CN116450578A - Aircraft engine material data maintenance management method - Google Patents
Aircraft engine material data maintenance management method Download PDFInfo
- Publication number
- CN116450578A CN116450578A CN202310707026.9A CN202310707026A CN116450578A CN 116450578 A CN116450578 A CN 116450578A CN 202310707026 A CN202310707026 A CN 202310707026A CN 116450578 A CN116450578 A CN 116450578A
- Authority
- CN
- China
- Prior art keywords
- data
- information
- file
- data source
- attribute
- 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.)
- Granted
Links
- 239000000463 material Substances 0.000 title claims abstract description 151
- 238000012423 maintenance Methods 0.000 title claims abstract description 22
- 238000007726 management method Methods 0.000 title claims abstract description 20
- 238000000034 method Methods 0.000 claims description 27
- 230000008569 process Effects 0.000 claims description 13
- 239000000126 substance Substances 0.000 claims description 11
- 238000011990 functional testing Methods 0.000 claims description 5
- 230000008520 organization Effects 0.000 claims description 5
- 230000006835 compression Effects 0.000 claims description 4
- 238000007906 compression Methods 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 2
- 239000000945 filler Substances 0.000 claims description 2
- 238000012856 packing Methods 0.000 claims description 2
- 238000013523 data management Methods 0.000 abstract description 4
- 238000004806 packaging method and process Methods 0.000 abstract description 2
- 238000012360 testing method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000011207 functional examination Methods 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 238000013479 data entry Methods 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F16/00—Information retrieval; Database structures therefor; File system structures therefor
- G06F16/10—File systems; File servers
- G06F16/11—File system administration, e.g. details of archiving or snapshots
- G06F16/122—File system administration, e.g. details of archiving or snapshots using management policies
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F16/00—Information retrieval; Database structures therefor; File system structures therefor
- G06F16/10—File systems; File servers
- G06F16/13—File access structures, e.g. distributed indices
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F16/00—Information retrieval; Database structures therefor; File system structures therefor
- G06F16/10—File systems; File servers
- G06F16/16—File or folder operations, e.g. details of user interfaces specifically adapted to file systems
- G06F16/164—File meta data generation
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F40/00—Handling natural language data
- G06F40/10—Text processing
- G06F40/166—Editing, e.g. inserting or deleting
- G06F40/174—Form filling; Merging
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F40/00—Handling natural language data
- G06F40/10—Text processing
- G06F40/166—Editing, e.g. inserting or deleting
- G06F40/177—Editing, e.g. inserting or deleting of tables; using ruled lines
- G06F40/18—Editing, e.g. inserting or deleting of tables; using ruled lines of spreadsheets
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F40/00—Handling natural language data
- G06F40/20—Natural language analysis
- G06F40/205—Parsing
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F40/00—Handling natural language data
- G06F40/20—Natural language analysis
- G06F40/279—Recognition of textual entities
- G06F40/289—Phrasal analysis, e.g. finite state techniques or chunking
- G06F40/295—Named entity recognition
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/20—Administration of product repair or maintenance
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q50/00—Systems or methods specially adapted for specific business sectors, e.g. utilities or tourism
- G06Q50/04—Manufacturing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/30—Computing systems specially adapted for manufacturing
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Business, Economics & Management (AREA)
- General Health & Medical Sciences (AREA)
- Computational Linguistics (AREA)
- Audiology, Speech & Language Pathology (AREA)
- Artificial Intelligence (AREA)
- Databases & Information Systems (AREA)
- Human Resources & Organizations (AREA)
- Data Mining & Analysis (AREA)
- Marketing (AREA)
- Strategic Management (AREA)
- Tourism & Hospitality (AREA)
- General Business, Economics & Management (AREA)
- Economics (AREA)
- Manufacturing & Machinery (AREA)
- Quality & Reliability (AREA)
- Operations Research (AREA)
- Primary Health Care (AREA)
- Entrepreneurship & Innovation (AREA)
- Human Computer Interaction (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- Information Retrieval, Db Structures And Fs Structures Therefor (AREA)
Abstract
The application provides an aeroengine material data maintenance management method, which belongs to the technical field of data management and comprises the following steps: establishing a table group, and naming different tables in the table group by categories of material data respectively; filling data attributes in one column of each table, wherein each attribute has a corresponding value, a data source of the value comprises characters, forms and pictures, the forms and the pictures are respectively stored in the form of data source files, and value information of each attribute is sequentially filled in the other column of the table, and is file information of the characters and/or the data source files; packaging the data file and the table group of the values in a compressed package; completing a material information file of a plurality of materials; analyzing and identifying the total file, extracting information in the data source file to obtain detailed data information of each material, and importing the detailed data information of the material into a material database. By the processing scheme, the material data quality is improved.
