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118 results about "Grit blasting" patented technology

Method and apparatus for applying external coating to grid array packages for increased reliability and performance

A method and apparatus are disclosed for selective removal of a conformal coating from the solder balls of grid array packages such that the benefits of the coating are realized. An ancillary benefit of the invention is improved process-ability of the grid array package by improving the mechanical containment of the solder during the reflow process and improved electrical isolation between the individual solder attachment points. For example, a method for coating a ball grid array is provided, which includes coating the ball grid array with a thin layer of parylene. Next, the solder ball side of the part is butter smeared or squeegeed with a water soluble coating and assembled wet. A mask having holes in the same pattern as the balls in the grid, and a thickness that is about 80% of the height of the balls, is applied to the solder ball side of the part. This side of the part is then butter smeared again with the water soluble coating, and the entire assembly is allowed to dry. At this point, about 20% of each parylene-coated solder ball protrudes higher than the surface of the mask. The solder ball side of the part is then grit blasted with an abrasive material. The extent that the abrasive material removes the parylene coating from the solder balls is limited by the mask and the layer of water soluble coating. Therefore, the grit blasting removes the parylene coating from only the protruding areas (e.g., about top 20%) of the solder balls. Water is then used to remove the water soluble coating, and the parylene coated part is baked to remove moisture. Thus, a parylene coated ball grid array (or column grid array) is provided that is highly impervious to moisture, has a very high dielectric strength, and thereby improves the electrical performance and reliability of the surface mounted part.
Owner:HONEYWELL INT INC

Sand dredger filling construction method of soft soil foundation embankment

InactiveCN102605697ASolve the leveling problemGuarantee the construction qualityRoadwaysFlatness problemLand resources
The invention discloses a sand dredger filling construction method of a soft soil foundation embankment. The sand dredger filling construction method comprises the steps of: (1) cleaning the surface of an embankment dredger filling field; (2) measuring and lofting, and setting an elevation mark of the dredger filling construction in a dredger filling region; (3) performing the dredger filling work in a manner of segmenting and layering, to be specific, forming a cofferdam, establishing plastic water discharge plates, building construction roads, distributing grit blasting pipe lines, dredger-filling the embankment, constructing a drain opening, and constructing water collecting wells; and (4) performing stability observation and settlement observation on the dredge-filled sand land of the embankment. The sand dredger filling construction method disclosed by the invention has the advantages of solving the flatness problem of road area at coastal tidelands, rivers, fishponds and the like, performing roadbed filling of municipal administration by fully making use of the characteristics of abundant fin sand resource in the local area, reducing exploitation usage amount of the land resource, decreasing construction cost while guaranteeing construction quality of the roadbed, being simple, convenient, feasible, efficient and practical, increasing working efficiency, saving cost and creating conditions for advanced construction of the next procedure.
Owner:TIANJIN 20 CONSTR

Seepage prevention method and fixture for aerial engine blade rabbet

The invention relates to a seepage prevention method and a fixture for an aerial engine blade rabbet. The seepage prevention method for the aerial engine blade rabbet comprises the following steps of: after heating the cleaned blade rabbet, winding aluminum oxide cotton on the outer surface of the blade rabbet, and clamping the aluminum oxide cotton wound on the blade rabbet by two metal clamps; then putting the blade rabbet wrapped by the aluminum oxide cotton into a metal protective jacket together with the metal clamps; and taking mixtures of ferro-aluminum powders, aluminum-silicon powders and tetra-methylammonium chloride as seepage agents, and carrying out gas aluminizing in a conventional method. The aluminum oxide, used in the invention, can resist corrosive atmosphere, and can not generate any chemical reaction and further generate pollution to a blade. Due to the adoption of the seepage prevention method and the fixture for the aerial engine blade rabbet, seepage layers on the rabbet part can be completely removed by only carrying out processes of wet grit blasting and coloring for one time, the repeated processes of dry grit blasting and the coloring are avoided, the production efficiency is improved for 1-2 times, and 30-40% of cost is saved; and furthermore, the operation is simple, and the seepage prevention effect is good.
Owner:AECC AVIATION POWER CO LTD

Molding process for straight bevel gear

The invention relates to a processing technique for a straight bevel gear and aims to provide a molding process for a straight bevel gear in order to improve the forging processing precision and processing efficiency of the bevel gear. The molding process comprises the following steps: (1) tooth die modeling includes rough forging tooth die modeling and finishing tooth die modeling; the pitch circle chordal tooth thickness of the rough forging tooth die is slightly smaller than that of the finishing tooth die, and the tooth whole depth of the rough forging tooth die is larger than the tooth whole depth of the finishing tooth die; the single tooth profile volume of a 0.992 rough forging tooth equals to the product of the single tooth profile volume of the finishing tooth die and 1.008; (2) the warm forging plastic forming is carried out; (3) hot forging edge cutting is carried out; (4) rough forged pieces are subjected to normalization, surface grit blasting and phosphorous saponification; (5) cold accurate alignment plastic forming is carried out. The processing technique for the straight bevel gear has the advantages that the quantity of raw materials is saved, the technological requirements on blank processing are lowered; the production cycle is reduced, and the cost is reduced; the product quality is stable, the product precision is high, the mechanical performance is good, the tonnage of required equipment is small, and the cost is low.
Owner:SICHUAN ZHONGYOU MACHINERY

