Assembly process quality management method and system and electronic equipment

Abstract

The invention discloses an assembly process quality management method and system and electronic equipment, and the method comprises the steps: creating a first structure tree comparison graph according to first query information from a user side; according to a preset database table, performing data synchronization on the first structure tree comparison graph to obtain a second structure tree comparison graph; generating a first progress chart according to second query information from the user side; generating a second progress chart according to third query information from the user side; generating a first structure tree graph according to the second structure tree comparison graph, the first progress graph and the second progress graph; according to the historical time and the first query information, obtaining a second structure tree graph and comparing the second structure tree graph with the first structure tree graph to obtain a third structure tree comparison graph; according to the method, effective management and control of the BBOM material bill of material are realized, field operation personnel are helped to find field business data problems in time, the data quality is improved, the efficient operation of the aircraft production process is promoted, and the productivity is improved.

Description

Technical Field

[0001] The present application relates to the field of aviation equipment manufacturing, and in particular to an assembly process quality management method, system and electronic equipment. Background Art

[0002] BBOM (Built Bill of Material) is established following the manufacturing and assembly process of each aircraft. It can be said that the BBOM status of each aircraft is unique. It is the instantiation data of MBOM. Its structure inherits the structural information of MBOM (Manufacturing Bill of Material), reflecting the physical information of components under each component of the product, including serial number, processing record, deviation data, product software and hardware installation version and other information. Based on the initial BBOM, different aircraft structure production units feedback the latest physical information and assembly quality information of each component, and complete the feedback of physical information at the production delivery node to form a complete single-flight BBOM. Through BBOM, the physical assembly status management of the whole process is realized, and the control and traceability of the manufacturing physical at key nodes is realized. The rapid development of the aviation industry in today's era and the rapid development of the air transportation industry have greatly accelerated the growth of demand for new aircraft, and the task of aircraft development has become increasingly heavy.

[0003] However, in the existing technology, the display of BBOM's real-time installation status is heavily dependent on the data exported from different views. It is difficult for users to intuitively see the installation progress and problems in the quality control process through only table data. Moreover, when the view is exported, the query will lag due to unstable system performance. At the same time, when the view is updated, a large number of database tables need to be maintained, and the operation is cumbersome. Summary of the invention

[0004] The main purpose of this application is to provide an assembly process quality management method, system and electronic equipment, aiming to solve the technical problem of difficulty in quality control during assembly according to the BBOM physical bill of materials.

[0005] In a first aspect, to achieve the above-mentioned purpose, the present application provides an assembly process quality management method, comprising the following steps:

[0006] Creating a first structure tree comparison chart according to first query information from the user end, wherein the first query information at least includes a model and a flight number of the target aircraft;

[0007] According to a preset database table, data synchronization is performed on the first structure tree comparison chart to obtain a second structure tree comparison chart;

[0008] generating a first progress chart according to the second query information from the user terminal;

[0009] generating a second progress chart according to the third query information from the user terminal;

[0010] generating a first structure tree diagram according to the second structure tree comparison diagram, the first progress chart and the second progress chart;

[0011] According to the historical time and the first query information, a second structure tree diagram is obtained and the second structure tree diagram is compared with the first structure tree diagram to obtain a third structure tree comparison diagram.

[0012] Optionally, the first query information also includes a rank number of the target aircraft, and the rank number is used to query the installation status of a specific rank.

[0013] Optionally, the step of creating a first structure tree comparison chart according to the first query information from the user terminal includes:

[0014] According to the first query information, the MBOM manufacturing material list is expanded according to the AO assembly outline to obtain a first structure tree;

[0015] Expand the BBOM physical material list according to the first query information to obtain a second structure tree;

[0016] A comparison diagram of the first structure tree is obtained according to the first structure tree and the second structure tree.

[0017] Optionally, the step of creating a first structure tree comparison chart according to the first query information from the user terminal includes:

[0018] According to the first query information, the MBOM manufacturing material list is expanded according to the material to obtain a third structure tree;

[0019] Expand the BBOM physical material list according to the first query information to obtain a second structure tree;

[0020] A comparison diagram of the first structure tree is obtained according to the second structure tree and the third structure tree.

[0021] Optionally, the step of synchronizing the data of the first structure tree comparison chart according to a preset database table to obtain the second structure tree comparison chart includes:

[0022] According to the preset timing task, the latest AO assembly outline execution information of the target aircraft is obtained regularly and the AO assembly outline execution information is stored in the database table, and the update record is stored in the database table.

