing secondary gear ring nitrogenized deformation

The invention provides a thermal treatment method for reducing secondary gear ring nitrogenized deformation. The method comprises the following steps: (a) tempering after a secondary gear ring is roughly processed; (b) tempering; (c) processing by a gear milling machine, and destressing at high temperature; (d) processing by a gear grinding machine, and performing gas nitrogenization, wherein the gas nitrogenization comprises the following steps: uniformly fixing and supporting a plurality of cylindrical clamps in a gear ring groove; flushing a gear ring in a bell type gas nitrogenation oven, heating, and introducing 8-12m<3>/h nitrogen for 3-5 hours; heating to 400-500 DEG C, introducing 4-8m<3>/h ammonia, and insulating for 0.2-0.8 hours; heating to 500-550 DEG C, controlling the flow rate of ammonia to be 10-15m<3>, and penetrating for 60-65 hours, wherein Kn is 6; turning to diffuse, controlling the flow rate of ammonia at 4-6m<3>/h, and diffusing for 30-32 hours, wherein Kn is 2; cooling along with the oven, introducing 8-12m<3>/h nitrogen while cooling; moving the heating mantle when the temperature is reduced to 400-500 DEG C; discharging parts from the oven when the temperature is reduced to lower than 90 DEG C. The thermal treatment method has the characteristics that the deformation is small, a high-hardness high-wearing nitride layer can be obtained on the surface, the contact fatigue strength can be improved, the drawing performance and accurate requirement can be fulfilled, the product quality can be improved, and the like.
Owner:HANGZHOU ADVANCE GEARBOX GRP

Process for strengthening nodular cast iron and finished product thereof

The invention discloses a process for strengthening nodular cast ion and a finished product thereof. The process comprises the following steps of: putting cleaned nodular cast iron parts into a carburizing furnace; performing carbonitriding, namely adding methanol and ammonia at the temperature of between 800 and 840 DEG C, wherein the addition of the methanol is 80-120 drops / minute, the adding volume of the ammonia is 1 to 5 percent of the volume of the methanol cracked gas, the carbon potential is maintained to between 0.8 and 1.2 percent, and the processing time is 2 to 4 hours; and performing quenching to obtain a part finished product. In the carbonitriding process, the decarbonization preventing technological measure is adopted, the metallographic structure of the finished product comprises a surface layer, a sublayer and a substrate in turn, the surface layer is a granular or continuously distributed compound layer, the sublayer is hidden needle-like nitrogenous martensite, retained austenite and graphite, and the substrate is thin needle-like martensite, retained austenite and graphite. The process can improve the scratch resistance, wear resistance and contact fatigue strength, can effectively prevent full decarbonization during carbonitriding of the nodular cast ion, and has the advantages of low process difficulty and low production cost.
Owner:DONGFENG MOTOR CORP HUBEI

Carbon-carbon composite guide rail and preparation method thereof

The invention discloses a carbon-carbon composite material guide rail for an aircraft braking wheel and a preparation method of the carbon-carbon composite material guide rail. The carbon-carbon composite material guide rail is made of a carbon-carbon composite material, and the cross section of the guide rail is U-shaped, V straight channel-shaped or V-shaped. The carbon-carbon composite material guide rail is prepared through a composite process of dipping and chemical vapor deposition, or a chemical vapor deposition method. The carbon-carbon composite material guide rail disclosed by the invention has the advantages of light weight, impossibility of softening deformation at a high temperature and the like, is used as an airplane wheel guide rail, can avoid steel guide rail corrosion, deformation, cracks and a dynamic disk clamping stagnation problem caused by guide rail deformation, and can ensure that a steel clip does not need to be arranged on a dynamic disk key groove, so that potential safety hazards of rivet fracture and steel clip falling are eliminated. The carbon-carbon composite material guide rail is used for a brake shell, and replaces a convex key on the brake shell to match with a static disk key groove, so that the problem of abnormal wear of the side surface of the static disk key groove is fundamentally solved.
Owner:XIAN AVIATION BRAKE TECH
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