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86results about How to "Eliminate microcracks" patented technology

Method and system for scribing brittle ultrathin piece by water jet and laser

InactiveCN103358028AEliminate thermal effectsEliminate residual stress and micro-cracksLaser beam welding apparatusPhysicsSpray nozzle
The invention discloses a method and system for scribing a brittle ultrathin piece by a water jet and laser. According to the method, a laser beam penetrates through a water jet beam to focus on the surface of a workpiece; the distance between the center of the jet point, on the surface of the workpiece, of the water jet beam and the center of the focus point, on the surface of the workpiece, of the laser beam is equal to or smaller than 1-2.5 times the radius of the focus point, on the surface of the workpiece, of the laser beam. The distance between an intersection point I and an intersection point II is equal to or smaller than 1-2.5 times the radius of the focus point of the laser beam, wherein the intersection point I is the intersection point of the surface of the workpiece and the water jet beam generated by the jet nozzle of the system, and the intersection point II is the intersection point of the surface of the workpiece and the laser beam. The longitudinal center line of the jet nozzle coincides with the center line of the laser beam. A workbench is provided with a working cavity filled with water; a water layer with a thickness of 0.5-1.5 mm is arranged on the surface of the workpiece on the top surface of a boss at the top of the workbench; the overflow port of the working cavity is connected to a water tank; a water pump is used for pumping water in the water tank into the jet nozzle to generate the water jet. According to the invention, the laser is used for laser ablating and scribing, and the water jet beam is used for cooling and washing a processed area, so that the effect that a processed surface is free from recast layers, residual stress and micro cracks is achieved; the processing efficiency is improved.
Owner:GUILIN UNIV OF ELECTRONIC TECH

High-counter-pressure casting method for high-tensile and high-density aluminum silicon alloy

InactiveCN101569924AImprove micro-shrinkage feeding capacityImprove mechanical propertiesHigh densitySilicon alloy
The invention provides a high-counter-pressure casting method for a high-tensile and heavy aluminum silicon alloy, which relates to a counter-pressure casting method for the high-tensile and high-density aluminum silicon alloy. The invention solves the problem that the conventional counter-pressure casting technology cannot meet the requirement of producing castings with high mechanical properties and high density due to the limit on the density and internal quality increase of the castings. The invention has the following main steps of: regulating a counter-pressure casting machine to an operating bearing pressure of 3.0 MPa, preparing aluminum silicon alloy, controlling the temperature of the fusant after thinning and modification at 720 DEG C to 740 DEG C, and carrying out the liquid lifting, mold filling, pressurization, pressure maintaining and pressure relief of high-counter-pressure casting with the counter-pressure casting machine. The invention obviously eliminates internal pinholes, micro-shrinkage porosity and tiny cracks in the castings, and enhances the mechanical properties and density of the castings; because of small thermal resistance between the fusant and the mold wall, the setting rate of the castings accelerates, and the setting structure is obviously thinned, thereby further enhancing the mechanical properties of the castings. The method is especially suitable for the cast form of large-sized complex thin-wall parts.
Owner:HARBIN INST OF TECH

Combined machining method for blade air film holes and device thereof

The invention discloses a combined machining method for blade air film holes and a device thereof, and relates to the field of non-traditional machining. The combined machining method comprises the steps that the air film holes with the needed size are rapidly drilled in a thermal barrier coating high-temperature alloy matrix through laser heating auxiliary drilling; secondly, a drill bit rotatingat a high speed serves as a cathode, blades serve as an anode, the drill bit moves up and down, online electrolysis aftertreatment is conducted on part of the air film holes of the metal matrix, andthe defects of residual stress, a heat affected zone and the like in the drilling process are eliminated; and meanwhile, tiny abrasive particles are suspended in the electrolyte, tiny impact scratching is conducted on the hole wall under the driving of the drill bit rotating at a high speed, the similar grinding and polishing effect is achieved, and the quality of the whole inner wall of the air film holes including the thermal barrier coating is further improved. The method is simple and easy to implement, laser transmission is not affected by the surrounding environment, the environmental adaptability is high, repeated tool setting is not needed, and the defects that the thermal barrier coating cannot be machined through a conventional electric machining method, the single crystal alloylaser machining efficiency is low, and thermal damage is likely to be generated are overcome.
Owner:JIANGSU UNIV

Alloying-element-strengthened high-silicon aluminum composite and preparation method thereof

The invention provides a preparation method of an alloying-element-strengthened high-silicon aluminum composite and belongs to the technical field of material preparation. The preparation method is particularly suitable for preparation of electronic packaging material. The designed alloying-element-strengthened high-silicon aluminum composite comprises, by mass percent, 48.0%-52.0% of silicon, 0.5%-4.0% of X and the balance aluminum. The X is copper and/or magnesium. The preparation method of the alloying-element-strengthened high-silicon aluminum composite comprises the steps that a silicon source, an aluminum source and an X source are prepared according to the designed components, the prepared silicon source, the prepared aluminum source and the prepared X source are smelted, and then a melt is obtained; and atomized spray deposition is conducted on the obtained melt, so that a deposition preform is obtained, hot isostatic pressing treatment is conducted on the deposition preform, and then a finished product is obtained, wherein during hot pressing pressure treatment, the temperature is controlled to be 520-600 DEG C, and the pressure is controlled to be 150-200 MPa. The designed composite has the advantages of being excellent in comprehensive performance, outstanding in mechanical property, low in preparation cost and the like and is suitable for large-scale industrial production.
Owner:CENT SOUTH UNIV

Technological method for composite asynchronous polishing of ceramics using picosecond-nanosecond laser

The invention discloses a technological method for composite asynchronous polishing of ceramics using picosecond-nanosecond laser. The technological method comprises the steps of firstly, irradiatingthe ceramic surface to be machined through picosecond laser along a certain scanning trace, and removing micro protrusions of the ceramic surface, so that the preliminary flattening is achieved; meanwhile, generating a large number of micro-nano particles by using a removal mechanism for the electronic state of ceramic materials through picosecond laser, wherein the micro-nano particles exist at adjacent space areas of the irradiated ceramic surface; starting a low power nanosecond laser according to the preset time for tracing the scanning path of the picosecond laser, and irradiating and fusing the micro-nano particles uniformly distributed on the ceramic surface; and finally forming a compact and smooth fine-grain melted layer so that the polishing effect is achieved. According to the technological method, original pore cracks of the ceramic materials are repaired, and the shortcomings that a heat affected zone generated by traditional laser polishing is large and the material surface is liable to generate micro-cracks and pores are overcome; and low removal amount, high efficiency and accuracy and submicron-level fine polishing of the ceramic materials is achieved.
Owner:BEIJING UNIV OF TECH

Diamond cladded polarization maintaining optical fiber and manufacturing method thereof

ActiveCN105985014AStrong process scalabilityGood process scalabilityGlass making apparatusOptical fibre with polarisationBatch productionCore (optical fiber)
The invention discloses a diamond cladded polarization maintaining optical fiber and a manufacturing method thereof. The manufacturing method comprises the following steps that a chemical vapor deposition method is adopted to manufacture a core stress integrated rod, wherein the core stress integrated rod comprises a core layer, a stress layer and an outer cladding layer; the core stress integrated rod is machined to make a cross section diamond; a target rod with a diamond cross section is manufactured and is put inside a quartz glass sleeve, an outer spraying process is adopted to conduct deposition on the quartz glass sleeve, the target rod is removed to form a pure quartz glass diamond inner-hole sleeve after the deposition process is completed; the core stress integrated rod with the diamond cross section is placed in the pure quartz glass diamond inner-hole sleeve to form a polarization maintaining optical fiber perform, the olarization maintaining optical fiber perform is subjected to drawing to form the diamond cladded polarization maintaining optical fiber. The polarization maintaining optical fiber I good in process performance and product quality, high in manufacturing precision and finished product rate, good in machining adaptability and suitable for batch production.
Owner:武汉长盈通光电技术股份有限公司

High-air-tightness low-free-oxygen-content nano disperse copper alloy and short-process preparation technology

The invention discloses a high-air-tightness low-free-oxygen-content nano disperse copper alloy and a short-process preparation technology, and wherein the alloy components comprise Al2O3, Ca and La.The preparation technology is made by the following steps that preparing Cu-Al2O3 alloy powder by adopting an internal oxidation method, and then mixing the Cu-Al2O3 alloy powder with Cu-Ca-La alloy powder, wrap covering the mixed powder under the protection of argon, carrying out hot extrusion at 900-920 DEG C and then rotary forging, after rotary forging, the wrap covering is vacuumized to be less than or equal to 10<-3>Pa, the wrap covering is sealed and is placed in a nitrogen atmosphere with the temperature of 450-550 DEG Cand the pressure intensity of 40-60 Mpa for 3-5 hours. According to the preparation technology disclosed by the invention, the secondary solid reduction of Ca and La is utilized, so that residual free oxygen is effectively removed and the dispersion strengthening effect is achieved, and finally the high density is obtained through vacuum medium-temperature creep deformation. The disperse copper prepared by the invention has the advantages that low free oxygen content (<= 15ppm), high dimensional stability and good air tightness after hydrogen annealing, good in gas tightness, the gas leakage rate is less than or equal to 1.0*10<-10> Pa.m<3> / s, the preparation technology is suitable for industrial production and can be used as a variety of sealing device materials such as an electric vacuum shell sealing device and a novel energy automobile high-voltagedirect-current relay.
Owner:湖南高创科惟新材料股份有限公司

Laser machining method and system of surface composite micro-structure of nodular cast iron material

The invention provides a laser machining method and system of a surface composite micro-structure of a nodular cast iron material and belongs to the technical field of laser machining. The laser machining method and system utilize the feature that spherulitic graphite is randomly and evenly distributed in cast iron, and obtain micro-pit arrays in distribution of multiple diameters and depths through ablation of the spherulitic graphite; by adjusting the laser parameters, the micro-pit distribution of the ideal dimension proportion is obtained; and meanwhile, by means of the feature of a laserremelting technology, a surface of a lower roughness is obtained on the peripheral region of the micro-pits, and micro-cracks, scratches and other defects on the original material surface are eliminated. The laser machining method can achieve continuous one-time machining of the composite micro-structure surface, and eliminates the original scratches, micro-cracks and other defects of the materialduring machining at the same time. The prepared composite micro-structure surface has a low friction coefficient and high anti-wear performance. The laser machining method and system of the surface composite micro-structure of the nodular cast iron material has the features of being high in efficiency and low in cost and can achieve assembly line production.
Owner:SHANDONG UNIV OF TECH

TiAl-based alloy stator blade isothermal forming manufacturing method and device thereof

The invention discloses a TiAl-based alloy stator blade isothermal forming manufacturing method and a device thereof, and belongs to the field of isothermal forming manufacturing methods. The method comprises the steps of machining blank manufacturing, isothermal pre-forging, isothermal final forging and heat treatment. The invention further provides a TiAl-based alloy stator blade isothermal forming device. Compared with a commonly-adopted machining mode that a square blank is extruded and then machined into a part, and due to the fact that the extruded square blank is not deformed, the structure and the performance of a prepared stator blade cannot meet the design requirements, according to the method provided by the invention, blade forging forming is achieved through machining blank manufacturing and isothermal forming, and then the blank is machined into a part. Due to the fact that a TiAl-based alloy is large in deformation resistance and poor in shaping, a common forming methodcannot be achieved, so that the blank manufacturing process is a major problem needing to be solved. According to the method, turning is adopted for blank manufacturing, the blank shape is close to the shape of a final forging, isothermal forging forming is adopted, and uniform deformation of all parts of a blade is achieved, so that the structure and the performance of the blade forging are greatly improved.
Owner:SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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