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297 results about "Computer-aided manufacturing" patented technology

Computer-aided manufacturing (CAM) or Computer-aided Machining is the use of software to control machine tools and related ones in the manufacturing of workpieces. This is not the only definition for CAM, but it is the most common; CAM may also refer to the use of a computer to assist in all operations of a manufacturing plant, including planning, management, transportation and storage. Its primary purpose is to create a faster production process and components and tooling with more precise dimensions and material consistency, which in some cases, uses only the required amount of raw material (thus minimizing waste), while simultaneously reducing energy consumption. CAM is now a system used in schools and lower educational purposes. CAM is a subsequent computer-aided process after computer-aided design (CAD) and sometimes computer-aided engineering (CAE), as the model generated in CAD and verified in CAE can be input into CAM software, which then controls the machine tool. CAM is used in many schools alongside Computer-Aided Design (CAD) to create objects.

Method and system for computer aided manufacturing measurement analysis

The invention relates to a computer-based method and system to facilitate quality control for manufactured assemblies based on computer aided design (CAD) files. The instant invention mitigates the problems encountered with large CAD files by decomposing each of such files into a multi-file format. A large CAD file is thereby broken-down into smaller files that organize the information contained in the larger file. The organization is performed in such a way that the information pertinent to the measurement process is segregated into a different smaller file than the information not needed to calculate measurements. Thus, the computer running the computation accesses a smaller file containing a higher percentage of required information. Additionally, assisting the user in coordinating a match-up between the physical surfaces being measured and the proper associated CAD model version of that surface further increases the handling speed. In particular, the instant invention uses selection regions for each surface. A selection region consists of the representation of a three-dimensional rectangle region just large enough to enclose each individual surface. A selection region indexes each surface. Thus, when a measurement point is taken, a list of surface regions is automatically scanned in order to determine which region contains that point. The corresponding distance of that measurement point to the surface is then calculated.
Owner:FARO TECH INC

Intelligent numerical control machining programming system and intelligent numerical control machining programming method for aircraft structural parts

The invention relates to an intelligent numerical control machining programming system and an intelligent numerical control machining programming method for aircraft structural parts. According to the system, an existing CAD / CAM (Computer-Aided Design / Computer-Aided Manufacturing) system is taken as a platform; the system comprises a model detection module, a process scheme automatic generation module, a process resource and knowledge base management model, an automatic programming subsystem module and a numerical control program intelligent optimization module. The system is established on the basis of a three-dimensional model, the numerical control machining programming specialization process of the aircraft structural parts is relatively systematically and accurately reflected and supported, the man-machine interaction operation required in the technological preparation and programming process can be greatly reduced, the problems of unstable program, long programming period and the like caused by interactive programming based on universal platform and artificial experience are effectively solved, the numerical control machining preparation and programming efficiency and quality can be obviously improved, and the specialization level and the intelligence level of the CAD / CAM system are promoted.
Owner:SHENYANG AIRCRAFT CORP

Ruled surface impeller tool path planning and processing method

InactiveCN101271326ASolving the Problems of Five-Axis MachiningHigh degree of automationProgramme controlComputer controlImpellerNumerical control
A path planning processing method of a ruled surface impeller cutter relates to a cutter path planning processing method. The invention solves the problems of the prior numerical control processing method of an impeller part, the problem are that a whole processing technology for processing a integral type ruled surface impeller is not proposed, the calculating method of the point of a knife centre or the point of a knifepoint is not given, the processing cutting efficiency is low, the operation is complex and the degree of automation is low and the five-axis processing of the ruled surface impeller can not be realized etc. The main steps of the method are the establishment of the calculator assistant manufacturing model CAM of an impeller part, the calculation of the vector of a cutter shaft, the calculation of the point of the knife centre, the planning of whole cutter path and the achievement of the processing of the impeller part. The method of the invention solves the problem of the five-axis processing of the ruled surface impeller and has the advantages of high processing cutting efficiency, easy operation and high degree of automation The ruled surface impeller processed by the method has the characteristics of orderly linage of flow passage, symmetrical structure and the uniform distribution of cutter path at the surface of the flow passage, thus reducing the workload of subsequent polishing processing greatly.
Owner:哈尔滨工大宏图橡塑科技有限公司

