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2569results about How to "Shorten the processing cycle" patented technology

Method for thermal deformation error compensation of digital control gear hobbing machine

The invention discloses a method for thermal deformation error compensation of a digital control gear hobbing machine, which comprises the following steps of: 1, adopting temperature and displacement sensors to detect variable values of a temperature and a thermal deformation displacement on line when the digital control gear hobbing machine is in the course of working; 2, using a fuzzy clustering analytic method to calculate linearly dependent coefficients of variables of the temperature and the displacement, performing classification and optimization on the variable of the temperature, and determining the displacement variable Xi for model building and optimized p temperature independent variables T1, T2, T3, ..., and Tp; 3, adopting a multiple linear regression-least square method to establish a mathematic model of thermal errors and temperature variables; and 4, realizing online real-time compensation of thermal deformation errors of the digital control gear hobbing machine by using a zero programming system. The method solves thermal deformation error problems of a processing gear of the digital control gear hobbing machine, and by performing the online real-time error compensation on the digital control gear hobbing machine, the method improves the gear processing quality, the accuracy and the efficiency, reduces the rejection rate, saves the cost and shortens the processing cycle.
Owner:CHONGQING MACHINE TOOL GROUP +1

Multi-process planning comprehensive evaluation system and method based on digital twinning and deep learning

The invention relates to a multi-process planning comprehensive evaluation system and method based on digital twinning and deep learning, and belongs to the field of process planning virtual simulation. The system comprises a physical equipment layer, a data sensing layer, an information processing layer, a virtual space layer and a digital twinning layer, the data sensing layer collects related real-time data and historical data of the physical equipment layer in the machining process and sends the data to the information processing layer for data fusion analysis and processing; meanwhile, the acquired data is transmitted to a virtual space layer, and a dynamic virtual model corresponding to the physical entity is constructed under the guidance of requirements of related models in a digital twinning layer; the digital twinning layer is used for leading the other layers together, carrying out virtual-real interaction feedback, fusion analysis and iterative optimization, and carrying out comprehensive evaluation analysis on different process schemes of the to-be-processed part, so that process parameter optimization and process route improvement are realized. According to the method, the flexibility and dynamic adaptability of process planning are improved, the resource utilization rate can be improved, the processing period is shortened, and the production cost is reduced.
Owner:CHONGQING INST OF GREEN & INTELLIGENT TECH CHINESE ACADEMY OF SCI +1

Superplastic forming/diffusion bonding forming method for heat-resistant titanium alloy envelope

The invention belongs to the technical field of metal plastic processing, and aims at providing a superplastic forming/diffusion bonding forming method for a heat-resistant titanium alloy envelope with high material utilization ratio, high dimension control precision and high product performance. As a mould is adopted to control the appearance and dimension of a workpiece, the forming of a titanium alloy workpiece provided with a complex profile is completed, the production process of the heat-resistant envelope workpiece is shortened, and production cost is lowered; as the process of diffusion bonding followed by superplastic forming is adopted, the diffusion bonding is realized at the contact part of an inner envelope and an outer envelope, and the superplastic forming is realized at a separated part, the once-formed heat-resistant envelope with the complex profile and a hollow structure has the advantages of greatly improved structural integrity of a component, enhanced specific strength and specific stiffness of the component and increased welding rate of the diffusion bonding; the processed workpiece has the advantages of high dimension accuracy, high integral performance, light weight and the like; and the method disclosed by the invention has the advantages of shortened processing period, high material utilization ratio and lowered production cost.
Owner:北京普惠三航科技有限公司

Machining process of axial-flow type turbine blade

The invention discloses a machining process of an axial-flow type turbine blade. The machining process of the axial-flow type turbine blade comprises the following steps that two side faces are machined on a square blank stock through an end face end mill on an ordinary milling machine through two process of rough milling and finish milling, another two side faces are machined with the two machined side faces as base planes, and then the two end faces are machined through the end face end mill; a steam outlet side face is machined on one side face through two process of rough milling and finish milling, the position, close to the steam outlet side face, of the blade root end face is marked as C, a face which forms an acute angle with the steam outlet side face and is adjacent to the steam outlet side face is marked as N and is the inner radial surface, and the other three side faces are machined to be a parallelogram through rough milling and finish milling; central holes are drilled in the blade root end face and the blade crown end face; the blade type is roughly milled through the end face end mill, the blade root is roughly milled, and finally the blade crown is roughly milled; then the blade is installed on a five-axis numerical control machining center for alignment and is machined in a finish mode; a process head at the blade root end face is roughly sawn through a sawing machine; the turbine blade is detected according to the requirements of a drawing.
Owner:南京赛达科技有限公司

Combination machining tool for installation position of door pocket frame

The invention relates to a combination machining tool for an installation position of a door pocket frame. The combination machining tool comprises a numerical control doorframe fixed-length slot milling machine 1, a workpiece turnover machine 2, a numerical control doorframe drilling machine 3 and a numerical control doorframe hardware slot machining machine 4. The numerical control doorframe fixed-length slot milling machine takes out a pair of workpieces 5 from the bottom of a stock bin 11 of the numerical control doorframe fixed-length slot milling machine every time for conducting fixed-length cutting and decoration plate slot milling, wherein the front faces of the workpieces 5 face each other, and the workpieces 5 are stacked vertically. Then, the pair of workpieces are conveyed to the workpiece turnover machine, the workpiece turnover machine turns over the upper workpiece so as to enable the front faces of the pair of workpieces to face upwards, then the workpieces are fed into the numerical control doorframe drilling machine together, after all holes are machined in the workpieces, the pair of workpieces are fed into the numerical control doorframe hardware slot machining machine for machining doorframe hinge slots and doorframe spring bolt slots in the workpieces at the same time, and after the slot machining is completed, the workpieces are conveyed out in pairs. The machining tool has the advantages of being high in efficiency and product consistency and low in rejection rate.
Owner:NANTONG YUETONG CNC EQUIP CO LTD

Blisk manufacturing method based on 3D (three-dimensional) printing and electric spark finishing

The invention discloses a blisk manufacturing method based on 3D (three-dimensional) printing and electric spark finishing. The blisk manufacturing method includes: 1) manufacturing a wheel hub of a blisk, washing the wheel hub of the blisk prior to positioning and fixing the wheel hub on a numerical control table; 2) generating a slicing file; 3) manufacturing a blisk blank on the numerical control table by 3D printing according to the slicing file; 4) subjecting the blisk blank to hot isostatic pressing; 5) measuring a practical three-dimensional model of the blisk blank; 6) acquiring the accuracy error and deformation amount between the practical three-dimensional model of the blisk blank and a target three-dimensional model of the blisk; 7) determining spark machining allowance according to the accuracy error and the deformation amount; 8) subjecting the blisk bland to spark machining according to the spark machining allowance so as to obtain a blisk sample; 9) removing a fused layer on the surface of the blisk sample and grinding the blisk sample to obtain the blisk. The blisk manufacturing method based on 3D printing and electric spark finishing has the advantages of capability of blisk manufacturing, material saving and high machining precision.
Owner:XI AN JIAOTONG UNIV

Method for machining arc-tooth tenon blade of aircraft engine gas compressor

The invention belongs to machining technologies of blades of aircraft engine gas compressors, and provides a method for machining an arc-tooth tenon blade of an aircraft engine gas compressor. The method includes the steps that a blade blank with a root process boss and a blade tip process boss is clamped to a numerical control milling machine, and rough milling is conducted on the intake side and the exhaust side of the blade; the blade subjected to the rough milling is clamped in a positioning casting fixture and cast through low-melting-point alloy, and the outline of the cast blade is a cuboid; rough milling is conducted on the cuboid blade obtained after being clamped and cast on the numerical control milling machine so that a tenon and a margin plate can be formed at the root of the blade, and the blade root process boss is removed; the tenon is subjected to finish grinding on a six-axis creep-feed grinding center to be in an arc-tooth shape; the cuboid blade is placed into a melting furnace and heated to be 180 DEG C, and is taken out after the low-melting-point alloy melts; finish grinding is conducted on the intake side and the exhaust side on a numerical control abrasive belt grinding machine by using the tenon for positioning and clamping; and the blade tip is machined on a numerical control linear cutting machine by using the tenon for positioning and clamping, and the blade tip process boss is removed.
Owner:AECC AVIATION POWER CO LTD

Manufacturing method of mobile phone middle frame

The invention discloses a manufacturing method of a mobile phone middle frame. The manufacturing method comprises the following steps: S1, preparing a stainless steel rim; S2, putting the stainless steel rim into a pressure casting die, then adding smelted aluminum alloy liquid into the pressure casting die for pressure casting to form an aluminum alloy middle plate, and integrally forming an aluminum alloy-stainless steel middle frame from the aluminum alloy middle plate and the stainless steel rim; S3, covering the aluminum alloy middle plate with protective rubber capable of resisting corrosion of acidic liquid and alkaline liquid, putting the aluminum alloy-stainless steel middle frame into microhole treatment liquid for corrosion to form micro holes, and then removing the protective rubber; S4, forming a plastic structural member on the aluminum alloy-stainless steel middle frame through injection molding; and S5, performing post machining treatment on the aluminum alloy middle frame. The manufacturing method can avoid the problem that only the aluminum alloy is corroded, but the stainless steel cannot be corroded due to different activities of metals in the manufacturing process. According to the method, the machining amount of the whole structure of the middle frame can be reduced, the appearance effect is good, and the yield is high.
Owner:GUANGDONG JANUS SMART GRP CO LTD

Method for analyzing vibration characteristics of bearing retainer based on finite elements

The invention relates to a method for analyzing the vibration characteristics of a bearing retainer based on finite elements and aims at solving the problem that no automatic analysis procedure for the vibration characteristics of the bearing retainer is developed at present to prevent the frequency range of resonance of the bearing retainer of an aero-engine. The method is implemented through a step 1 of creating the three-dimensional model of the bearing retainer and saving the three-dimensional model under the working directory set by finite element software, a step 2 of establishing a finite element model and applying the rotating speed of the bearing to the finite element model for performing statics analysis and modal analysis, a step 3 of obtaining the stress and the strain as well as the inherent frequency and the corresponding formation thereof under the action of the rotating speed of the bearing, a step 4 of determining whether the stress and the deformation of the bearing retainer under the action of the centrifugal force meet the design requirements, and the like. The method for analyzing the vibration characteristics of the bearing retainer based on the finite elements is applied to the field of the vibration characteristics of the bearing retainers.
Owner:AVIC HARBIN BEARING

Ribbed steel bar truss concrete superimposed sheet and construction method thereof

A ribbed steel bar truss concrete superimposed sheet and a ribbed steel bar truss concrete construction method comprise a prefabricated layer and a superimposed layer. The prefabricated layer comprises a steel bar truss net and a concrete layer arranged on the lower portion of the prefabricated layer. A steel bar truss is composed of a lower chord steel bar, an upper chord steel bar and a web member steel bar connecting the lower chord steel bar and the upper chord steel bar. The steel bar truss net is composed of the steel bar truss, an additional steel bar shelved on the lower chord steel bar and vertical to the steel bar truss and a longitudinal steel bar in the lower portion of the prefabricated layer and parallel to the lower chord steel bar of the steel bar truss in the same plane. A plurality of concrete ribs are arranged on the upper end face of the concrete layer along the longitude direction and arranged in parallel. The superimposed layer is a cast-in-place concrete layer arranged on the prefabricate layer. A steel rib net is buried in the superimposed layer. The superimposed layer is connected with the upper chord steel bar in the steel bar truss of the prefabricate layer. The superimposed layer comprises an upper longitudinal bar and the additional steel bar vertical to the upper chord steel bar, and poured into a whole with the upper chord steel bar in the steel bar truss of the prefabricate layer and the web member steel bar. The ribbed steel bar truss concrete superimposed sheet and the ribbed steel bar truss concrete construction method have the advantages of being reasonable in steel bar overall arrangement, good in economy, convenient to hoist and transport, and effective in solving problem of sheet joint cracking.
Owner:SHANGHAI IRON & STEEL TECHN INST
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