Bidirectional injection moulding method of stator rubber of screw drilling tools

InactiveCN101637955AExtended use timeImprove glue injection rateLow speedVulcanization
The invention discloses a bidirectional injection moulding method of stator rubber of screw drilling tools, which belongs to the technical field of stator rubber injection of screw drilling tools andcomprises the following steps: grit-blasting; washing and drying; brushing adhesive; assembling a mould core into an internal hole of a steel pipe; putting a stator and an injection moulding mould inan oven and heating; carrying out vacuum negative-pressure rubber injection from two ends to the center of the stator; sealing the stator and putting the stator in a vulcanizing boiler to carry out vulcanization; taking out the stator and cooling; disassembling screw nuts, end caps and shims used for positioning on two ends of the stator, and pushing the mould core out of the rubber layer of the internal hole of the stator so as to be disengaged. The rubber injection method from two ends to the center of the stator prevents rubber from pressing the mould core to cause linear deformation of themould core, fundamentally eliminates the wrapping extent and the core shift of the rubber layer hole in the internal hole of the stator, greatly prolongs the service life of the stator, reduces air bubbles in the rubber layer of the stator and defects on the surface, such as pits, flow marks and the like and increases the qualification rate. The method overcomes the defects of low speed and longtime of rubber injection.
Owner:南京金三力橡塑有限公司

Metal tube taking plastic tube as liner and manufacturing method of metal tube

The invention provides a metal tube taking a plastic tube as a liner and a manufacturing method of the metal tube. The metal tube taking a plastic tube as a liner comprises a metal tube and a plastic composite tube stock; the plastic composite tube stock is formed by an outer layer hot melting adhesive layer and an inner layer plastic tube; plastic composite tube stock is manufactured online, the inner wall of the metal tube is subjected to sand blasting and shot blasting or grit blasting after being polished, the plastic composite tube stock is pulled into the well-processed metal tube, and the two ends of the plastic composite tube stock are sealed and inflated and are placed in a sealed steam room or baking room to be heated, such that the metal tube and the plastic composite tube stock are adhered fixedly, and trimming and spraying are performed. The invention further comprises a manufacturing method of the metal tube taking a plastic tube as a liner. The sealed steam room or baking room is adopted for heating, the product quality is stable, and percent of pass is high; a plurality of or even different models and types of tube stocks can be heated simultaneously, the total heating time is less, the production efficiency is high, the energy consumption cost for product heating can be saved, plants and production devices for production can be saved more, and investment cost is reduced.
Owner:肖和飞

Extrusion forming method for blade made of GH2787 high-temperature alloy

The invention discloses an extrusion forming method for a blade made of GH2787 high-temperature alloy. The extrusion forming method comprises the first step of heating a billet electric furnace to 1000-1050 DEG C, keeping the temperature for 3 minutes and performing direct extrusion forming on the blade, wherein according to the deformation amount of the blade, the head of the blade is 20%-30%, and the extrusion ratio of the body of the blade is 5-7; the second step of clearing the surface of a forge piece in a grit-blasting mode, the third step of performing vibrating finishing, clearing the surface of the forge piece and improving the roughness and light integrity of the surface of the forge piece, and the fourth step of performing solution treatment and aging treatment on the forge piece, wherein the temperature of the solution treatment is 940+ / -10 DEG C and is kept for 1-2 hours, then air cooling is performed on the forge piece, the temperature of the aging treatment is 780+ / -10 DEG C and is kept for 16 hours, and finally air cooling is performed on the forge piece. Compared with a traditional precision forging forming technology, the extrusion forming method has the advantages that four sets of tool design and manufacture are saved, the costs of the tool manufacture are saved by close to RMB 80,000 yuan, and meanwhile the preparation time of the blade is shortened; due to the facts that the forge piece of the blade is designed by adopting the method of adding allowance in equal proportion, and the allowance for machining the single surface of the blade is only 0.3+ / -0.2mm, the use rate of the material is enhanced.
Owner:SHENYANG LIMING AERO-ENGINE GROUP CORPORATION

Processing method for TC4 titanium alloy spiral groove screw tap

The invention provides a processing method for a TC4 titanium alloy spiral groove screw tap. The method comprises the working procedures of blanking, rough turning, finish turning, milling, benching, heat treatment, grit blasting, surface treatment, external grinding working procedure, thread grinding, cutter grinding, relief grinding, laser carving, and the like. In the thread grinding working procedure, a tail of a spiral groove is used as a grinding benchmark, threads are at least fed for three times to grinding and processing, the threads are relief grinded to meet the requirement, and annealing is strictly prevented; in the relief grinding working procedure, different relief grinding manners are adopted according to the actual demands of the production, one manner is that a 0.5-1mm of allowance is kept during relief grinding of a dorsal horn, and another manner is that only the about 0.1mm of allowance is kept during relief grinding of the dorsal horn. Through the adoption of the method disclosed by the invention, the accuracy requirement of the spiral groove screw tap based on the TC4 titanium alloy materials can be effectively ensured, the production efficiency is greatly improved, and even more, the processing problem that a spiral tooth back is a curve tooth surface is perfectly solved.
Owner:SHENYANG AIRCRAFT CORP
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