Five-axis side milling machining process parameter design method

InactiveCN102129232AAccurate transient cutting thicknessImprove accuracyNumerical controlNumerical controlAnalytical expressions
The invention discloses a five-axis side milling machining process parameter design method, belongs to the technology of numerical control (NC) machining, and solves the problem that real machining conditions cannot be reflected in cutting force calculation in the conventional process parameter design method. The method comprises the following steps of: tool path planning, cutting force calculation and process parameter optimization; in the tool path planning step, an NC code is generated by using computer-aided manufacturing (CAM) software; in the cutting force calculation step, first, a continuous tool path is generated from the NC code; then, a cutting thickness is obtained; and finally, the cutting force is calculated according to the cutting thickness; and in the process parameter optimization step, whether the calculated cutting force is not greater than a design threshold is judged; if the calculated cutting force is not greater than the design threshold, the NC code, the cutting depth and a feed rate are taken as input parameters; and otherwise, an NC code is regenerated. In the method, the real machining conditions are reflected by utilizing a tool enveloping surface analytical expression and the obtained transient cutting thickness is more accurate, so that the accuracy of the calculation of the cutting thickness and the cutting force is improved, and reliable assurance is provided for precisely and efficiently machining a spatial curved surface.
Owner:HUAZHONG UNIV OF SCI & TECH

Acceleration and deceleration look-ahead control method for high-speed machining of numerical control machine tool

The invention relates to an acceleration and deceleration look-ahead control method for the high-speed machining of a numerical control machine tool. The method comprises the following operation steps of: (1) cutting the curve data of a CAD/CAM (Computer-Aided Design/Computer-Aided Manufacturing) model into a NC (Numerical Control) curve data model according to a contour error; (2) inputting system parameters, such as interpolation cycle T, maximum speed Vmax, and the like, on the basis of a NC code; (3) carrying out microfield integral S-shaped speed planning on the basis of the system parameters and determining the corresponding speed (i is equal to 1:N, N is a look-ahead field number, that is to say, a speed value from the first field to the Nth field is determined) of all fields on a S-shaped speed curve; (4) determining a microfield adapting angle allowed passing speed (i is equal to 1:N); (5) determining a point at which the adapting angle allowed speed is smaller than planned speed; (6) outputting a machining interpolation point; and (7) executing the information and finishing the machining of parts by a motion control system. In the step (5), the reasonable speed at which the microfield machining can be carried out is determined on the basis of comparing the speed on the S-shaped speed curve with the adapting angle allowed passing speed, and thereby, the S-shaped speedcurve with highest efficiency is obtained; and finally, the machining interpolation point is output to the motion control system. According to the method, the machining precision is ensured, the machining efficiency is greatly increased, the flexible impact of the machine tool is effectively prevented and the service life of the machine tool and cutters is prolonged.
Owner:SHANGHAI UNIV

Cavity-characteristic-based high-efficiency rough machining method of aircraft structural part

The invention discloses a cavity-characteristic-based high-efficiency rough machining method of an aircraft structural part, which belongs to the technical field of CAD/CAPP/CAM (Computer Aided Design/Computer Aided Process Planning/Computer Aided Manufacturing). The method is characterized by comprising the following steps of: firstly, performing preprocessing such as input of a part and read-in of characteristic information of the part; selecting characteristic of a cavity to be subjected to rough machining, automatically generating a cavity rough machining region according to information such as rough machining margin, diameter of a tool and cutting depth of the tool, and calculating a plunge milling tool site for rough machining of the cavity; and finally, generating a plunge milling rough machining track and a saw tooth residue clear track according to a set feeding strategy. By utilization of the method, rough machining of the aircraft structural part is performed, so that the rough machining efficiency of the aircraft structural part can be greatly improved, the loss of the tool is reduced, and the cost is saved. The method has great application and promotion prospect in rough machining of a difficult-to-machine material of the aircraft structural part.
Owner:SUZHOU MACHINING PRECISION ELECTRONICS

