CN114297837A - Design method of intelligent management system of satellite final assembly production line - Google Patents
Design method of intelligent management system of satellite final assembly production line Download PDFInfo
- Publication number
- CN114297837A CN114297837A CN202111569630.7A CN202111569630A CN114297837A CN 114297837 A CN114297837 A CN 114297837A CN 202111569630 A CN202111569630 A CN 202111569630A CN 114297837 A CN114297837 A CN 114297837A
- Authority
- CN
- China
- Prior art keywords
- design
- management
- test
- equipment
- intelligent
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000013461 design Methods 0.000 title claims abstract description 136
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 93
- 238000000034 method Methods 0.000 title claims abstract description 74
- 238000007726 management method Methods 0.000 claims abstract description 135
- 239000000463 material Substances 0.000 claims abstract description 61
- 238000013439 planning Methods 0.000 claims abstract description 30
- 238000003860 storage Methods 0.000 claims abstract description 5
- 238000007728 cost analysis Methods 0.000 claims abstract description 4
- 238000012795 verification Methods 0.000 claims abstract description 4
- 238000012360 testing method Methods 0.000 claims description 61
- 238000005259 measurement Methods 0.000 claims description 23
- 238000007689 inspection Methods 0.000 claims description 12
- 238000005516 engineering process Methods 0.000 claims description 9
- 238000012384 transportation and delivery Methods 0.000 claims description 9
- 238000009826 distribution Methods 0.000 claims description 8
- 238000011161 development Methods 0.000 claims description 6
- 238000012544 monitoring process Methods 0.000 claims description 6
- 238000007619 statistical method Methods 0.000 claims description 6
- 238000012546 transfer Methods 0.000 claims description 6
- 230000010354 integration Effects 0.000 claims description 5
- 238000004458 analytical method Methods 0.000 claims description 3
- 239000013070 direct material Substances 0.000 claims description 3
- 229910052734 helium Inorganic materials 0.000 claims description 3
- 239000001307 helium Substances 0.000 claims description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 3
- 238000010191 image analysis Methods 0.000 claims description 3
- 230000002452 interceptive effect Effects 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 claims description 3
- 238000003672 processing method Methods 0.000 claims description 3
- 238000000275 quality assurance Methods 0.000 claims description 3
- 239000002994 raw material Substances 0.000 claims description 3
- 238000011084 recovery Methods 0.000 claims description 3
- 238000012827 research and development Methods 0.000 claims description 3
- 238000004088 simulation Methods 0.000 claims description 3
- 206010063385 Intellectualisation Diseases 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000013872 defecation Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Images
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- General Factory Administration (AREA)
Abstract
The embodiment of the invention discloses a design method of an intelligent management system of a satellite assembly production line, which comprises the design of a product full life cycle management system (PLM), the design of an enterprise resource planning management system (ERP), the design of a warehousing system (WMS), the design of a Manufacturing Execution System (MES) and the design of a physical layer. The design method of the intelligent management system of the satellite final assembly production line comprises the steps that a product full life cycle management system (PLM) is designed to receive orders, process and production collaborative verification, digitalized process design and technical state management are carried out, an enterprise resource planning management system (ERP) is designed to put forward purchasing demands, a purchasing plan is made, the purchasing demands are issued to suppliers, information is determined, cost analysis is carried out on materials, a storage system (WMS) is designed, the materials are coded, and finally a Manufacturing Execution System (MES) is designed and a physical layer is designed, so that the problem that the automation, digitalization and intellectualization of the satellite final assembly production line are insufficient is solved.
Description
Technical Field
The invention relates to the technical field of production line management systems, in particular to a design method of an intelligent management system of a satellite final assembly production line.
Background
Along with the development of commercial aerospace and the rapid increase of the satellite demand of China, the traditional satellite assembly integration is difficult to meet the requirement of mass production, meanwhile, low cost also becomes an important factor of market requirement, the automation, the digitization and the intellectualization of the satellite assembly integration are realized, the enterprise competitiveness is improved, the establishment of the intelligent satellite assembly production line is absolutely necessary, the intelligent satellite production line is taken as a core, a novel space industry ecological system with low cost, high efficiency and quick response is created, and the aerospace industry and the regional economic development are promoted.