Description
Technical Field
The application relates to the field of data management, in particular to an aeroengine material data maintenance management method.
Background
In the field of aeroengines, due to the special nature of engine products, special requirements on accuracy, high quality, reliability and high temperature resistance of materials are met, so that in the construction of a material database, special attention is paid to material data sources, accuracy of data acquisition and maintenance, data consistency and inspectability.
At present, the main technical means of data acquisition of materials in the market is to construct a data input and maintenance interface based on information technology (Information Technology, abbreviated as IT), and input or change the number value one by one according to the number of the material, and the technical scheme accounts for more than 95% of the database management systems of similar materials in the market, and is also the most common solution of data acquisition and maintenance of the information management system. However, most of the number values of the aerial hair materials contain a table, the table is extremely complex, a plurality of cells crossing rows and columns, a plurality of material performance parameters and a plurality of test conditions are contained in the table, and data operation rules and descriptions of a plurality of forms are also contained, so that the data acquisition and maintenance requirements of the material table data cannot be met by the simple data entry one by one.
Disclosure of Invention
In view of the above, the application provides an aeroengine material data maintenance management method, which solves the problems in the prior art and improves the consistency and accuracy of material data.
The method for maintaining and managing the material data of the aero-engine adopts the following technical scheme:
an aircraft engine material data maintenance management method, comprising:
step 1, a table group is established, wherein the table group comprises a plurality of tables, and the tables are named according to the types of material data respectively;
step 2, sequentially filling the attribute of the data corresponding to the material data category in a column of each table named by the material data category, wherein each attribute has a corresponding value, the data source of the value comprises characters, forms and pictures, the forms and the pictures are respectively stored in the form of data source files, the value information of each attribute is sequentially filled in a column adjacent to the attribute column in the table, and the value information is the file information of the characters and/or the data source files;
step 3, packing the data file and the table group of the values in a compression package, and naming the compression package according to the material marks to form a material information file;
step 4, completing material information files of various materials according to the steps 1 to 3;
and 5, integrating the plurality of material information files into a total file, analyzing and identifying the total file, extracting information in the data source file, enabling value information displayed by the file information of the data source file in a table of each material to correspond to detailed data in the data source file one by one, obtaining detailed data information of each material, and importing the detailed data information of the material into a material database.
Optionally, the class names of the material data include basic information, summaries, physical and chemical properties, mechanical properties, organizational structures, process performance and requirements, functional test trials, usage advice, and references.
Optionally, the file information of the data source file is: the file name of the data source file or the file name of the data source file.
Optionally, the attribute column in the table named with the basic information fills in the parameter names of the materials, which include the material brand, material identification, material alias name, and material classification.
Optionally, the individual number sequence numbers and the names of the individual numbers of the filler materials are listed with attributes in the tables named overview, physical and chemical properties, mechanical properties, organizational structure, process performance and requirements, functional test trials, usage advice and references.
Optionally, the attribute columns in the tables named with the overview, physical and chemical properties, mechanical properties, organization structure, process performance and requirements, functional examination test, use advice and references are also filled with a ranking type, the ranking type is the type of value information of the attribute, and the type of value information of the attribute comprises a compound, a character, a picture and a form.
Optionally, the file name of the data source file is the rank number of the material.