Automatic generation method of plunge milling toolpath for corner features

The invention discloses an automatic generation method of a plunge milling toolpath for corner features, and belongs to the technical field of CAD (Computer-Aided Design)/CAPP (Computer-Aided Process Planning)/CAM (Computer-Aided Manufacturing). The automatic generation method comprises the following steps: firstly, conducting the pretreatment such as part selection, part feature information read-in and the like; secondarily, obtaining geometric surfaces needed in corner processing from the part feature information, and automatically calculating the corner plunge milling area geometric auxiliary point, the axial corner geometric auxiliary point and the plunger milling generation geometric auxiliary point according to information such as the plunger milling processing redundancy, the radius of a cutting tool in the former process or work step as well as the rough processing redundancy and the like; and finally, generating the plunger milling tooth-paths of all part corners through the auxiliary points automatically. The plunge milling tool-paths for corners, generated through the invention, are high in speed and high in accuracy rate, and can process a corner in a large processing area, a corner containing scattered surfaces, a five-axis corner, and a corner of which the proximal surface is a big-curvature side surface, so that the method solves the problem that the manual corner plunger milling programming process is trivial and complicated and low in efficiency. Through the invention, a good effect on plunger milling of corners of an aircraft structural part can be obtained.
Owner:SUZHOU MACHINING PRECISION ELECTRONICS

Integrated fiber post for dental restoration and preparation method thereof

The invention discloses an integrated fiber post for dental restoration and a preparation method thereof. The integrated fiber post for dental restoration is characterized by integrating a post and a core and comprising a post and core tail part and a head core part; the conical structure of the post and core tail part is consistent with the conical structure of a dental drilling head; the head core part is in an umbrella cap structure; the lower edge of the umbrella cap structure is fully matched with the residual part of a defected tooth; the outline part of the umbrella cap structure is fully matched with a crown part; and a porcelain crown is directly sleeved on the head core part. The method for forming and machining the integrated fiber post comprises the following steps of: (1) acquiring CT (computed tomography) data of the defected tooth; (2) reconstructing the three-dimensional model of the tooth and a post and core crown through a computer; (3) building a CAD (computer-aideddesign) model of the integrated post and core; (4) transferring the information of the CAD model of the integrated fiber post and core into a CAM (computer-aided manufacturing) numerical control center; and (5) cutting and machining the integrated fiber post and core by a machining center of a numerical control machine. The fiber post of the invention has improved strength, reduced post and core abhesion in application, and avoidances of breakage of tooth posts and failure of restoration caused by stress concentration.
Owner:北京欧亚瑞康新材料科技有限公司

Non-standard knowledge acquisition method used for constructing mechanical product design knowledge base

The invention discloses a method for obtaining irregular knowledge used for constructing a mechanical product design knowledge base. Aiming at the requirements for knowledge processing and knowledge base system development in the mechanical product design field, the invention defines the irregular knowledge, discloses a computation module for dividing irregular knowledge granularity by adopting granularity calculation principle, studies mechanical product design irregular knowledge base structure system and basic format, discloses an irregular knowledge base display method based on metadata, and invents a method for obtaining semantic matching, irregular knowledge base in serial data source, and multi-mode irregular knowledge based on irregular example knowledge obtaining of cluster analysis; and on the basis, designs a system frame and a prototype software system for mechanical product design knowledge base system construction and application. The invention can be used to solve the technical problem of treating irregular knowledge in an information processing system such as CAD (computer-aided design), CAM (computer-aided manufacturing), CAE (computer-aided engineering) or PDM (products data management) in manufacturing industry, so as to satisfy the requirements for the deepening development of the manufacturing industry information project technology.
Owner:SICHUAN UNIV

Method used for manufacturing multi-layer circuit board by employing 3D printing technology

The invention provides a method used for manufacturing a multi-layer circuit board by employing the 3D printing technology. The method is additionally provided with a heatproof insulation layer on the basis of an original printed circuit board. Raw material powder of the circuit comprises copper alloy powder and tin powder which are in a certain proportion, the heatproof insulation layer is ceramic powder, the 3D molding method is a laser irradiation molding method. During processing, the computer auxiliary manufacturing (CAM) technology is firstly utilized, circuit board design is accomplished on computer software and is transmitted to a 3D printer. The ceramic powder is fixed on the circuit board to form the heatproof insulation layer by utilizing the laser 3D printer, circuit molding of the powder is directly carried out on the heatproof insulation layer base body by utilizing the 3D printing technology, the steps above are repeated, and thereby the multi-layer circuit board is formed. Compared with a traditional printed circuit board, the multi-layer circuit board can be rapidly produced in a lab or under the small-batch production condition, moreover, the circuit does not easily generate defects, cost is low, response is rapid, equipment investment is small, and the method employing the 3D printing technology provides feasible small-batch customized production.
Owner:ANHUI NEOFOUND TECH +2
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