The defecation inducing and weight reducing composition disclosed by the conventional automatic stamping production line of the parabolic satellite antenna with the publication number of CN205309068U and the preparation method thereof improve the processing precision and the automation degree of a satellite production line, are suitable for mass production, but do not solve the problems of insufficient automation, digitalization and intellectualization of the satellite assembly production line, and therefore, the design method of the intelligent management system of the satellite assembly production line is provided.
Disclosure of Invention
Technical problem to be solved
The embodiment of the invention provides a design method of an intelligent management system of a satellite assembly production line, which solves the problem that the automation, digitalization and intellectualization of the satellite assembly production line are insufficient.
(II) technical scheme
In order to achieve the above purpose, the embodiment of the invention is realized by the following technical scheme: a design method of an intelligent management system of a satellite final assembly production line comprises a product full life cycle management system (PLM) design, an enterprise resource planning management system (ERP) design, a warehousing system (WMS) design, a Manufacturing Execution System (MES) design and a physical layer design.
Preferably, the product full lifecycle management system (PLM) design comprises a digital process management module, a digital design, a digital process, a digital manufacturing, a digital collaboration and a technical state management, and the digital process management module comprises an overall design data access, a process design and a test design.
Preferably, the enterprise resource planning management system (ERP) design comprises production planning, procurement requirements and cost accounting, the warehousing system (WMS) design comprises warehousing management, ex-warehouse management, in-warehouse operation, inventory operation, system strategies, basic data and report statistics, the Manufacturing Execution System (MES) design comprises material requirements, planning and scheduling, operation management, quality management and equipment management, and the physical layer design comprises digital assembly, a measurement system, intelligent comprehensive testing, automatic testing and intelligent equipment design.
Preferably, the digitalized process management data access comprises an integrated overall digitalized design software data access capability, the process design comprises an integrated process digitalized design platform, the satellite overall process design is realized, a data exchange interface between the satellite overall process design and a manufacturing execution system is established, and the relevant test program development supporting the automatic test rules, the test interpretation service, the test interpretation client and the satellite system parameter processing method is included.
Preferably, the order access carries out scheduling on production line operation, enterprise operation resource management taking a scheduling plan as a core is adopted, and cost accounting comprises direct material, direct labor and manufacturing cost, sales cost, management cost, research and development cost, financial cost and other cost accounting.
Preferably, the intelligent management of the warehouse is realized based on bar code management, RFID (radio frequency identification) technology and information management technology, including warehouse entry management, warehouse exit management, warehouse operation, inventory operation, system policy, basic data and report statistics, the bar code management comprises the steps of coding materials, uploading coded information to a manufacturing execution system, realizing the intelligent management of material information, including material names, model specifications, warehouse entry and exit time, supplier information, weight, quality inspection information and the like, the management of the material in and out library comprises the management of basic information, material tracking, inventory statistical analysis, material cost analysis and the like of the material, automatic distribution of parts, parts and consumables is carried out according to the requirements of a manufacturing execution system, the material is automatically sent to the positions of an assembly area and a test area, and the parts and the products are automatically loaded and unloaded after being sent to a station.
Preferably, the planning and scheduling includes setting conditions of equipment, personnel, materials and the like of a production task, generating a production plan, monitoring monthly plan execution, daily plan completion rate, daily plan coincidence rate, a manufacturing cycle and the like in real time and displaying a terminal, and the design method of the Manufacturing Execution System (MES) includes the following steps:
s1: quality management, including technical state control, readiness check, unqualified inspection, consistency comparison and risk early warning, checking the technical state of the satellite product in real time, quickly searching the resume of parts, tracing the operation recording function, automatically collecting and summarizing data packet planning contents, completing the inspection and signing of quality assurance processes such as technical state change, unqualified product inspection, supplementary test application and the like on line, directly hooking with a specific production task, continuously tracking and realizing closed-loop management;
s2: and equipment management, including equipment state implementation monitoring, maintenance information management, timely system reminding for finding problems, automatic recording of equipment records and the like.