In summary, the present application includes the following beneficial technical effects:
when the aeroengine material data maintenance management method is used, when the data source type of the attribute value is a character, the character is directly filled in a table, when the data source type of the attribute value is a form or a picture, the file name of a data source file is filled in the table, the corresponding data source files are simultaneously stored, a data manager does not need to input the data information of a complex form of the data source into a system one by one, but analyzes and identifies an excel table of a material by a computer, the file information of the data source file in the data information in the table corresponds to the detailed data in the data source file one by one to obtain the detailed data information of each material, the detailed data information of the material is imported into a material database, the efficiency of data input is improved, and errors in data input are reduced; when a category of material data is selected and then an attribute is selected, the value of the attribute is displayed in a form of a character or a data source file or a picture in the data source. In the material data management process, a material data manager does not need to input complex data, so that the professional complexity of the material is reduced, and the quality and standardization of the material data are improved.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a flow diagram of a method for aircraft engine material data maintenance management;
FIG. 2 is a schematic diagram of the table contents named basic information of the present application;
fig. 3 is a schematic diagram of the table contents named mechanical properties in the present application.
Detailed Description
Embodiments of the present application are described in detail below with reference to the accompanying drawings.
Other advantages and effects of the present application will become apparent to those skilled in the art from the present disclosure, when the following description of the embodiments is taken in conjunction with the accompanying drawings. It will be apparent that the described embodiments are only some, but not all, of the embodiments of the present application. The present application may be embodied or carried out in other specific embodiments, and the details of the present application may be modified or changed from various points of view and applications without departing from the spirit of the present application. It should be noted that the following embodiments and features in the embodiments may be combined with each other without conflict. All other embodiments, which can be made by one of ordinary skill in the art based on the embodiments herein without making any inventive effort, are intended to be within the scope of the present application.
It is noted that various aspects of the embodiments are described below within the scope of the following claims. It should be apparent that the aspects described herein may be embodied in a wide variety of forms and that any specific structure and/or function described herein is merely illustrative. Based on the present application, one skilled in the art will appreciate that one aspect described herein may be implemented independently of any other aspect, and that two or more of these aspects may be combined in various ways. For example, an apparatus may be implemented and/or a method practiced using any number of the aspects set forth herein. In addition, such apparatus may be implemented and/or such methods practiced using other structure and/or functionality in addition to one or more of the aspects set forth herein.
It should also be noted that the illustrations provided in the following embodiments merely illustrate the basic concepts of the application by way of illustration, and only the components related to the application are shown in the drawings and are not drawn according to the number, shape and size of the components in actual implementation, and the form, number and proportion of the components in actual implementation may be arbitrarily changed, and the layout of the components may be more complicated.
In addition, in the following description, specific details are provided in order to provide a thorough understanding of the examples. However, it will be understood by those skilled in the art that the aspects may be practiced without these specific details.
The embodiment of the application provides an aeroengine material data maintenance management method.
As shown in fig. 1, an aeroengine material data maintenance management method includes:
step 1, a table group is established, wherein the table group comprises a plurality of tables, and the tables are named according to the types of the material data. In one embodiment, a plurality of sheets are created in an excel table to form a table group, and the plurality of sheets are named by category of material data, respectively.
And 2, sequentially filling the attribute of the data corresponding to the material data category in a column of each table named by the material data category, wherein each attribute has a corresponding value, the data source of the value comprises characters, forms and pictures, the forms and the pictures are respectively stored in the form of data source files, the value information of each attribute is sequentially filled in a column adjacent to the attribute column in the table, and the value information is file information of the characters and/or the data source files.
And 3, packaging the data file and the table group of the values in a compressed package, and naming the compressed package according to the material marks to form a material information file.
And 4, finishing the material information files of the various materials according to the steps 1 to 3.
And 5, integrating the plurality of material information files into a total file, analyzing and identifying the total file, extracting information in the data source file, enabling value information displayed by the file information of the data source file in a table of each material to correspond to detailed data in the data source file one by one, obtaining detailed data information of each material, and importing the detailed data information of the material into a material database.
