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6results about How to "Improve assembly pass rate" patented technology

A blood collection tube cap apparatus for an automated assembly line

ActiveCN224411345UImprove work efficiencySubsequent assembly is quickly realizedBlood Collection TubeControl engineering
The utility model discloses a blood taking tube cover device for automatic assembly line, including two sliding frames and assembly seat, two sliding frames keep parallel, and the inboard slide connection of sliding frame has a plurality of sliding rings, and the fixed connection of between upper and lower sliding rings has two synchronous bars, and two synchronous bars respectively through the both ends surface of limiting fixture and with limiting fixture slide connection, and the inboard of limiting fixture has blood taking tube body, and the surface of sliding ring directly above blood taking tube body inserts and has cover body, the utility model discloses two sliding frames are set up to convey blood taking tube body and cover body respectively, and every group sliding ring is connected with synchronous bar, thereby guaranteeing that both are always on same vertical line in the conveying process, guaranteeing that subsequent assembly can be realized fast through pressing, need not using complex machinery to position, and the accurate alignment of both can be realized only through mechanical linkage, effectively shorten single assembly positioning time, and the efficiency of assembly line operation is improved significantly.
Owner:SICHUAN MINGYUAN WELLCOME TECH CO LTD

Heating assembly, aerosol generating device and aerosol generating system

ActiveCN222466092UImprove assembly pass rateIncrease productivityTobaccoPhysicsAerosol Solution
The embodiment of the utility model discloses a heating assembly, an aerosol generating device and an aerosol generating system.The heating assembly comprises a mounting support, a heating part and a sealing part; the mounting support is provided with a mounting groove; the heating piece is used for heating the aerosol generating substrate, the two ends of the heating piece in the axial direction are the first end and the second end respectively, and the first end is arranged in the mounting groove; the sealing piece is clamped between the peripheral wall of the heating piece and the groove wall of the mounting groove in a sealing manner; wherein the peripheral wall of the heating piece is further provided with a limiting face facing the first end, and the sealing piece abuts against the limiting face. According to the heating assembly provided by the embodiment of the invention, one end of the sealing element is limited through the limiting surface, so that the probability of displacement of the sealing element on the heating element is reduced, the assembly qualification rate of the sealing element is improved, and the production efficiency of the heating assembly is improved.
Owner:SHENZHEN MERIT TECH CO LTD

A UAV aileron structure

ActiveCN224739655UAccurate control responseImproved control response
The utility model provides a kind of unmanned aerial vehicle aileron structure, comprising: composite skin, it is cylindrical structure, and at least one weight-reducing hole is set on it and passes through, both ends of weight-reducing hole and the both ends of cylindrical structure are through-penetrating;Two mounting plates are respectively installed in the opposite two sides position of composite skin, and the side surface of mounting plate close to composite skin is provided with the protruding part compatible with the weight-reducing hole of composite skin, the protruding part can be embedded in weight-reducing hole, so that the end of mounting plate and composite skin is fixed together.The utility model can realize once solidification forming by the cooperation of composite skin and mounting plate, and the forming manufacturing operation of aileron can be completed, through end insertion type connection, ensure the high coaxiality of left and right mounting plates, forming process is simple, forming efficiency is higher, and it is more stable and safe, solve the problem of the difference of coaxiality, assembly complex, weak overall rigidity of traditional multi-component assembly aileron.
Owner:TIANJIN QUANHUA TIMES AEROSPACE TECH DEV +1

Full-automatic solid tire press-fitting machine

This utility model discloses a fully automatic solid tire pressing machine, aiming to solve the technical problems of poor versatility, excessive manual intervention, and insufficient pressing efficiency and accuracy of existing solid tire pressing equipment. The pressing machine includes a conveyor roller conveyor, a four-column tire press, a lower cylinder displacement sensor, a lower tire pressing fixture, a solid tire, a solid tire rim, a rim positioning fixture, a lower lifting cylinder pin, a pin cylinder, a lower fixture lifting cylinder, a tire rim transfer arm, a pressing cylinder displacement sensor, a tire pressing cylinder, an upper tire pressing fixture, a tire centering arm, a roller conveyor motor, a lower lifting cylinder pin shaft, and an electrical control system. The self-adaptive clamping structure of the tire rim transfer arm adapts to workpieces of different specifications, and the dual displacement sensors achieve precise control of pressing force and displacement. Combined with the automated transfer and loading / unloading mechanism, the entire process is automated.
Owner:SHIYAN HENGRUI MACHINERY EQUIP CO LTD +1

A post-processing device for cable joint sheath processing

ActiveCN121440330BImprove assembly pass rateresolve skew
This invention discloses a post-processing device for cable joint sheath processing, belonging to the technical field of cable joint sheath processing. It includes: a support platform; an electric turntable fixedly connected to the upper surface of the support platform; multiple limiting plates arranged in an equidistant ring on the surface of the electric turntable; a tinning mechanism fixedly connected to one side of the electric turntable; a clamping mechanism adapted to the limiting plates fixedly connected to one side of the tinning mechanism; a sheath assembly mechanism for assembling the sheath fixedly connected to one side of the clamping mechanism; and a detection and unloading mechanism fixedly connected to one side of the sheath assembly mechanism. The tinning mechanism, clamping mechanism, sheath assembly mechanism, and detection and unloading mechanism are arranged in a ring around the outside of the electric turntable. A storage box is fixedly connected to one side of the support platform. This invention, in addition to processing cable joint sheaths, also enables multi-station distributed work and automated assembly and identification.
Owner:LIANYUNGANG HUIZHOU CONSTRUCTION ENGINEERING CO LTD

Assembling and connecting method and structure of forced ignition type aviation piston engine combustion chamber

PendingCN119435199AReduce side stress levelsReduce scaling differencesInternal combustion piston enginesGas turbine plantsCombustion chamberHeat balance
The invention relates to an assembly connection method and structure of a forced ignition type aviation piston engine combustion chamber, the structure comprises a cylinder body, a cylinder cover, a screw and a gasket, the cylinder cover is provided with a taper hole corresponding to a threaded connection hole of the cylinder body, the screw comprises a threaded section, a taper rod section and a screw head, and the screw is connected with the cylinder body at the threaded section. And meanwhile, the conical rod section is attached to the conical hole, so that the stress contact area between the screw and the cylinder cover is increased, additional torque formed by uneven combustion stress of the cylinder cover on the screw can be decomposed through conical surface fit, the axial tension borne by the cylindrical screw is reduced, and the difference of the expansion amount of each screw group on the cylinder cover is reduced. According to the method, through optimized and innovative design of a connecting fastener and a matching part, on the basis of a temperature difference assembly method, a cylinder cover is heated to 110 DEG C in advance, primary assembly is completed in a near-vacuum environment, pre-tightening force is loaded step by step, secondary loading of screws is conducted after heat balance is achieved between the connecting piece and the cylinder cover, and then the cylinder cover is assembled. And it is ensured that the pre-tightening force meets the design requirement, and then the assembling quality and sealing reliability are improved. The sealing performance of the flange face of the combustion chamber is improved, the system assembling difficulty is reduced, the thermal shock resistance of the structure is enhanced, the structure adapts to the offset combustion chamber layout, and the safety and reliability of an engine are guaranteed.
Owner:CHONGQING AEROSPACE ROCKET ELECTRONIC TECH CO LTD