Preferably, the physical layer design comprises a physical layer design including digital assembly, a measurement system, intelligent comprehensive test, automatic test and intelligent equipment design; the physical layer design method comprises the following steps:
s1: the digital assembly design comprises a three-dimensional assembly process system, interactive process planning and simulation are carried out by utilizing a digital assembly technology, and a virtual assembly system based on virtual reality is constructed;
s2: the design of a measuring system comprises camera measurement, laser tracker measurement and laser radar measurement, wherein the camera measurement utilizes an image system to photograph a structural component, and information such as a component structure, an outline dimension and a relative position is obtained through image analysis;
s3: the intelligent comprehensive test design comprises housekeeping front-end software, measurement and control front-end software, acquisition processor software, automatic test software, test data distributed real-time processing software, distributed big data storage software, mass data query analysis software and distributed database backup and recovery software;
s4: the automatic test design comprises the steps of automatically running test items of each development stage, carrying out automatic test, completing unified setting and management of test equipment, carrying out offline analysis and arrangement on data, inquiring and analyzing mass data, and having functions of distributed big data backup and recovery;
s5: the intelligent equipment comprises a logistics vehicle, attitude adjusting equipment, measuring equipment, detecting equipment and testing equipment, wherein the logistics vehicle comprises a logistics transfer vehicle, the automatic distribution of materials of all stations and the automatic loading, unloading and transfer of part products are completed, the measuring equipment mainly comprises a measuring camera, a laser tracker and a laser radar, and the detecting equipment mainly comprises a helium mass spectrometer leak detector.
A design method for an intelligent management system of a satellite final assembly production line comprises the following design steps:
s1: the product full life cycle management system (PLM) design comprises a CRM system receiving orders, process and production collaborative verification, digital process design and technical state management;
s2: an enterprise resource planning management system (ERP) design comprises the steps of providing a purchasing demand, making a purchasing plan of raw materials required by production and matched ground equipment, issuing the purchasing demand to a supplier, confirming a material supply period and delivery time with the supplier, making a production plan according to the material arrival period, and analyzing material cost;
s3: the design of a storage system (WMS) comprises the steps of coding materials, uploading coded information to a manufacturing execution system, and managing in and out of a warehouse, wherein the management comprises the steps of basic information of the materials, material tracking, inventory statistical analysis and automatic distribution management;
s4: designing a Manufacturing Execution System (MES), wherein the design comprises production planning and scheduling, material demand statistics, material delivery, operation management, quality management and equipment management;
s5: and physical layer design, including digital assembly, a measurement system, intelligent comprehensive test, automatic test and intelligent equipment design, including the whole-process assembly integration and test of material delivery to a satellite factory.
(III) advantageous effects
The embodiment of the invention provides a design method of an intelligent management system of a satellite assembly production line, which is used for realizing an integrated and automatic management mode of the assembly production line, realizing intelligent manufacturing of satellites by a digital factory, improving the intelligence of the satellite production line and improving the efficiency.
Drawings
FIG. 1 is a schematic compositional diagram of an embodiment of the present invention;
FIG. 2 is an information system layer composition diagram of an embodiment of the present invention;
FIG. 3 is a control composition schematic of an embodiment of the present invention;
FIG. 4 is a diagram illustrating the physical layer composition of the design method according to an embodiment of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without making creative efforts based on the embodiments of the present invention, belong to the protection scope of the embodiments of the present invention.
As shown in fig. 1 to 4, an embodiment of the present invention provides a design method for an intelligent management system of a satellite assembly production line, where the design method includes a product full life cycle management system (PLM) design, an enterprise resource planning management system (ERP) design, a warehousing system (WMS) design, a Manufacturing Execution System (MES) design, and a physical layer design.
Example 1:
the product full life cycle management system (PLM) design comprises a digital process management module, a digital design module, a digital process module, a digital manufacturing module, a digital cooperation module and a technical state management module, wherein the digital process management module comprises overall design data access, process design and test design.
The design of an enterprise resource planning management system (ERP) comprises production planning, purchasing demand and cost accounting, the design of a storage system (WMS) comprises warehousing management, ex-warehouse management, in-warehouse operation, inventory operation, system strategy, basic data and report statistics, the design of a Manufacturing Execution System (MES) comprises material demand, planning and scheduling, operation management, quality management and equipment management, and the design of a physical layer comprises digital assembly, a measurement system, intelligent comprehensive test, automatic test and intelligent equipment design.
The digitalized process management data access comprises an integrated overall digitalized design software data access capacity, the process design comprises an integrated process digitalized design platform, the overall process design of the satellite is achieved, a data exchange interface between the overall process design of the satellite and a manufacturing execution system is established, and the relevant test program development supporting the automatic test rules, the test interpretation service, the test interpretation client and the satellite system parameter processing method is achieved.
The order access carries out scheduling on production line operation, enterprise operation resource management taking a scheduling plan as a core is adopted, and cost accounting comprises direct material, direct labor and manufacturing cost, sales cost, management cost, research and development cost, financial cost and other cost accounting.
The intelligent warehouse management is realized based on bar code management, RFID (radio frequency identification) technology and information management technology, including warehouse entry management, warehouse exit management, warehouse operation, inventory operation, system strategy, basic data and report statistics, the bar code management comprises the steps of coding materials, uploading coded information to a manufacturing execution system, realizing the intelligent management of material information, including material names, model specifications, warehouse entry and exit time, supplier information, weight, quality inspection information and the like, the warehouse entry and exit management comprises the steps of managing basic information, material tracking, inventory statistical analysis, material cost analysis and the like of the materials, automatically distributing parts, parts and consumables according to the requirements of the manufacturing execution system, automatically delivering the materials to assembly areas and test areas, and automatically loading and unloading after the parts and the products reach stations.
The planning and scheduling comprises the steps of setting conditions of equipment, personnel, materials and the like of a production task, generating a production plan, monitoring and displaying monthly plan execution, daily plan completion rate, daily plan coincidence rate, manufacturing cycle and the like in real time and in a terminal mode, wherein the design method of a Manufacturing Execution System (MES) comprises the following steps:
s1: quality management, including technical state control, readiness check, unqualified inspection, consistency comparison and risk early warning, checking the technical state of the satellite product in real time, quickly searching the resume of parts, tracing the operation recording function, automatically collecting and summarizing data packet planning contents, completing the inspection and signing of quality assurance processes such as technical state change, unqualified product inspection, supplementary test application and the like on line, directly hooking with a specific production task, continuously tracking and realizing closed-loop management;
s2: and equipment management, including equipment state implementation monitoring, maintenance information management, timely system reminding for finding problems, automatic recording of equipment records and the like.
The method comprises the following steps of designing a physical layer, wherein the physical layer comprises the physical layer, including digital assembly, a measurement system, intelligent comprehensive test, automatic test and intelligent equipment design; the physical layer design method comprises the following steps:
s1: the digital assembly design comprises a three-dimensional assembly process system, interactive process planning and simulation are carried out by utilizing a digital assembly technology, and a virtual assembly system based on virtual reality is constructed;
s2: the design of a measuring system comprises camera measurement, laser tracker measurement and laser radar measurement, wherein the camera measurement utilizes an image system to photograph a structural component, and information such as a component structure, an outline dimension and a relative position is obtained through image analysis;
s3: the intelligent comprehensive test design comprises housekeeping front-end software, measurement and control front-end software, acquisition processor software, automatic test software, test data distributed real-time processing software, distributed big data storage software, mass data query analysis software and distributed database backup and recovery software;
s4: the automatic test design comprises the steps of automatically running test items of each development stage, carrying out automatic test, completing unified setting and management of test equipment, carrying out offline analysis and arrangement on data, inquiring and analyzing mass data, and having functions of distributed big data backup and recovery;
s5: the intelligent equipment comprises a logistics vehicle, attitude adjusting equipment, measuring equipment, detecting equipment and testing equipment, wherein the logistics vehicle comprises a logistics transfer vehicle, the automatic distribution of materials of all stations and the automatic loading, unloading and transfer of part products are completed, the measuring equipment mainly comprises a measuring camera, a laser tracker and a laser radar, and the detecting equipment mainly comprises a helium mass spectrometer leak detector.
Example 2:
a design method for an intelligent management system of a satellite final assembly production line comprises the following design steps:
s1: the product full life cycle management system (PLM) design comprises a CRM system receiving orders, process and production collaborative verification, digital process design and technical state management;
s2: an enterprise resource planning management system (ERP) design comprises the steps of providing a purchasing demand, making a purchasing plan of raw materials required by production and matched ground equipment, issuing the purchasing demand to a supplier, confirming a material supply period and delivery time with the supplier, making a production plan according to the material arrival period, and analyzing material cost;
s3: the design of a storage system (WMS) comprises the steps of coding materials, uploading coded information to a manufacturing execution system, and managing in and out of a warehouse, wherein the management comprises the steps of basic information of the materials, material tracking, inventory statistical analysis and automatic distribution management;
s4: designing a Manufacturing Execution System (MES), wherein the design comprises production planning and scheduling, material demand statistics, material delivery, operation management, quality management and equipment management;
s5: and physical layer design, including digital assembly, a measurement system, intelligent comprehensive test, automatic test and intelligent equipment design, including the whole-process assembly integration and test of material delivery to a satellite factory.