[0023] Optionally, the step of generating a first progress chart according to the second query information from the user terminal includes:

[0024] Obtaining a node type of a target node according to the second query information;

[0025] If the node type is a root node, generating the first progress chart showing the completion degree of a single machine;

[0026] If the node type is a section, the first progress chart showing the AO assembly outline execution information of the current section is generated.

[0027] Optionally, the step of generating a second progress chart according to the third query information from the user terminal includes:

[0028] According to the third query information, obtaining progress information of the target section;

[0029] A progress management page of the target section is generated according to the progress information, wherein the progress management page includes a plurality of the second progress charts.

[0030] Optionally, the step of generating a second progress chart according to the third query information from the user terminal further includes:

[0031] Store the related files of the second progress chart in the MinIO storage service.

[0032] In the second aspect, to achieve the above-mentioned purpose, the present application also provides an assembly process quality management system, including:

[0033] A first chart module, the first chart module is used to create a first structure tree comparison chart according to first query information from the user terminal, wherein the first query information at least includes a model and a flight number of a target aircraft;

[0034] A data synchronization module, the data synchronization module is used to synchronize the data of the first structure tree comparison chart according to a preset database table to obtain a second structure tree comparison chart;

[0035] a second chart module, the second chart module being used to generate a first progress chart according to second query information from the user end;

[0036] a third chart module, wherein the second chart module is used to generate a second progress chart according to third query information from the user terminal;

[0037] a fourth chart module, the fourth chart module being used to generate a first structure chart according to the second structure tree comparison chart, the first progress chart and the second progress chart;

[0038] A fifth chart module is used to obtain a second structure diagram according to historical time, the first query information and the first structure diagram, and compare the second structure diagram with the first structure diagram to obtain a third structure tree comparison diagram.

[0039] In a third aspect, the present application further provides an electronic device, including:

[0040] A processor and a memory, wherein the memory is used to store a computer program; and the processor is used to load and execute the computer program so that the electronic device performs the method as described in any one of the first aspects.

[0041] The beneficial effects that this application can achieve are as follows:

[0042] The assembly process quality management method proposed in the embodiment of the present application constructs a BBOM and MBOM installation comparison structure diagram according to the machine model, batch number and other information input by the user, uses the latest data in the local database table to synchronize the BBOM and MBOM installation comparison structure diagram, displays the corresponding section information and timing diagram details according to the query type clicked by the user, and finally outputs the comparison between the BOM structure of the historical version and the current latest BOM structure;

[0043] Solved the technical problem of difficulty in quality control during assembly based on BBOM physical bill of materials;

[0044] It realizes the full process control of the technical status of the BBOM physical material list software, builds a technical status control environment based on the BBOM physical material list software, and at the same time, realizes the effective control of the BBOM physical material list, enhances the intuitiveness and real-time nature of the data, and can help on-site operators to promptly discover on-site business data problems, thereby improving data quality, and ultimately promoting the efficient production process of aircraft and increasing aircraft production capacity. BRIEF DESCRIPTION OF THE DRAWINGS

[0045] Figure 1 It is a flow chart of an embodiment of the method for quality management of the assembly process in the present application;

[0046] Figure 2 A schematic diagram of a first structure tree comparison diagram in an embodiment of the assembly process quality management method in the present application;

[0047] Figure 3 It is a first schematic diagram of a second progress chart in an embodiment of the assembly process quality management method in the present application;

[0048] Figure 4 A second schematic diagram of a second progress chart in an embodiment of the assembly process quality management method in the present application;

[0049] Figure 5 It is a schematic diagram of the functional modules of an embodiment of the assembly process quality management system in this application.

[0050] The realization of the purpose, functional features and advantages of this application will be further explained in conjunction with embodiments and with reference to the accompanying drawings. DETAILED DESCRIPTION

[0051] In order to enable those skilled in the art to better understand the scheme of the present disclosure, the technical scheme in the embodiments of the present disclosure will be clearly and completely described below in conjunction with the drawings in the embodiments of the present disclosure. Obviously, the described embodiments are only part of the embodiments of the present disclosure, not all of the embodiments. Based on the embodiments in the present disclosure, all other embodiments obtained by ordinary technicians in the field without creative work should fall within the scope of protection of the present disclosure.