When the aeroengine material data maintenance management method is used, when the data source type of the attribute value is a character, the character is directly filled in a table, when the data source type of the attribute value is a form or a picture or a large number of characters, the file name of a data source file is filled in the table, the corresponding data source files are simultaneously stored, a data manager does not need to input the data information of the complex form or picture of the data source into a system one by one, but analyzes and identifies an excel table of a material by a computer, the file information of the data source file in the value information corresponds to detailed data in the data source file one by one to obtain detailed data information of each material, the detailed data information of the material is imported into a material database, the efficiency of inputting the data is improved, and errors in inputting the data are reduced; when a category of material data is selected and then an attribute is selected, the value of the attribute is displayed in a form of a character or a data source file or a picture in the data source. In the material data management process, a material data manager does not need to input complex data, so that the professional complexity of the material is reduced, and the quality and standardization of the material data are improved.
In step 2, the file information of the data source file is: the file name of the data source file or the file name of the data source file. The file name of the data source file may also be added { }, and the suffix or the file name of the data source file is filled into { }, for example: { filename of data source file. Suffix }; the computer takes { } as a flag identifying the file name of the data source file.
In one embodiment, the file name of the data source file is the rank number of the material. The number sequence number and the number name should be consistent with the original information of the material, and a mode of adding dots by numbers is adopted, such as 3.1.1.2; freely expanding ranking also obeys the above-mentioned rules. The ranking number is consistent with the material manual and cannot be repeated, the software determines whether to newly add ranking or modify ranking according to the ranking number, the ranking number is in a tree structure, and the lower ranking number is generated according to a ranking number generation rule on the basis of the upper ranking number; the last digit of the rank number layer is generated in the form of increasing by 1; the number sequence number cannot contain any other character, such as a space, except a numerical value and a dot.
When the data source is a form, the form may be saved as an excel format file, and file information of the data source file may be the following example: 3.1.1.1.Xlsx,3.1.1.2.Xlsx; the method can also be as follows: {3.1.1.1.Xlsx }, {3.1.1.2.Xlsx }; the method can also be as follows: 3.1.1.1,3.1.1.2; the method can also be as follows: {3.1.1.1 },{3.1.1.2 }.
When the data source is a picture, the file stored as a jpg format file, and the file information of the data source file may be the following examples: 3.1.1.Jpg,3.1.2.Jpg; the method can also be as follows: {3.1.1.Jpg }, {3.1.2.Jpg }; the method can also be as follows: 3.1.1,3.1.2; the method can also be as follows: {3.1.1.},{3.1.2 }.
As shown in fig. 2 and 3, the category names of the material data include basic information, overview, physical and chemical properties, mechanical properties, organization structure, process performance and requirements, functional examination experiments, use suggestions, references, and others, and it should be noted that: other matters herein are not omitted, and are not meant otherwise as such, but as a category name, see specifically the last category name of fig. 2.
As shown in fig. 2, the attribute column in the table named with the basic information fills the parameter names of the materials including the material brand, material identification, material alias name, material major classification, material minor classification, material name, technical standard, chemical composition/basic composition, supply manufacturing status, supply heat treatment status, variety standard, smelting and casting process, characteristics and applications, import/home-made, new material, density unit, density tolerance, density, application unit, price, remark, and the like. The name of the material license plate must be consistent with a standard manual and cannot be repeated, and the software can determine whether to newly add the material license plate or modify the existing material license plate information according to the name; the material identifier is consistent with the name of the material brand under the default condition, and can adopt the unified purchasing material codes of an aviation group or the unified specified material codes in a unit; the basic information in principle all cells have to be filled, otherwise default values will be taken, which may be empty strings.
As shown in fig. 3, the respective number sequence numbers and the names of the respective numbers of the filling materials are listed by attributes in the tables of overview, physical and chemical properties, mechanical properties, organization, process properties and requirements, functional examination experiments, use advice, references, and other designations.
The attribute columns in the tables named with overview, physical and chemical properties, mechanical properties, organization structures, process properties and requirements, functional exam tests, use suggestions, references and other names are also filled with number types, which are types of value information of the attributes, including composites, characters, pictures and forms. When the type of the value information of the attribute is compound, the value information of the attribute is the file name of the character and the data source file, and the data source file can be a form and a picture. When the type of the value information of the attribute is a character, the value information of the attribute is a character. When the type of the value information of the attribute is a picture, the value information of the attribute is the file name of the data source file, and the data source file is the picture. When the type of the value information of the attribute is a form, the value information of the attribute is the file name of the data source file, and the data source file is the form.
The computer automatically updates and maintains the material information in batches, provides a simple file uploading interface, packages the catalogue of the material data into a compressed package according to the steps 1-4, uploads the compressed package to a computer server for decompression, automatically processes the material data templates in batches, and maintains the material basic information, the attribute and the value information of the attribute into a material database.
The problems of complex operation and low efficiency of maintenance work of the material data of the aeroengine are solved by adopting a template idea, and an aeroengine material data specification is formulated for specifying key information such as necessary filling items, data association relations, data uniqueness, data updating conditions and the like of the material data, so that the consistency and accuracy of the material data are ensured, the quality of the material data is improved, and the material data meets the requirements of general guidelines of the database of aviation and is based on the characteristics of the aeroengine material; the method has the advantages that the material data acquisition is realized by adopting the excel-type table, the material information is automatically and batched maintained based on the data specification, the excel-type table is formulated in combination with the use requirement of the aeroengine material, the data acquisition quality and the data standardization of the material data can be greatly improved through training in advance, the complexity of the aeroengine material can be simplified, the problem that the material data of a digital aeroengine material database system is difficult to maintain and the efficiency is low can be solved, the material brand information can be directly managed and maintained through the excel-type table template under the condition of no digital system, the method specifically comprises the contents of multiple aspects such as physical and chemical technology test, the excel-type table template is simple to use and convenient to check, and the management cost can be remarkably reduced for small-batch material use units.
According to the method, the excel type form templates are adopted to collect the material data, so that the collection work is not limited by the region of the software system, the data collection can be carried out anytime and anywhere, and then the data can be uniformly maintained in the material information base, the collection difficulty is reduced, and the construction process of the material database is quickened.
The foregoing is merely specific embodiments of the present application, but the scope of the present application is not limited thereto, and any changes or substitutions easily conceivable by those skilled in the art within the technical scope of the present application should be covered in the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.
Claims (7)
1. The aircraft engine material data maintenance and management method is characterized by comprising the following steps of:
step 1, a table group is established, wherein the table group comprises a plurality of tables, and the tables are named according to the types of material data respectively;
step 2, sequentially filling the attribute of the data corresponding to the material data category in a column of each table named by the material data category, wherein each attribute has a corresponding value, the data source of the value comprises characters, forms and pictures, the forms and the pictures are respectively stored in the form of data source files, the value information of each attribute is sequentially filled in a column adjacent to the attribute column in the table, and the value information is the file information of the characters and/or the data source files;
step 3, packing the data file and the table group of the values in a compression package, and naming the compression package according to the material marks to form a material information file;
step 4, completing material information files of various materials according to the steps 1 to 3;
and 5, integrating the plurality of material information files into a total file, analyzing and identifying the total file, extracting information in the data source file, enabling value information displayed by the file information of the data source file in a table of each material to correspond to detailed data in the data source file one by one, obtaining detailed data information of each material, and importing the detailed data information of the material into a material database.
2. The aircraft engine material data maintenance management method of claim 1, wherein class names of material data include basic information, summaries, physical and chemical properties, mechanical properties, organizational structures, process performance and requirements, functional test trials, usage advice, and references.
3. The aircraft engine material data maintenance management method according to claim 1, wherein in step 2, a file name of the data source file or file information of the data source file is: and (3) file name and suffix of the data source file.
4. The aircraft engine material data maintenance management method according to claim 2, wherein the attribute column in the table named with the basic information fills in the parameter names of the materials, the parameter names of the materials including material branding, material identification, material alias names, and material classification.
5. The aircraft engine material data maintenance management method of claim 2, wherein the respective ranking numbers and the names of the respective ranking numbers of the filler materials are listed by attributes in tables named overview, physical and chemical properties, mechanical properties, organizational structure, process performance and requirements, functional test, usage advice and references.
6. The method of claim 5, wherein the attribute columns in the tables named with overview, physical and chemical properties, mechanical properties, organization, process performance and requirements, functional test, usage advice and references are also populated with a ranking type, the ranking type being a type of value information of the attribute, the type of value information of the attribute including composites, characters, pictures and forms.
7. The aircraft engine material data maintenance management method of claim 1, wherein the file name of the data source file is a ranking number of the material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310707026.9A CN116450578B (en) | 2023-06-15 | 2023-06-15 | Aircraft engine material data maintenance management method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310707026.9A CN116450578B (en) | 2023-06-15 | 2023-06-15 | Aircraft engine material data maintenance management method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN116450578A true CN116450578A (en) | 2023-07-18 |
| CN116450578B CN116450578B (en) | 2023-09-15 |
Family
ID=87127702
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310707026.9A Active CN116450578B (en) | 2023-06-15 | 2023-06-15 | Aircraft engine material data maintenance management method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116450578B (en) |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060229896A1 (en) * | 2005-04-11 | 2006-10-12 | Howard Rosen | Match-based employment system and method |
| CN106294825A (en) * | 2016-08-17 | 2017-01-04 | 浪潮软件股份有限公司 | A kind of excel data managing method and system, client, service end |
| CN106528684A (en) * | 2016-10-25 | 2017-03-22 | 北京瑞风协同科技股份有限公司 | Method and system for establishing engineering material database |
| CN107291674A (en) * | 2017-06-12 | 2017-10-24 | 广东川田卫生用品有限公司 | A kind of method that Excel list datas are converted to database format |
| CN109255114A (en) * | 2018-09-17 | 2019-01-22 | 四川长虹电器股份有限公司 | The system and method for Excel table and legend is generated based on data configuration |
| US20190286636A1 (en) * | 2018-03-13 | 2019-09-19 | deFacto Global, Inc. | Systems, methods, and devices for generation of analytical data reports using dynamically generated queries of a structured tabular cube |
| CN111061696A (en) * | 2019-12-17 | 2020-04-24 | 中国银行股份有限公司 | Method and device for analyzing transaction message log |
| CN111259006A (en) * | 2019-11-19 | 2020-06-09 | 中国科学院计算机网络信息中心 | Universal distributed heterogeneous data integrated physical aggregation, organization, release and service method and system |
| CN115175019A (en) * | 2022-07-01 | 2022-10-11 | 深圳市千宝通通科技有限公司 | Intelligent meter reading data management system and method |
| CN115269515A (en) * | 2022-09-22 | 2022-11-01 | 泰盈科技集团股份有限公司 | Processing method for searching specified target document data |
| CN115495658A (en) * | 2022-09-29 | 2022-12-20 | 建信金融科技有限责任公司 | Data processing method and device |
| CN115795066A (en) * | 2022-12-28 | 2023-03-14 | 深圳软牛科技有限公司 | Method and related device for interconversion of iBootim image and PNG image |
| CN116226172A (en) * | 2023-05-08 | 2023-06-06 | 深圳市新国都数字科技有限公司 | Statistical analysis file analysis method, device and storage medium |
-
2023
- 2023-06-15 CN CN202310707026.9A patent/CN116450578B/en active Active
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060229896A1 (en) * | 2005-04-11 | 2006-10-12 | Howard Rosen | Match-based employment system and method |
| CN106294825A (en) * | 2016-08-17 | 2017-01-04 | 浪潮软件股份有限公司 | A kind of excel data managing method and system, client, service end |
| CN106528684A (en) * | 2016-10-25 | 2017-03-22 | 北京瑞风协同科技股份有限公司 | Method and system for establishing engineering material database |
| CN107291674A (en) * | 2017-06-12 | 2017-10-24 | 广东川田卫生用品有限公司 | A kind of method that Excel list datas are converted to database format |