Claims (9)
1. A design method of an intelligent management system of a satellite final assembly production line is characterized by comprising the following steps: the design method comprises product full life cycle management system (PLM) design, enterprise resource planning management system (ERP) design, warehousing system (WMS) design, Manufacturing Execution System (MES) design and physical layer design.
2. The design method of the intelligent management system of the satellite final assembly production line according to claim 1, characterized in that: the product full lifecycle management system (PLM) design includes a digital process management module, a digital design, a digital process, a digital manufacturing, a digital collaboration and a technical state management, the digital process management module includes a total design data access, a process design and a test design.
3. The design method of the intelligent management system of the satellite final assembly production line according to claim 1, characterized in that: the design of the enterprise resource planning management system (ERP) comprises production planning, purchasing demand and cost accounting, the design of the warehousing system (WMS) comprises warehousing management, ex-warehouse management, in-warehouse operation, inventory operation, system strategies, basic data and report statistics, the design of the Manufacturing Execution System (MES) comprises material demand, planning and scheduling, operation management, quality management and equipment management, and the design of the physical layer comprises digital assembly, a measurement system, intelligent comprehensive testing, automatic testing and intelligent equipment design.
4. The product full lifecycle management system (PLM) design of claim 1, wherein: the digitalized process management data access comprises an integrated overall digitalized design software data access capacity, the process design comprises an integrated process digitalized design platform, the satellite overall process design is achieved, a data exchange interface between the satellite overall process design and a manufacturing execution system is established, and the digitalized process management data access comprises the development of related test programs supporting automatic test rules, test interpretation services, test interpretation clients and satellite system parameter processing methods.
5. An enterprise resource planning management system (ERP) design according to claim 1, wherein: the order access carries out scheduling on production line operation, enterprise operation resource management taking a scheduling plan as a core is adopted, and cost accounting comprises direct material, direct labor and manufacturing cost, sales cost, management cost, research and development cost, financial cost and other cost accounting.
6. Warehousing system (WMS) design according to claim 1, characterized in that: the intelligent management of the warehouse is realized based on bar code management, RFID (radio frequency identification) technology and information management technology, including warehouse entry management, warehouse exit management, warehouse operation, inventory operation, system strategy, basic data and report statistics, the bar code management comprises the steps of coding materials, uploading coded information to a manufacturing execution system, realizing the intelligent management of material information, including material names, model specifications, warehouse entry and exit time, supplier information, weight, quality inspection information and the like, the management of the material in and out library comprises the management of basic information, material tracking, inventory statistical analysis, material cost analysis and the like of the material, automatic distribution of parts, parts and consumables is carried out according to the requirements of a manufacturing execution system, the material is automatically sent to the positions of an assembly area and a test area, and the parts and the products are automatically loaded and unloaded after being sent to a station.
7. A Manufacturing Execution System (MES) design according to claim 1, wherein: the planning and scheduling comprises the steps of setting conditions of equipment, personnel, materials and the like of a production task, generating a production plan, monitoring monthly plan execution, daily plan completion rate, daily plan coincidence rate, manufacturing cycle and the like in real time and displaying terminal, wherein the design method of a Manufacturing Execution System (MES) comprises the following steps:
s1: quality management, including technical state control, readiness check, unqualified inspection, consistency comparison and risk early warning, checking the technical state of the satellite product in real time, quickly searching the resume of parts, tracing the operation recording function, automatically collecting and summarizing data packet planning contents, completing the inspection and signing of quality assurance processes such as technical state change, unqualified product inspection, supplementary test application and the like on line, directly hooking with a specific production task, continuously tracking and realizing closed-loop management;
s2: and equipment management, including equipment state implementation monitoring, maintenance information management, timely system reminding for finding problems, automatic recording of equipment records and the like.