[0052] It should be noted that the terms "first", "second", etc. in the specification and claims of the present disclosure and the above-mentioned drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or sequence. It should be understood that the data used in this way can be interchangeable where appropriate, so that the embodiments of the present disclosure described herein can be implemented in an order other than those illustrated or described herein. In addition, the terms "including" and "having" and any variations thereof are intended to cover non-exclusive inclusions, for example, a process, method, system, product, or device that includes a series of steps or units is not necessarily limited to those steps or units that are clearly listed, but may include other steps or units that are not clearly listed or inherent to these processes, methods, products, or devices.

[0053] Example 1

[0054] Reference Figure 1 , an embodiment of the assembly process quality management method comprises the following steps:

[0055] S1. Creating a first structure tree comparison chart according to first query information from a user terminal, wherein the first query information at least includes a model and a flight number of a target aircraft;

[0056] Specifically, when the user makes a query, he or she first needs to input at least the model and flight number of the target aircraft, that is, the first query information. According to the first query information, the MBOM manufacturing bill of materials data and the BBOM physical bill of materials data corresponding to the target aircraft are obtained in the local database table. Then, the BBOM physical bill of materials is expanded to obtain the BBOM physical bill of materials structure tree. The MBOM manufacturing bill of materials data is expanded according to the material method to obtain the MBOM manufacturing bill of materials structure tree, that is, the installation structure tree. The BBOM physical bill of materials structure tree and the MBOM manufacturing bill of materials structure tree are compared to obtain the first structure tree comparison chart; refer to Figure 2 In the BBOM physical bill of materials structure tree, only the structure with installation information is displayed, and the structure without materials will not be expanded. At the same time, the nodes of the two structure trees will indicate the current installation status through different color labels. For example, green can indicate completion, blue can indicate execution, and red can indicate not started. By comparing the structure and node colors in the comparison diagram of the first structure tree, the inquirer can intuitively obtain the latest installation information.

[0057] Optionally, the first query information further includes a stage number of the target aircraft, and the stage number is used to query the installation status of a specific stage;

[0058] Specifically, when the user is querying, he also enters the segment number to be queried, and then the AO assembly outline instantiation situation under the segment can be accurately obtained. Figure 2 If there is a relevant node in the MBOM manufacturing bill of materials structure tree, but not in the BBOM physical bill of materials structure tree, it means that the AO assembly outline under the section has not been instantiated. At this time, it is necessary to contact the relevant section personnel to verify or query the downstream system to trace the whereabouts of the AO assembly outline. The different colors of the nodes indicate the different execution status of the AO assembly outline. Similarly, green can indicate completion, blue can indicate execution, and red can indicate not started.

[0059] Of course, the first query information may also include the first query time, that is, the time when this query is performed.

[0060] Optionally, the step of creating a first structure tree comparison chart according to the first query information from the user terminal includes:

[0061] According to the first query information, the MBOM manufacturing material list is expanded according to the material to obtain a first structure tree;

[0062] Expand the BBOM physical material list according to the first query information to obtain a second structure tree;

[0063] Obtaining a comparison diagram of the first structure tree according to the first structure tree and the second structure tree;

[0064] Optionally, the step of creating a first structure tree comparison chart according to the first query information from the user terminal includes:

[0065] According to the first query information, the MBOM manufacturing material list is expanded according to the AO assembly outline to obtain a third structure tree;

[0066] Expand the BBOM physical material list according to the first query information to obtain a second structure tree;

[0067] Obtaining a comparison diagram of the first structure tree according to the second structure tree and the third structure tree;

[0068] Specifically, refer to Figure 2 In this embodiment, the first structure tree comparison chart is composed of the first structure tree, the second structure tree and the third structure tree, that is, the first query information also includes the model, sortie number and segment number of the target aircraft, and the MBOM manufacturing material list is also expanded according to the AO assembly outline and material.

[0069] S2. Synchronizing the data of the first structure tree comparison chart according to a preset database table to obtain a second structure tree comparison chart;

[0070] Optionally, the step of synchronizing the data of the first structure tree comparison chart according to a preset database table to obtain the second structure tree comparison chart includes:

[0071] According to a preset timing task, the latest AO assembly outline execution information of the target aircraft is obtained at a regular time and the AO assembly outline execution information is stored in the database table, and the update record is stored in the database table;

[0072] Specifically, it can be updated regularly every day. The page can query the daily pull status and the number of updated nodes. You can also click on the updated node, and the page that jumps to it will display the details of the updated node and record the specific changes, such as MCI, MSI, CI, DSI structure and node changes. In this way, the latest data can be retained in the local database table, improving the previous shortcomings of slow and untimely export of views and reports.

[0073] Using the daily AO assembly outline execution information as the data source, construct an AO assembly outline execution information table based on the local database, analyze different AO assembly outline execution information, and retain update records. At the same time, draw a line chart of the AO assembly outline execution information based on the daily AO assembly outline execution information execution quantity. Analyze the trend of the line to estimate the completion status and delivery nodes, so as to specify the follow-up plan;

[0074] The system will update the assembly overall status page based on the latest information pulled, for example, update the activation status, that is, the number of each model currently being assembled and the name of the assembly batch, update the AO assembly outline execution information progress, that is, the execution status of the AO assembly outline execution information required for each batch (green means completed, blue means in execution, and red means not started), update the record, that is, display the latest update time of the corresponding batch, including update time, update node, update status, and update content;

[0075] At the same time, users can view the update log by clicking the details bar, which will display the specific updated node name, node status and parent-child relationship of the node.

[0076] S3. Generate a first progress chart according to the second query information from the user terminal;

[0077] Optionally, the step of generating a first progress chart according to the second query information from the user terminal includes:

[0078] Obtaining a node type of a target node according to the second query information;

[0079] If the node type is a root node, generating the first progress chart showing the completion degree of a single machine;

[0080] If the node type is a section, generating the first progress chart showing the AO assembly outline execution information of the current section;

[0081] Specifically, the second query information may be a specific node. After the user selects a specific node, the AO assembly outline execution progress of each node can be displayed through the selected node. The node types of the target node may include root nodes and sections. If the root node is selected, the AO assembly outline assembly progress (i.e., completion status) of a single machine is displayed. If it is a section, the AO assembly outline execution information of the current section is obtained. The progress of the AO assembly outline of each section can be intuitively seen through the overview diagram.

[0082] S4. Generate a second progress chart according to the third query information from the user terminal;

[0083] Optionally, the step of generating a second progress chart according to the third query information from the user terminal includes:

[0084] According to the third query information, obtaining progress information of the target section;

[0085] Generating a progress management page of the target section according to the progress information, wherein the progress management page includes a plurality of the second progress charts;

[0086] Optionally, the step of generating a second progress chart according to the third query information from the user terminal further includes:

[0087] Store the files related to the second progress chart in the MinIO storage service;

[0088] Specifically, the third query information may be a specific section, referring to Figure 3When the user clicks on a specific section, the page will jump to the progress management page of the section, that is, the second progress chart. The second progress chart is based on the time series perspective and intuitively displays the assembly status of each part of the aircraft under a single flight. In the second progress chart, refer to Figure 4 , you can view key progress information such as material information, AO assembly outline execution progress, single machine status, quality documents, etc. Among them, material information can include missing parts warning, disassembly and assembly records, installation information, serial assembly sections, exception materials, etc. AO assembly outline execution progress can include AO assembly outline execution status, reserved information, etc. Single machine status can include material comparison, ECO inclusion status, secondary planning execution status, etc. Quality documents can include deviation orders, out-of-tolerance orders, document execution orders, on-site problem handling orders, procurement change execution orders, etc.;

[0089] The related files of the second progress chart can include various files generated during the assembly process, such as the AO assembly outline document in the AO assembly outline execution progress, the ECO file in the stand-alone state, the technical problem on-site processing sheet, deviation sheet, file execution sheet in the quality document, etc. These files will be stored in MinIO's storage service, using MinIO's encryption and anti-tampering features to provide confidentiality, integrity and authenticity guarantees for the encrypted data of the documents, and support users to preview or download in real time on the front-end page.

[0090] Through steps S3 to S4, the entire life cycle of parts from production to assembly can be traced, from parts to components to sections and finally to complete machines. The installation progress of each part can be calculated and analyzed, and it can be estimated whether the entire assembly time will exceed the node requirements, thereby efficiently constructing the assembly process of the entire aircraft.

[0091] S5, generating a first structure tree diagram according to the second structure tree comparison diagram, the first progress chart and the second progress chart;

[0092] Specifically, since data synchronization is performed in step S2, the first structure tree can reflect the latest BOM material list structure.

[0093] S6. Acquire a second structure tree diagram according to the historical time and the first query information, and compare the second structure tree diagram with the first structure tree diagram to obtain a third structure tree comparison diagram;

[0094] Specifically, according to the historical time and the first query information, the second structure tree obtained can reflect the BOM material list structure of the historical version, and the historical time can be any query time earlier than the first query time corresponding to the first query information;

[0095] Starting from the overall BBOM physical bill of materials structure, the first structure tree diagram and the second structure tree diagram are compared to obtain the third structure tree comparison diagram. The differentiated parts on both sides of the third structure tree comparison diagram will be highlighted in different colors (red can indicate deletion, green can indicate addition, and blue can indicate modification). Each difference part, that is, the changed node, has traceable information such as modification time and modifier, so that it is easy to grasp the overall assembly progress during this period, which is convenient for data analysis and statistics of aircraft assembly, designation of assembly delivery nodes, and issuance of production and manufacturing plan tasks.

[0096] In summary, through this embodiment, the problem of aircraft installation process information data can be discovered and handled. The physical state of assembly is controlled by the independent BBOM physical bill of materials software management, so as to realize the whole process control of the technical state of airborne software, build a software-based technical state control environment, realize the effective control of the technical state of airborne software, enhance the intuitiveness and real-time performance, and help on-site operators to timely discover the business data problems on site, so as to improve the data quality, and finally promote the efficient production process of aircraft and improve the production capacity of aircraft.

[0097] At the same time, it also realizes the physical assembly status management of the whole process, and realizes the control and traceability of the manufacturing physical objects at key nodes. Compared with various previous report export views, this embodiment effectively reduces time and labor costs through progress, data visualization, local data storage, and regular pulling of the latest data. It solves the problem that when the MBOM manufacturing bill of materials structure changes due to emergencies such as design changes and temporary AO assembly outline changes, the BBOM physical bill of materials can only query the data of the current structure, and cannot intuitively discover changes in assembly status, cannot reproduce historical assembly requirements, and some historical nodes may be lost. The structured and easy-to-analyze data provided in this embodiment also makes it easy for users to quickly discover problems in the assembly process and better deliver finished products.

[0098] Example 2

[0099] Reference Figure 5 , an embodiment of an assembly process quality management system, comprising:

[0100] A first chart module, the first chart module is used to create a first structure tree comparison chart according to first query information from the user terminal, wherein the first query information at least includes a model and a flight number of a target aircraft;

[0101] A data synchronization module, the data synchronization module is used to synchronize the data of the first structure tree comparison chart according to a preset database table to obtain a second structure tree comparison chart;

[0102] a second chart module, the second chart module being used to generate a first progress chart according to second query information from the user end;

[0103] a third chart module, wherein the second chart module is used to generate a second progress chart according to third query information from the user terminal;

[0104] a fourth chart module, the fourth chart module being used to generate a first structure chart according to the second structure tree comparison chart, the first progress chart and the second progress chart;

[0105] A fifth chart module is used to obtain a second structure diagram according to historical time, the first query information and the first structure diagram, and compare the second structure diagram with the first structure diagram to obtain a third structure tree comparison diagram.

[0106] Example 3

[0107] An embodiment of an electronic device includes: a processor and a memory, wherein the memory is used to store a computer program; the processor is used to load and execute the computer program so that the electronic device performs any of the methods described above.

[0108] In the above embodiments of the present disclosure, the description of each embodiment has its own emphasis. For parts that are not described in detail in a certain embodiment, reference can be made to the relevant descriptions of other embodiments.

[0109] In the several embodiments provided in this application, it should be understood that the disclosed technical content can be implemented in other ways. Among them, the device embodiments described above are only schematic. For example, the division of units can be a logical function division. There may be other division methods in actual implementation. For example, multiple units or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or direct coupling or communication connection shown or discussed can be through some interfaces, indirect coupling or communication connection of units or modules, which can be electrical or other forms.

[0110] The units described as separate components may or may not be physically separated, and the components shown as units may or may not be physical units, that is, they may be located in one place or distributed over multiple units. Some or all of the units may be selected according to actual needs to achieve the purpose of the present embodiment.

[0111] In addition, each functional unit in each embodiment of the present disclosure may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit. The above-mentioned integrated unit may be implemented in the form of hardware or in the form of software functional units.

[0112] If the integrated unit is implemented in the form of a software functional unit and sold or used as an independent product, it can be stored in a computer-readable non-volatile storage medium. Based on this understanding, the technical solution of the present disclosure is essentially or the part that contributes to the prior art or all or part of the technical solution can be embodied in the form of a software product, and the computer software product is stored in a non-volatile storage medium, including a number of instructions to enable a computer device (which can be a personal computer, server or network device, etc.) to perform all or part of the steps of the various embodiments of the present disclosure. The aforementioned non-volatile storage medium includes: U disk, read-only memory (ROM, Read-Only Memory), random access memory (RAM, Random Access Memory), mobile hard disk, disk or optical disk and other media that can store program codes.

[0113] The above are only preferred embodiments of the present disclosure. It should be pointed out that, for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the principles of the present disclosure. These improvements and modifications should also be regarded as the protection scope of the present disclosure.

Claims

1. A method for quality management of an assembly process, characterized in that: The following steps are involved: Creating a first structure tree comparison chart according to first query information from the user end, wherein the first query information at least includes a model and a flight number of the target aircraft; According to a preset database table, data synchronization is performed on the first structure tree comparison chart to obtain a second structure tree comparison chart; generating a first progress chart according to the second query information from the user terminal; generating a second progress chart according to the third query information from the user terminal; generating a first structure tree diagram according to the second structure tree comparison diagram, the first progress chart and the second progress chart; According to the historical time and the first query information, a second structure tree diagram is acquired and the second structure tree diagram is compared with the first structure tree diagram to obtain a third structure tree comparison diagram.

2. An assembly process quality management method as claimed in claim 1, characterized in that: The first query information also includes the segment number of the target aircraft, and the segment number is used to query the installation status of a specific segment.

3. An assembly process quality management method as claimed in claim 2, characterized in that: The step of creating a first structure tree comparison diagram according to the first query information from the user terminal includes: According to the first query information, the MBOM manufacturing material list is expanded according to the AO assembly outline to obtain a first structure tree; Expand the BBOM physical material list according to the first query information to obtain a second structure tree; A comparison diagram of the first structure tree is obtained according to the first structure tree and the second structure tree.

4. The assembly process quality management method according to claim 1, characterized in that: The step of creating a first structure tree comparison diagram according to the first query information from the user terminal includes: According to the first query information, the MBOM manufacturing material list is expanded according to the material to obtain a third structure tree; Expand the BBOM physical material list according to the first query information to obtain a second structure tree; A comparison diagram of the first structure tree is obtained according to the second structure tree and the third structure tree.

5. The assembly process quality management method according to claim 2, characterized in that: The step of synchronizing the data of the first structure tree comparison chart according to the preset database table to obtain the second structure tree comparison chart comprises: According to the preset timing task, the latest AO assembly outline execution information of the target aircraft is obtained regularly and the AO assembly outline execution information is stored in the database table, and the update record is stored in the database table.

6. The assembly process quality management method according to claim 1, characterized in that: The step of generating a first progress chart according to the second query information from the user terminal includes: Obtaining a node type of a target node according to the second query information; If the node type is a root node, generating the first progress chart showing the completion degree of a single machine; If the node type is a section, the first progress chart showing the AO assembly outline execution information of the current section is generated.

7. An assembly process quality management method as claimed in claim 1, characterized in that: The step of generating a second progress chart according to the third query information from the user terminal includes: According to the third query information, obtaining progress information of the target section; A progress management page of the target section is generated according to the progress information, wherein the progress management page includes a plurality of the second progress charts.

8. An assembly process quality management method as claimed in claim 1, characterized in that: The step of generating a second progress chart according to the third query information from the user terminal further includes: Store the related files of the second progress chart in the MinIO storage service.

9. An assembly process quality management system, characterized in that: include: A first chart module, the first chart module is used to create a first structure tree comparison chart according to first query information from the user terminal, wherein the first query information at least includes a model and a flight number of a target aircraft; A data synchronization module, the data synchronization module is used to synchronize the data of the first structure tree comparison chart according to a preset database table to obtain a second structure tree comparison chart; a second chart module, the second chart module being used to generate a first progress chart according to second query information from the user end; a third chart module, wherein the second chart module is used to generate a second progress chart according to third query information from the user terminal; a fourth chart module, the fourth chart module being used to generate a first structure chart according to the second structure tree comparison chart, the first progress chart and the second progress chart; A fifth chart module is used to obtain a second structure diagram according to historical time, the first query information and the first structure diagram, and compare the second structure diagram with the first structure diagram to obtain a third structure tree comparison diagram.

10. An electronic device, characterized in that: include: A processor and a memory, wherein the memory is used to store a computer program; and the processor is used to load and execute the computer program so that the electronic device executes the method as described in any one of claims 1 to 8.

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