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160results about How to "Reduce interface stress" patented technology

Powder metallurgy preparation method of localization reinforced composite

The invention belongs to the technical field of composite preparation, and particularly relates to a powder metallurgy preparation method of a localization reinforced composite for manufacturing wear-resisting quick-wear parts of mining and building machines. The method comprises the following steps that (1) tungsten carbide powder and titanium carbide powder are used as reinforced particles, reduced iron powder and high-speed steel powder are used as a metal binder, and hard alloy powder is prepared according to a certain proportion; (2) the prepared hard alloy powder is put into a ball mill, and a process control agent is added for ball milling and mixing; and (3) a forming agent is added into the hard alloy powder subjected to uniform ball milling and mixing, and then the steps of mixing, prepressing, smashing, sieving particle making and the like are carried out. In a composite layer of the composite prepared through the method, discontinuous reinforcement areas are uniformly distributed in a continuous matrix area, cracks are not prone to being produced and expanding in the service process of the composite, and strength-toughness matching performance of the composite is achieved well; and the wear resistance of the composite can be obviously improved, and the service life of the composite can be obviously prolonged.
Owner:SICHUAN UNIVERSITY OF SCIENCE AND ENGINEERING

Buffer layer for sulfide solid-state battery, preparation method of buffer layer, and solid-state battery

The invention provides a buffer layer for a sulfide solid-state battery. The buffer layer comprises a polymer material and ethylene carbonate, and is formed in situ on an electrode plate through a buffer layer solution; and due to the existence of a polymer, poor physical contact between an electrode and an electrolyte caused by volume deformation of a positive electrode material in a charging/discharging process can be improved. The buffer layer is existent between the positive electrode and the solid electrolyte of the solid-state battery and between the negative electrode and the solid-state electrolyte, so that the solid-solid interface impedance can be reduced; and meanwhile, good ionic conductivity of the buffer layer can improve the lithium ion transmission capacity. The sulfide composite positive electrode in the solid-state battery provided by the invention contains the polymer material, and the existence of the polymer can improve the poor physical contact between the electrode and the electrolyte caused by the volume deformation of the positive electrode material in the charging/discharging process; and meanwhile, the solid-state battery contains the buffer layer, so that the solid-state battery has low interface resistance and high ionic conductivity, and is excellent in capacity and cycling performance.
Owner:SHANGHAI INST OF SPACE POWER SOURCES

In-situ non-crystallizing modification method for surface of metal material

The invention belongs to the technical field of modification of surfaces of metal materials, and discloses an in-situ non-crystallizing modification method for the surface of a metal material. The method comprises the steps that amorphous alloy components matched with components of a metal matrix material are selected based on the components of the metal matrix material; then, required simple-substance element powder except main elements of a metal matrix is matched according to the amorphous alloy components; after being mixed, the element powder is preplaced on the surface of the metal matrix; laser is adopted to directly irradiate the mixed powder and the metal matrix to melt the mixed powder and the metal matrix and mix the melts; and an amorphous alloy is generated through the in-situ alloying reaction of the mixed element powder and the main elements of the metal matrix under the condition of quick cooling, and an amorphous alloy surface is prepared. According to the method, the interfacial stress of the amorphous alloy surface and the metal matrix is effectively reduced, the thickness of the amorphous alloy surface is increased, and the surface performance of the metal material is remarkably improved; and the amorphous alloy surface prepared through the method is different from an amorphous alloy coating prepared through a traditional method, the amorphous alloy surface is generated through the in-situ alloying reaction on the surface of the metal matrix, the interface bonding is high, and the performance is excellent.
Owner:常熟市大地机械铸造厂

Low-loss optical fiber and manufacturing method thereof

The invention discloses a low-loss optical fiber and a manufacturing method of the low-loss optical fiber, and relates to the field of optical fibers. The low-loss optical fiber comprises a step change waveguide; the step change waveguide comprises a core layer, a core cladding transition layer, a core cladding interface transition layer, a deep fluorine-doped cladding, a cladding sleeve transition layer, a cladding sleeve interface transition layer and a sleeve layer, wherein the core layer, the core cladding transition layer, the core cladding interface transition layer, the deep fluorine-doped cladding, the cladding sleeve transition layer, the cladding sleeve interface transition layer and the sleeve layer are arranged in sequence from inside to outside; the core layer is made of a pure silicon core slightly doped with fluorine or boron, wherein the relative refringence between the core layer and the pure silicon core is 0-0.1%; the deep fluorine-doped cladding is made of pure silicon dioxide deeply doped with fluorine, wherein the relative refringence between the deep fluorine-doped cladding and the core layer is 0.24%-0.28%; the refractivity in the core cladding transition layer is distributed in a gradient change mode according to a parabola curve, wherein the range of the absolute value of stress coefficients is from 0.005 to 0.015; the base point temperature rises gradually from 900-950 DEG C to 1150-1200 DEG C. The attenuation coefficient of the low-loss optical fiber manufactured according to the manufacturing method can be reduced to less than 0.158 dB/km in a 1550 nm wave band.
Owner:FENGHUO COMM SCI & TECH CO LTD +1

Method for preparing titanium/diamond-like nanometer multilayer film on silicon surface

The invention discloses a method for preparing a titanium/diamond-like nanometer multilayer film on a silicon surface. The method concretely comprises the following steps of: drying a monocrystalline silicon substrate subjected to chemical cleaning in advance; putting the dried monocrystalline silicon substrate onto a rotating sample table of a cathode arcing device; performing vacuum pumping; introducing argon gas into a vacuum chamber; performing sputtering cleaning on the surface of the silicon substrate through an ion source; using high-purity metal titanium and graphite as targets, and using a direct current and pulse double-excitation-source cathode plasma discharge technology for respectively preparing a titanium nanometer function layer and a diamond-like film; and performing later-stage vacuum annealing treatment according to needs. The method has the advantages that the preparing process is simple; and the method can be used for preparing the diamond-like nanometer multilayer composite film with different surface structures. The titanium/diamond-like nanometer multilayer film prepared by the method provided by the invention has the advantages of high hardness, low stress and friction-reduction and abrasion-resistant performance.
Owner:TAIYUAN UNIV OF TECH

Method for printing combustion chamber lining by using GRCop-42 spherical powder

The invention discloses a method for printing a combustion chamber lining by using GRCop-42 spherical powder. The GRCop-42 alloy spherical powder comprises the following chemical components in percentage by weight: 2-4wt% of Cu, 2-4wt% of Cr and Nb. The method comprises the following steps of: 1) heating the spherical powder in vacuum, cooling the spherical powder along with a furnace, then performing ultrasonic vibration, screening the spherical powder and preparing to discharge the spherical powder into the furnace; 2) establishing a process model of a part, and slicing the model in layers to form a laser scanning path of each layer; 3) setting process parameters of powder laying and printing equipment, placing a rear bottom plate substrate, and fully laying the GRCop-42 spherical powderin a powder cylinder; 4) starting the equipment and starting printing and forming; 5) after laser scans one layer, descending a forming cylinder by one layer, then ascending the powder cylinder by one layer, laying a layer of copper powder on the processed layer surface by using the powder in the powder cylinder through a scraper, then descending the powder cylinder, and repeating the steps on each layer until the printing of the structure is finished; 6) performing annealing treatment; and 7) cutting and separating the structure from the substrate, and performing sand blasting on the surfaceof the structure. The method solves the problem of domestic application of advanced materials, and meets the preparation requirement of an aerospace copper alloy structure.
Owner:SHAANXI SIRUI ADVANCED MATERIALS CO LTD
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