8. The physical layer design of claim 1, wherein: the physical layer design comprises a physical layer design which comprises digital assembly, a measuring system, intelligent comprehensive test, automatic test and intelligent equipment design; the physical layer design method comprises the following steps:
s1: the digital assembly design comprises a three-dimensional assembly process system, interactive process planning and simulation are carried out by utilizing a digital assembly technology, and a virtual assembly system based on virtual reality is constructed;
s2: the design of a measuring system comprises camera measurement, laser tracker measurement and laser radar measurement, wherein the camera measurement utilizes an image system to photograph a structural component, and information such as a component structure, an outline dimension and a relative position is obtained through image analysis;
s3: the intelligent comprehensive test design comprises housekeeping front-end software, measurement and control front-end software, acquisition processor software, automatic test software, test data distributed real-time processing software, distributed big data storage software, mass data query analysis software and distributed database backup and recovery software;
s4: the automatic test design comprises the steps of automatically running test items of each development stage, carrying out automatic test, completing unified setting and management of test equipment, carrying out offline analysis and arrangement on data, inquiring and analyzing mass data, and having functions of distributed big data backup and recovery;
s5: the intelligent equipment comprises a logistics vehicle, attitude adjusting equipment, measuring equipment, detecting equipment and testing equipment, wherein the logistics vehicle comprises a logistics transfer vehicle, the automatic distribution of materials of all stations and the automatic loading, unloading and transfer of part products are completed, the measuring equipment mainly comprises a measuring camera, a laser tracker and a laser radar, and the detecting equipment mainly comprises a helium mass spectrometer leak detector.
9. The design method of the intelligent management system of the satellite final assembly production line according to claim 1, characterized in that: the design steps include:
s1: the product full life cycle management system (PLM) design comprises a CRM system receiving orders, process and production collaborative verification, digital process design and technical state management;
s2: an enterprise resource planning management system (ERP) design comprises the steps of providing a purchasing demand, making a purchasing plan of raw materials required by production and matched ground equipment, issuing the purchasing demand to a supplier, confirming a material supply period and delivery time with the supplier, making a production plan according to the material arrival period, and analyzing material cost;
s3: the design of a storage system (WMS) comprises the steps of coding materials, uploading coded information to a manufacturing execution system, and managing in and out of a warehouse, wherein the management comprises the steps of basic information of the materials, material tracking, inventory statistical analysis and automatic distribution management;
s4: designing a Manufacturing Execution System (MES), wherein the design comprises production planning and scheduling, material demand statistics, material delivery, operation management, quality management and equipment management;
s5: and physical layer design, including digital assembly, a measurement system, intelligent comprehensive test, automatic test and intelligent equipment design, including the whole-process assembly integration and test of material delivery to a satellite factory.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202111569630.7A CN114297837A (en) | 2021-12-21 | 2021-12-21 | Design method of intelligent management system of satellite final assembly production line |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202111569630.7A CN114297837A (en) | 2021-12-21 | 2021-12-21 | Design method of intelligent management system of satellite final assembly production line |
Publications (1)
Publication Number | Publication Date |
---|---|
CN114297837A true CN114297837A (en) | 2022-04-08 |
Family
ID=80967158
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202111569630.7A Pending CN114297837A (en) | 2021-12-21 | 2021-12-21 | Design method of intelligent management system of satellite final assembly production line |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114297837A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115587788A (en) * | 2022-09-19 | 2023-01-10 | 成都飞机工业(集团)有限责任公司 | Aviation manufacturing execution system design method, device, equipment and storage medium |
CN115729187A (en) * | 2022-11-17 | 2023-03-03 | 北京动力机械研究所 | Processing method and device based on engine digital assembly verification |
CN115860439A (en) * | 2023-02-27 | 2023-03-28 | 机科发展科技股份有限公司 | Discrete digital workshop information system integration method |
CN116795069A (en) * | 2023-08-29 | 2023-09-22 | 成都拓林思软件有限公司 | Intelligent manufacturing method based on edge calculation |
CN117611226A (en) * | 2024-01-22 | 2024-02-27 | 吉林大学 | Intelligent on-line logistics resource accounting method based on bicycle quota and equivalent flow |
CN115729187B (en) * | 2022-11-17 | 2024-09-03 | 北京动力机械研究所 | Processing method and device based on digital assembly verification of engine |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020013719A1 (en) * | 2000-06-09 | 2002-01-31 | Mitsubishi Denki Kabushiki Kaisha | Production control system and method for producing air conditioners |
CN110428148A (en) * | 2019-07-17 | 2019-11-08 | 华域汽车车身零件(上海)有限公司 | A kind of equipment maintenance intelligent management system |
CN112163014A (en) * | 2020-09-17 | 2021-01-01 | 上海卫星装备研究所 | Internet of things management system and method for satellite final assembly equipment |
-
2021
- 2021-12-21 CN CN202111569630.7A patent/CN114297837A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020013719A1 (en) * | 2000-06-09 | 2002-01-31 | Mitsubishi Denki Kabushiki Kaisha | Production control system and method for producing air conditioners |
CN110428148A (en) * | 2019-07-17 | 2019-11-08 | 华域汽车车身零件(上海)有限公司 | A kind of equipment maintenance intelligent management system |
CN112163014A (en) * | 2020-09-17 | 2021-01-01 | 上海卫星装备研究所 | Internet of things management system and method for satellite final assembly equipment |
Non-Patent Citations (1)
Title |
---|
陈芳浩;宋飞;丁凤林;: "基于智能AGV系统的卫星推进系统批量化研制研究", 电脑与信息技术, no. 05, 15 October 2020 (2020-10-15) * |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115587788A (en) * | 2022-09-19 | 2023-01-10 | 成都飞机工业(集团)有限责任公司 | Aviation manufacturing execution system design method, device, equipment and storage medium |
CN115729187A (en) * | 2022-11-17 | 2023-03-03 | 北京动力机械研究所 | Processing method and device based on engine digital assembly verification |
CN115729187B (en) * | 2022-11-17 | 2024-09-03 | 北京动力机械研究所 | Processing method and device based on digital assembly verification of engine |
CN115860439A (en) * | 2023-02-27 | 2023-03-28 | 机科发展科技股份有限公司 | Discrete digital workshop information system integration method |
CN116795069A (en) * | 2023-08-29 | 2023-09-22 | 成都拓林思软件有限公司 | Intelligent manufacturing method based on edge calculation |
CN116795069B (en) * | 2023-08-29 | 2023-11-14 | 成都拓林思软件有限公司 | Intelligent manufacturing method based on edge calculation |
CN117611226A (en) * | 2024-01-22 | 2024-02-27 | 吉林大学 | Intelligent on-line logistics resource accounting method based on bicycle quota and equivalent flow |
CN117611226B (en) * | 2024-01-22 | 2024-04-09 | 吉林大学 | Intelligent on-line logistics resource accounting method based on bicycle quota and equivalent flow |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN114297837A (en) | Design method of intelligent management system of satellite final assembly production line | |
US7443282B2 (en) | System and a method, including software and hardware, for providing real-time and synchronization views of supply chain information | |
CN109636135B (en) | Sharing-based digital supply chain management system | |
CN105005289B (en) | A kind of industrial platform of internet of things | |
CN107831750A (en) | IMES Intelligent Manufacturing Execution Systems | |
CN111210108B (en) | Performance management and control model of electric power material supply chain | |
CN110580572B (en) | Product life-span traceability system | |
CN105005885A (en) | Industrial automatic identification and data acquisition platform | |
CN105447663A (en) | Open-type pallet sharing service method and system based on social resource integration | |
CN103679322A (en) | Production data processing method, device thereof, and system thereof | |
WO2023217057A1 (en) | Production control method and system | |
CN107563627A (en) | Workshop MES management methods and system based on bar codes technique | |
CN112766857B (en) | Intelligent warehouse management platform, system and method | |
CN110889612A (en) | Management system based on MES and management method thereof | |
CN104460569B (en) | Goods-in-process monitoring method used for blade production | |
CN112269357A (en) | Intelligent management system of mill | |
CN104392343A (en) | Open pallet pool service system based on social resource integration | |
CN110826926A (en) | Intelligent manufacturing execution system for surface assembly production line | |
CN116347348A (en) | Ship body section workshop logistics information positioning method, device, equipment and medium | |
CN115147010A (en) | Enterprise ERP data analysis and supervision system and method based on cloud computing | |
CN114819710A (en) | Management method and device of electric energy metering device, computer equipment and storage medium | |
CN113793127A (en) | Intelligent production line for electrical equipment production | |
Taraniuk et al. | Research of development of Chinese logistics enterprises based on the technology of the internet of things | |
CN113888071A (en) | Spare part management method and system based on BIM technology | |
Zhongyi et al. | Material delivery system for aircraft composite component manufacturing workshop |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |