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204results about How to "Uniform transition" patented technology

Efficient image rendering method based on modeling

The invention provides an efficient image rendering method based on modeling. With the method, a target image under free points view points can be generated. A light field model is adopted for recording surface information of a target; on the premise that that a three-dimensional grid model of the target and an appropriate amount of view point surrounding images of the target, through determining of a visible view point list of every vertex, the view points under which sampling is performed are determined; a triangular face ring of every vertex is selected as a sampling unit, virtual view points are generated with the triangulation method, and sampling information under the virtual view points is generated according to weight interpolations; sampling matrixes of all the vertexes are compressed with a matrix decomposition and compression method to facilitate transmission of the sampling information; in order to generate the target under the free view points, the three-dimensional grid model just needs to be projected to a screen coordinate system of new view points, and then a view under the new view points can be generated through reading of the sampling information. The method not only considers the problem of handling of a lapped seam phenomenon in texture mapping, but also reduces storage space for texture information and simplifies the rendering process.
Owner:UNIV OF SCI & TECH OF CHINA

Method for designing shading transition facility for road tunnel entrance

InactiveCN103334768AImprove accuracyTransitional realizationTunnelsMedium frequencyRoad surface
The invention relates to a method for designing a shading transition facility for a road tunnel entrance. The facility mainly comprises transparent toughened glass plates (2), a plurality of arched steel-structure upright columns (3), cicada-wing-shaped nontransparent shading films (5) and a shading transition retroreflection system, wherein the arched steel-structure upright columns (3) are gradually heightened outwardly from tunnel cave entrance end walls (1), and horn-shaped openings are formed by the arched steel-structure upright columns (3) and the transparent toughened glass plates (2) on the upright columns; the cicada-wing-shaped nontransparent shading films are arranged on inner layers of the transparent toughened glass plates, and contour line planes and side face projections of the shading films are Boltzmann curves, and the two sides of each arched steel structure are triangularly hollowed; the retroreflection system comprises medium-frequency steel-structure upright column contour marks (7), medium-frequency guardrail contour marks (8), high-frequency guardrail facade marks (9), high-frequency pavement marking lines (10) and high-frequency pavement protrusion marks (11). The shading transition facility has the advantages that the intense transition of space, luminance and reference of the tunnel entrance can be improved, and the black-hole effect on the tunnel entrance is relieved.
Owner:WUHAN UNIV OF TECH

Supersonic free vortex mixing layer wind tunnel

ActiveCN102023079AFlow field characteristics researchEasy to implementAerodynamic testingEngineeringAirflow
The invention provides a supersonic free vortex mixing layer wind tunnel. The wind tunnel comprises a transition section (1), a stabilizing section (2) and a spray pipe experimental section (3), wherein the transition section (1) is used for introducing air flow; the stabilizing section (2) is connected to the downstream side of the transition section (1) and is provided with a first separation plate (21) for separating the introduced air flow into two strands of air flow; the spray pipe experimental section (3) is connected to the downstream side of the stabilizing section (2) and comprises a spray pipe part (31) and a mixing experimental part (32); a transparent window is formed on the peripheral wall of the spray pipe experimental section (3); the spray pipe part (31) has a double free vortex spray pipe structure and is used for accelerating the two strands of air flow to form a free vortex state respectively; the mixing experimental part (32) is positioned on the downstream side of the spray pipe part (31) and is used for mixing the two strands of air flow in the free vortex state to form a free vortex mixing layer, so that velocity fields of the two strands of air flow at an inlet of the experimental part of the wind tunnel meet the requirement of supersonic free vortex distribution; therefore, an ideal supersonic free vortex mixing layer can be obtained in the wind tunnel.
Owner:NAT UNIV OF DEFENSE TECH

Composite material propeller blade sheet molding and transition connection technical study

InactiveCN106965457AGuaranteed continuous fiberUniform transitionDomestic articlesFiberPropeller
The invention relates to composite material propeller blade sheet molding and transition connection technical study. The technical study includes the following steps that (1) propeller blade sheet molding is carried out, wherein a paddle die and a reinforcing material are selected and treated, a plurality of layers of carbon fiber cloth is led out from the interiors of paddles in the paddle paving design process, and die assembly, pressurizing, heating, curing and aftertreatment re carried out after paddle paving is finished; and (2) paddle and paddle hub transition connection is carried out, wherein a fixing tool is used for fixing the multiple paddles, the paddles are subject to paving design, the carbon fiber cloth led out from the interiors of the paddles is paved inside the paddles, and the carbon fiber cloth led out from the interiors of the paddles and the propeller hub are subject to co-curing. The processes of sheet molding propeller blades and transition connection are adopted, the continuity of fibers inside the paddles and the paddle hub is guaranteed, the continuity of fibers on the inner wall of the paddle hub is guaranteed, the strength of the connecting position of the propeller blade and the propeller hub is improved, the process is simple, and the reliability is high.
Owner:武汉海威船舶与海洋工程科技有限公司 +1

Bulging bag type cooling structure for binary spray pipe

The invention relates to a bulging bag type cooling structure used for cooling a contraction section, an expansion section and the side wall face of a binary spray pipe. The cooling structure comprising bulging bags is designed. The multiple bulging bags are formed on an upper heat isolation liner through punching, and impact holes are formed in the top ends of the bulging bags. A trapezoid air collecting cavity is formed by each bulging bag and a lower heat isolation liner, wherein the part, on the right side of the bottom of each bulging bag, of the lower heat isolation liner is provided with an air film hole. The upper heat isolation liner and the lower heat isolation liner are connected through welding. When cooling air passes through the bulging bags, convection heat exchange on the cooling air side is enhanced under the flow disturbing action of the bulging bags, the cooling air flows into the trapezoid air collecting cavities through the impact holes in the bulging bags, and impact cooling is formed for the lower heat isolation liner; and after the cooling air is decelerated and pressurized in the trapezoid air collecting cavities, the cooling air flows out of the air film holes and is converged into hot flow, an air film is formed on the inner surface of the lower heat isolation liner, and the lower heat isolation liner is protected. The structure is high in cooling efficiency and is hardly influenced by the main and secondary flow pressure ratio, and cooling structure downstream expanding-direction and axial-direction temperature distribution and transition are uniform; and the cooling air utilization is improved.
Owner:AECC SICHUAN GAS TURBINE RES INST

Intelligent lighting system for continuous tunnel group

The invention discloses a tunnel lighting control system. The system comprises the steps of receiving environmental information parameters and a vehicle information parameter, calculating brightness required by each section in tunnels, judging whether to adjust color temperatures according to the environment visibility and transmitting calculated brightness values and color temperature values of the sections in the tunnels and approach sections outside holes to a lighting lamp dimming module; and receiving a dimming instruction sent by a software system control module by the lighting lamp dimming module, controlling LED lighting lamps of the sections in the tunnels to be adjusted to the brightness values and color temperature values set by the software system control module and achieving uniform transition of the lighting brightness between a last exit section and a next entrance section. The system control mode is simple and convenient; the brightness and the color temperatures of the sections in the tunnels in the holes of tunnel sections in the continuous tunnel group and the approach sections outside the holes are intelligently controlled according to different environmental parameters and traffic flow conditions; and the uniform transition of the lighting brightness of the lamps of the tunnel sections in the continuous tunnel group is ensured.
Owner:JIANGSU CHANGLU ENERGY TECH DEV CO LTD

Method for molding hard alloy functionally gradient materials

The invention discloses a method for molding hard alloy functionally gradient materials. The method includes mixing additives with alloy materials to obtain mixtures; carrying out compound pressure molding on the obtained mixtures in compound die groups to obtain blanks; sintering the blanks to obtain the hard alloy functionally gradient materials. The compound die groups comprise outer-layer dies with high expansion coefficients, intermediate transition-layer die groups and inner-layer dies with low expansion coefficients. The method has the advantages that the large and multi-component hard alloy functionally gradient composite materials which are of complicated contour structures and are free of obvious interfaces can be manufactured by the aid of the method; the sintered molded functionally gradient materials are provided with gradient grain structures along the thickness directions of the sintered molded functionally gradient materials, the gradient grain structures are provided with the different components, have different grain sizes and are free of obvious interfaces, and accordingly the molded hard alloy materials are excellent in comprehensive mechanical performance with high hardness, abrasion resistance, strength and toughness.
Owner:SEED TECH CORP LTD

Stelmor air-cooled line controlled cooling process for improving structure and performance of spring steel 55SiCrA coil rod

ActiveCN106734261AImprove the sorbitization rateReduce the presence of retained austeniteWork cooling devicesMetal rolling arrangementsPearliteThermal insulation
The invention provides a stelmor air-cooled line controlled cooling process for improving the structure and performance of a spring steel 55SiCrA coil rod. The controlled cooling process includes the steps that the finish rolling temperature is 790-820 DEG C, the blast capacity of the front three draught fans is controlled to meet the requirement that under various specifications, the lowest temperature of the third draught fan is within 680-710 DEG C, and the cooling speed of the front two draught fans is controlled within 5-13 DEG C per second; the blast capacity of a fourth draught fan and a fifth draught fan is controlled to make the coil rod temperature rise by 10-50 DEG C; the blast capacity of a sixth draught fan and follow-up draught fans is controlled to make the cooling speed within 3 DEG C per second, after the coil rod temperature is within 670-700 DEG C, thermal insulation covers are closed, and all the thermal insulation covers are opened before the temperature range; the cooling speed in the each thermal insulation cover is controlled at 0.8-2.0 DEG C per second, the draught fans are closed, the final two thermal insulation covers are opened, and the temperature of the coil rod discharged from each thermal insulation cover is 580-630 DEG C. In the process, the 55SiCrA coil rod is uniform in structure and composed of pearlite and a small amount of ferrites, under the various specifications, the percentage of area reduction can reach 60 or above, the sorbitizing rate and the plasticity reach high standards, and the strength, the hardness and the like can meet the performance requirement.
Owner:ZENITH STEEL GROUP CORP

Parallel tri-wire welding system and method

The invention discloses a parallel tri-wire welding system and method. The welding system comprises a wide-range welding power supply, a wire conveying mechanism with a tri-slot wire conveying wheel and a welding gun with a tri-hole conductive nozzle, wherein three welding wires are simultaneously conveyed to the welding gun through the wire conveying mechanism and separately penetrate through three independent holes which are distributed in the conductive nozzle at certain intervals; and welding waveforms output by the welding power supply are supplied to the welding wires through the conductive nozzle, and welding is carried out by simultaneously using the three wires. After the bottom ends of the three wires are molten, molten drops attract each other under electromagnetic action, and the molten drops stably and smoothly flow into a molten bath. The single-power-supply and parallel-tri-wire system has the advantages that the welding efficieny is increased, electric arc shapes and weld penetration size and contours are improved, welding flaws are reduced, and mechanical strength is improved; and at the same time, the three welding wires are stably conveyed by one wire conveying mechanism and go through one conventional welding gun, the operation is convenient, the reaching range of the welding gun is great, and manual, semi-automatic and robot welding demands can be simultaneously met.
Owner:AOTAI ELECTRIC

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
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