| US20190286636A1 (en) * | 2018-03-13 | 2019-09-19 | deFacto Global, Inc. | Systems, methods, and devices for generation of analytical data reports using dynamically generated queries of a structured tabular cube |
| CN109255114A (en) * | 2018-09-17 | 2019-01-22 | 四川长虹电器股份有限公司 | The system and method for Excel table and legend is generated based on data configuration |
| CN111259006A (en) * | 2019-11-19 | 2020-06-09 | 中国科学院计算机网络信息中心 | Universal distributed heterogeneous data integrated physical aggregation, organization, release and service method and system |
| CN111061696A (en) * | 2019-12-17 | 2020-04-24 | 中国银行股份有限公司 | Method and device for analyzing transaction message log |
| CN115175019A (en) * | 2022-07-01 | 2022-10-11 | 深圳市千宝通通科技有限公司 | Intelligent meter reading data management system and method |
| CN115269515A (en) * | 2022-09-22 | 2022-11-01 | 泰盈科技集团股份有限公司 | Processing method for searching specified target document data |
| CN115495658A (en) * | 2022-09-29 | 2022-12-20 | 建信金融科技有限责任公司 | Data processing method and device |
| CN115795066A (en) * | 2022-12-28 | 2023-03-14 | 深圳软牛科技有限公司 | Method and related device for interconversion of iBootim image and PNG image |
| CN116226172A (en) * | 2023-05-08 | 2023-06-06 | 深圳市新国都数字科技有限公司 | Statistical analysis file analysis method, device and storage medium |
Non-Patent Citations (2)
| Title |
|---|
| ILWON JEONGKYUNGHOI KIM: "Evaluation of compressive strength and phosphate fixation characteristics of wastewater filter media using coal bottom ash and oyster shells", 《JOURNAL OF ENVIRONMENTAL MANAGEMENT》, pages 1 - 6 * |
| 李智 等: "基于表格的自动问答研究与展望", 《计算机工程与应用》, pages 67 - 76 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN116450578B (en) | 2023-09-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111259006B (en) | Universal distributed heterogeneous data integrated physical aggregation, organization, release and service method and system | |
| CN111753499B (en) | Method for merging and displaying electronic form and OFD format file and generating directory | |
| CN108228817A (en) | Data processing method, device and system | |
| US20060064428A1 (en) | Methods and apparatus for mapping a hierarchical data structure to a flat data structure for use in generating a report | |
| US20140317563A1 (en) | Generate field mapping | |
| CN111145051A (en) | Method and device for generating arbitration electronic document | |
| US11853365B2 (en) | Template-based faceted search experience | |
| JP2000148814A (en) | Component part data management system and computer readable storage medium with component part data management program stored therein | |
| CN106372044A (en) | Method for generating typed dimension XBRL (Extensible Business Reporting Language) report based on report form | |
| US9147040B2 (en) | Point-in-time query system | |
| CN114979120B (en) | Data uploading method, device, equipment and storage medium | |
| CN114090653A (en) | Resource data statistical method and device, meta-platform equipment and storage medium | |
| CN116468010A (en) | Report generation method, device, terminal and storage medium | |
| CN110110072A (en) | A kind of method, system, terminal and storage medium generating interactive electronic handbook | |
| CN115544183A (en) | Data visualization method and device, computer equipment and storage medium | |
| CN116401407A (en) | Node attribute configuration method, device, equipment and storage medium of mind map | |
| CN106127863B (en) | A kind of refrigerator foaming die series design system and its method | |
| CN116450578B (en) | Aircraft engine material data maintenance management method | |
| CN104699471B (en) | A kind of technical publications content delivering system and method | |
| CN105488146B (en) | Courseware material management method and system of computer aided training system | |
| JP7022472B1 (en) | Data management system, data management method and data management program | |
| US20180357297A1 (en) | Rdb system | |
| US9990415B2 (en) | Data structure for representing information using expressions | |
| Ziegler et al. | A metadata model to connect isolated data silos and activities of the CAE domain | |
| JP2004046650A (en) | Data management method and database structure |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |