CN114756976A - Method and system for generating work order in aircraft manufacturing and modifying - Google Patents

Method and system for generating work order in aircraft manufacturing and modifying Download PDF

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CN114756976A
CN114756976A CN202210676896.XA CN202210676896A CN114756976A CN 114756976 A CN114756976 A CN 114756976A CN 202210676896 A CN202210676896 A CN 202210676896A CN 114756976 A CN114756976 A CN 114756976A
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CN114756976B (en
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杨宾
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Beijing Hantuan Technology Co ltd
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Abstract

The invention provides a method and a system for generating a work sheet in aircraft manufacturing and modifying, wherein the work sheet is generated according to an aircraft manufacturing and modifying design drawing and an aircraft manufacturing and modifying range list, and the method comprises the following steps: analyzing the list of the manufacturing and modifying range of the aircraft to obtain analysis data; extracting a main graph in an aircraft manufacturing and modifying design drawing; reading main picture information in the main picture to generate a main picture work sheet; writing main picture information corresponding to the analysis data into the main picture worksheet; obtaining sub-image information contained in the main image and extracting the sub-image; reading sub-graph information in the sub-graphs and generating a sub-graph work sheet; writing the sub-graph information corresponding to the analysis data into a sub-graph work sheet; generating an incidence relation between the main graph and the sub graph, and generating an incidence relation between the main graph work order and the sub graph work order according to the incidence relation between the main graph and the sub graph; and respectively writing the analytical data corresponding to the main graph work order and the sub graph work order into the main graph work order and the sub graph work order, thereby generating the main graph work order and the sub graph work order.

Description

Method and system for generating work order in aircraft manufacturing and modifying
Technical Field
The invention relates to the field of aircraft manufacturing, in particular to a method and a system for generating a work order in aircraft manufacturing and modifying.
Background
The design drawing for manufacturing and modifying the aircraft is very important work guiding data in the process of manufacturing and modifying the aircraft and is also a main basis for manufacturing and modifying the aircraft. The design drawing for manufacturing and modifying the aircraft provides operation content, operation range and aviation material resource requirements in the operation process.
Aiming at the problem that a skilled engineer needs to continuously and repeatedly check and read and manually write a work sheet in thousands of drawings, thousands of operation resources and data during the manufacturing and modifying operation of the aircraft, and an operator is guided to carry out production operation according to a work card, so that great safety risk is generated and higher working cost is consumed.
Disclosure of Invention
In order to solve the problems in the background art, in a first aspect, the present invention provides a method for generating a work order in aircraft manufacturing and modifying, wherein the work order is generated according to an aircraft manufacturing and modifying design drawing and an aircraft manufacturing and modifying range list, and the generating method comprises the following steps: analyzing the list of the manufacturing and modifying ranges of the aircraft to obtain analysis data; extracting a main graph in the aircraft manufacturing and modifying design drawing; reading main picture information in the main picture and generating a corresponding main picture work sheet; writing main picture information corresponding to the analysis data into the main picture worksheet; obtaining sub-image information contained in the main image and extracting the sub-image; reading sub-graph information in the sub-graphs and generating corresponding sub-graph work lists; writing the sub-graph information corresponding to the analysis data into the sub-graph work sheet; generating the incidence relation between the main graph and the subgraph, and generating the incidence relation between the main graph work order and the subgraph work order according to the incidence relation between the main graph and the subgraph; and writing the analytic data corresponding to the main graph work order and the sub graph work order into the main graph work order and the sub graph work order respectively, thereby generating the main graph work order and the sub graph work order.
Further, extracting the main figures in the aircraft manufacturing and modifying design drawing comprises: acquiring a main figure number in a drawing information table of the drawing; scanning the drawing to match the main drawing number; taking the position of the main figure number as a base point, scanning a drawing, calculating the distance of a blank area along the scanning direction when the blank area is scanned, if the distance of the blank area is greater than a set boundary value, changing the scanning direction, continuing to scan by taking the position of the main figure number as the base point, and continuing to scan when content is scanned; when a blank area is scanned, calculating a blank area distance by taking the boundary position of a non-blank area and the blank area as a starting point, and if the blank area distance is greater than a set boundary value, taking the boundary position as the main image boundary point; when the scanning is finished, connecting the boundary points of the main graphs to form a closed graph, and taking the enclosed closed graph as the boundary of the main graph; and extracting the content in the boundary of the main graph to form the main graph.
Further, the method also comprises a content judgment step after the content is scanned; judging whether the content is a subgraph number or not; if so, taking the boundary of the content as the boundary of the main graph, and changing the scanning direction to continue scanning; if not, continuing to scan.
Further, extracting the subgraph comprises: identifying the subgraph drawing code and the position code in the main graph; positioning the sub-image position according to the sub-image position code, scanning the drawing by taking the position of the drawing code of the sub-image as a base point, calculating the distance of a blank area along the scanning direction when the blank area is scanned, if the distance of the blank area is greater than a set boundary value, converting the scanning direction, continuing to scan by taking the position of the sub-image number as the base point, and continuing to scan when the content is scanned; when a blank area is scanned, calculating a blank area distance by taking the boundary position of a non-blank area and the blank area as a starting point, and if the blank area distance is greater than a set boundary value, taking the boundary position as the sub-image boundary point; when the scanning is finished, connecting the boundary points of the subgraphs to form a closed graph, and taking the enclosed closed graph as the boundary of the subgraph; and extracting the content in the boundary of the subgraph to form the subgraph.
Further, analyzing the list of the aircraft manufacturing and modifying ranges to obtain analysis data, comprising the steps of: positioning a target page of the aircraft manufacturing and modifying range list through tag information; reading the content in the target page one by one to obtain structured data; and when an empty line is read in the target page, completing the content analysis in the target page to obtain the analysis data.
Further, the generating method further includes a working range determining step: reading the analysis data, and acquiring working range data in the analysis data; and determining the main graph work sheet and the sub graph work sheet corresponding to the working range according to the working range data.
In a second aspect, the present invention also provides a work order generation system in aircraft manufacturing retrofitting, comprising:
the refitting range list analyzing module is used for analyzing the aircraft manufacturing refitting range list to obtain analysis data; the main picture extraction module is used for extracting a main picture in an aircraft manufacturing modification design drawing; the main picture information analysis module is used for reading the main picture information in the main picture and generating a corresponding main picture work sheet; the main picture work order writing module is used for writing the main picture information corresponding to the analysis data into the main picture work order; the subgraph extraction module is used for acquiring subgraph information contained in the main graph and extracting the subgraph; the sub-graph information analysis module is used for reading sub-graph information in the sub-graphs and generating corresponding sub-graph work lists; a sub-graph information writing module used for writing the sub-graph information corresponding to the analysis data into the sub-graph work sheet; the structural relationship generation module is used for generating the association relationship between the main graph and the subgraph and generating the association relationship between the main graph work order and the subgraph work order according to the association relationship between the main graph and the subgraph; and the analysis data writing module is used for writing analysis data corresponding to the main work order and the sub-image work order into the main work order and the sub-image work order respectively so as to generate the main work order and the sub-image work order.
Further, the system also comprises a storage module for storing the main graph, the subgraph, the main graph work order and the subgraph work order; main pictures and subgraphs in the structuring module, main picture work lists and subgraph work list structuring data; and the modification range list analysis module obtains analysis data.
Furthermore, the system also comprises a test work management system which is used for reading the main graph information and the test work information contained in the sub graph information obtained by the main graph and sub graph data analysis module and associating the required test work information with the work order.
Furthermore, the system also comprises a drawing management module which is used for importing, auditing, version management and storage of drawings required in the aircraft manufacturing and modification.
Furthermore, the system also comprises an engineering file management system which is used for reading the main graph information and the engineering file information contained in the sub graph information which are obtained by the main graph and sub graph information analysis module, obtaining a corresponding test work task according to the engineering file information, and associating the test work task with a corresponding work order.
The invention has the following beneficial effects:
the work order generation method is based on the analysis of the modification range list and the modification design drawing, generates the corresponding work order according to the analysis result, associates the work order with the drawing, the required aircraft material information and the like, and finally obtains the complete work order, so that the generated work order is used for guiding production and manufacturing, the requirement of the capability of workers when the work order is manually made is lowered, the uncontrollable problem caused by human factors is avoided, the error probability is lowered, and the work order generation efficiency is improved.
Drawings
FIG. 1 is a flow chart of a method of generating a work order in an aircraft manufacturing retrofit of the present invention;
fig. 2 is a schematic structural diagram of a work order generation system in the modification of aircraft manufacturing according to the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs; the terminology used in the description of the application herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the application; the terms "including" and "having," and any variations thereof in the description and claims of this application and the description of the figures above, are intended to cover non-exclusive inclusions.
Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the application. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments.
The work order generation method and system in the aircraft manufacturing retrofit according to the present invention will be described in detail below with reference to the accompanying drawings.
As shown in fig. 1, the method for generating a work order in aircraft manufacturing and modifying of the present invention includes steps S1-S9, wherein the work order needs to be generated according to an aircraft manufacturing and modifying design drawing and an aircraft manufacturing and modifying range list, and specifically, the steps of generating the work order are as follows.
S1, analyzing a list of manufacturing and modifying ranges of the aircraft to obtain analysis data; s2, extracting a main picture in an aircraft manufacturing modification design drawing (the step S2 can be carried out simultaneously with or before S1 or S1, and the names of S1 and S2 are used for distinguishing steps and not for emphasizing the sequence); s3, reading main picture information (including a main picture drawing number (used as a work order number for generating a work order), a sub-picture number, a sub-picture position code, a navigation material number and the like) in the main picture, and generating a corresponding main picture work order (the content of the work order is empty and has no data); s4, writing main map information data (including resource information (such as a navigation material number) and a drawing number) corresponding to the analysis data into a main map work sheet; s5, obtaining sub-image information (including sub-image numbers and position codes) contained in the main image, and extracting the sub-image; s6, reading sub-graph information (a sub-graph number and resource information (namely a navigation material number)) in the sub-graph, and generating a corresponding sub-graph work sheet (taking the sub-graph number as a work sheet number); s7, writing the sub-image information data (including resource information (namely navigation material number) and sub-image number) corresponding to the analysis data into the sub-image work sheet; s8, generating an incidence relation between the main graph and the sub graph, and generating an incidence relation between the main graph work sheet and the sub graph work sheet according to the incidence relation between the main graph and the sub graph; and S9, respectively writing the analytic data corresponding to the main graph work sheet and the sub graph work sheet (namely the data corresponding to the resource information (navigation material number) in the main graph information, the resource information (navigation material number) in the drawing number and the drawing number in the sub graph information) into the main graph work sheet and the sub graph work sheet, and generating the main graph work sheet and the sub graph work sheet.
The work order generation method of the invention is suitable for: currently active air passenger companies a330, 320, 350; boeing B737, 747, 757, 767, 777; and (4) refitting various commercial airplanes such as domestic commercial airplanes ARJ21 and C919. The work order generation method is based on the analysis of the modification range list and the modification design drawing, generates the corresponding work order according to the analysis result, correlates the work order with the drawing, the required aviation material information and the like, and finally obtains the complete work order, so that the generated work order is used for guiding production and manufacturing, thereby not only reducing the requirement of the capability of workers when the work order is manually made, but also avoiding the uncontrollable problem caused by human factors, further reducing the error probability and improving the efficiency of work order generation.
Further, the generating method further includes a working range determining step: reading the analysis data, and acquiring working range data in the analysis data; and determining the main work sheet and the sub-picture work sheet corresponding to the work range according to the work range data, thereby determining the work sheet range related to the refitting operation.
In step S1, the list of aircraft manufacturing and modifying ranges is parsed to obtain parsed data, which specifically includes steps S11-S13.
S11, positioning a target page of the aircraft manufacturing and modifying range list through the tag information. It should be noted that the content in the existing list of the aircraft manufacturing and modifying range includes a data table, where the data table includes a table name and a field name, where the field name is a flight material number or a work order number, where the work order number is a drawing number or a work order number, where the table name may be referred to as tag information, and the tag information is located on a target page, and the field name is associated with the work order content. And S12, reading the content in the target page one by one (namely reading line by line, and reading line by line when reading an empty line) to obtain structured data. And S13, when an empty row is read in the target page (when all column fields in a certain row are empty), the content in the target page is analyzed and analyzed data are obtained. The analysis data at least comprises a navigation material number, required resource information (such as navigation materials required during refitting operation) and engineering document information corresponding to the navigation material number, operation execution condition information (including work type, work time period and work sequence) corresponding to a drawing number (work order number) and test work information required after refitting is completed.
The method comprises the steps that an aircraft manufacturing and modifying range list is an Excel format file with multiple sheet tabs, the content in the aircraft manufacturing and modifying range list comprises a data table, the data table comprises table names and field names, and the table names are consistent with the sheet tab names in the Excel format file in the aircraft manufacturing and modifying range list needing to be analyzed; positioning the content to be analyzed through the label information, and scanning line by using an OCR technology to obtain analysis data; and forming structured data according to the sheet tab-specific number of rows-columns. For example, the material information: specifically, a flight material number label (the flight material number refers to a flight material identification number defined by an aircraft manufacturer and available on the aircraft of the model) represented by 16-bit character string feature data of a combination of numbers, letters and a-is matched with the contents in the list of the aircraft manufacturing and modifying ranges, the contents (specific number of lines) of a sheet tab in the list of the modifying ranges are located, and scanning is started.
In step S2, extracting the main map in the aircraft manufacturing retrofit design drawing includes steps S21-S25.
S21, obtaining a main figure number in a drawing information table of the drawing (the drawing information table is a table at a fixed position in the drawing, the table contains the main figure number of the drawing, the main figure number is the figure number of the main figure in the drawing, and the main figure number is used as a work order number).
And S22, scanning the drawing to match the number of the main picture.
S23, taking the position of the main pattern number as a base point, and scanning the drawing (such as scanning line by line or in rows): when a blank area is scanned, calculating the distance of the blank area along the scanning direction, if the distance of the blank area is greater than a set boundary value (for example, the minimum distance between the parts of each sub-image with contents in the image is determined according to the actual situation), converting the scanning direction, and continuously scanning by taking the position of the main image number as a base point; when the content is scanned, the scanning is continued, namely, the scanning is continued according to the original direction.
Further, after the content is scanned, the method further comprises a content judgment step: whether the content is a sub-graph number (the sub-graph number is generally in a combined label (for example, an arrow linking line links a combined graph of the sub-graph number) is judged, when a similar combined label is scanned, the sub-graph number is judged to be scanned or the comparison can be directly carried out by taking an existing sub-graph number template as a reference, when the content which is the same as the existing sub-graph number template is scanned, the boundary of the content can be taken as the boundary point of the main graph, if so, the boundary of the content is taken as the boundary of the main graph, the scanning direction is changed to continue the scanning, if not, the scanning is continued, namely, the scanning is continued according to the original direction, and therefore, two drawings (the main graph and the sub-graph) are prevented from being mistaken for one drawing.
And S24, when the blank area is scanned, calculating a blank area distance by taking the boundary position of the non-blank area and the blank area as a starting point, and if the blank area distance is greater than a set boundary value, taking the boundary position as a main image boundary point.
S25, connecting the boundary points of the main graph to form a closed graph after scanning is finished, and taking the enclosed closed graph as the boundary of the main graph; and S26, extracting the content in the boundary of the main graph to form the main graph.
In step s3, reading the main graph information in the main graph, generating a corresponding main graph work sheet and step s6, reading the sub graph information in the sub graph, and in generating a corresponding sub graph work sheet, the adopted reading method is the same, specifically: scanning the main graph and the sub graph by using analytical data (aircraft material number and/or drawing number) of the list of the modified range as a comparison template through an OCR (optical character recognition) technology; and when the main map and the sub-map information matched with the analysis data are scanned, forming an association relation between the navigation material number and the drawing where the navigation material number is located and the content corresponding to the navigation material number and/or the drawing number in the analysis data, and storing the association relation.
In step S5, extracting the subgraph includes steps S51-S55.
S51, identifying the subgraph drawing code and the position code in the main graph; the subgraphs contained in the main graph all have independent coding positions (specifically, a box pattern with characters inside) and subgraph numbers in the main graph.
S52, positioning to a sub-graph position (sub-graph drawing coding position) according to the sub-graph position coding, wherein the sub-graph drawing coding positioning method comprises the following steps: the subgraph drawing code is positioned through drawing coordinates, the drawing coordinates refer to the intersection points of the x and y axes of the drawing, the x and y axes of each drawing are coordinate values which are symmetrical by letters and numbers on the left and right and up and down of the drawing respectively, and the intersection points of the coordinate values are coordinate values; if taking the position code 41D25 as an example, 41 represents the number of the sub-drawing, D is the x-axis coordinate, and 25 is the y-axis coordinate; the positioning method is as follows: determining the position where the coordinate is the intersection of the X-axis coordinate D point and the Y-axis coordinate 25 point, namely the position point of the 41 th drawing number of the sub-drawing), scanning the drawing by taking the position where the drawing code of the sub-drawing is located as a base point, calculating the distance of a blank area along the scanning direction when the blank area is scanned, if the distance of the blank area is greater than a set boundary value, converting the scanning direction, continuing to scan by taking the position where the sub-drawing number is located as the base point, and continuing to scan when the content is scanned.
S53, when the blank area is scanned, calculating the blank area distance by taking the boundary position of the non-blank area and the blank area as a starting point, and if the blank area distance is larger than a set boundary value, taking the boundary position as a sub-image boundary point.
And S54, when the scanning is finished, connecting the boundary points of the subgraphs to form a closed graph, and taking the enclosed closed graph as the boundary of the subgraph.
And S55, extracting the content in the boundary of the subgraph to form the subgraph.
Referring to fig. 2, the invention relates to a work order generation system in aircraft manufacturing and modification, which comprises: the modification range list analysis module is used for analyzing the aircraft manufacturing modification range list to obtain analysis data; the main picture extraction module is used for extracting a main picture in an aircraft manufacturing modification design drawing; the main picture information analysis module is used for reading the main picture information in the main picture and generating a corresponding main picture work sheet; the main picture work order writing module is used for writing the main picture information corresponding to the analytic data into the main picture work order; the subgraph extraction module is used for acquiring subgraph information contained in the main graph and extracting subgraphs; the sub-graph information analysis module is used for reading sub-graph information in the sub-graphs and generating corresponding sub-graph work lists; the sub-graph information writing module is used for writing the sub-graph information corresponding to the analysis data into the sub-graph work list; the structural relationship generation module is used for generating the incidence relationship between the main graph and the subgraph and generating the incidence relationship between the main graph work order and the subgraph work order according to the incidence relationship between the main graph and the subgraph; and the analysis data writing module is used for writing the analysis data corresponding to the main graph work sheet and the sub graph work sheet into the main graph work sheet and the sub graph work sheet respectively so as to generate the main graph work sheet and the sub graph work sheet.
The work sheet generation system obtains analysis data based on the modification range list analysis module, the main/sub image extraction module is split to obtain a main image and a sub image, the main/sub image information analysis module obtains main/sub image information (navigation material information and drawing number) required in modification, the main/sub image information write-in module writes the analysis data corresponding to the main/sub image information into a work sheet, then the analysis data corresponding to the main/sub image information is written into the work sheet, therefore, a final work sheet which can be used for work guidance is generated, the corresponding relation between the work sheet and the main image or the sub image and the corresponding relation between the work sheet and the analysis data are structurally stored, and the corresponding drawing and required navigation material resources can be reflected in the work sheet when the work sheet is extracted. Guiding production and manufacturing by the generated worksheet; the requirement on the capability of workers when the worksheet is made manually in the prior art is reduced, the uncontrollable problem caused by human factors is avoided, and the error probability is reduced; and the efficiency of the work order generation is improved.
Furthermore, the work order generation system of the invention also comprises a storage module, a storage module and a processing module, wherein the storage module is used for storing the main graph, the subgraph, the main graph work order and the subgraph work order; the main graph and the sub graph and the structural data of the main graph work order and the sub graph work order in the structural module (the structural data is the subordination relation between the main graph and the sub graph and the corresponding relation between the main graph and the main graph work order, the sub graph and the sub graph work order); and the modification range list analysis module obtains analysis data corresponding to the main graph work sheet and the sub graph work sheet.
Furthermore, the work order generation system of the invention further comprises a test work management system, which is used for reading the test work information contained in the main graph information and the sub graph information obtained by the main graph data analysis module and the sub graph data analysis module and associating the required test work information with the corresponding work order.
Furthermore, the work order generation system of the invention further comprises a file management module, which is used for uploading, importing, process approving (including uploading, examining and releasing of files), version management (mainly storing historical versions and version validity management, and analyzing effective versions) and storage of drawings and modification range list files required in aircraft manufacturing and modification.
Furthermore, the work order generation system of the invention also comprises an engineering file management system, which is used for reading the main picture information and the engineering file information contained in the sub-picture information obtained by the main picture and sub-picture information analysis module, obtaining the corresponding test work task according to the engineering file information, and associating the test work task with the corresponding work order; the engineering documentation information referred to herein is component update information sent by the aircraft manufacturer.
Furthermore, the work order generation system of the invention also comprises a label management module used for storing labels used in analysis, and the modification range list analysis module, the main picture extraction module, the main picture information analysis module, the main picture work order writing module, the subgraph extraction module, the subgraph information analysis module, the subgraph work order writing module, the analysis data writing module and the test work management system adopt the labels in the label management module to analyze the content.
Furthermore, the work order generation system of the invention also comprises a work range analysis module for reading the analysis data and obtaining the work range data in the analysis data; and determining the main graph work sheet and the sub graph work sheet corresponding to the working range according to the working range data.

Claims (10)

1. A method for generating a work order in aircraft manufacturing and modifying, wherein the work order is generated according to an aircraft manufacturing and modifying design drawing and an aircraft manufacturing and modifying range list, and the method for generating the work order comprises the following steps:
analyzing the list of the aircraft manufacturing and modifying range to obtain analysis data;
extracting a main graph in the aircraft manufacturing and modifying design drawing;
reading main picture information in the main picture and generating a corresponding main picture work sheet;
writing main picture information corresponding to the analysis data into the main picture worksheet;
obtaining sub-image information contained in the main image and extracting the sub-image;
reading sub-graph information in the sub-graphs and generating corresponding sub-graph work lists;
writing sub-graph information corresponding to the analysis data into the sub-graph worksheet;
generating the incidence relation between the main graph and the subgraph, and generating the incidence relation between the main graph work order and the subgraph work order according to the incidence relation between the main graph and the subgraph;
and writing the analytic data corresponding to the main graph work order and the sub graph work order into the main graph work order and the sub graph work order respectively, thereby generating the main graph work order and the sub graph work order.
2. The method of generating a work order in an aircraft manufacturing retrofit of claim 1 wherein extracting a master graph in the aircraft manufacturing retrofit design drawing comprises:
acquiring a main figure number in a drawing information table of the drawing;
scanning the drawing to match the main drawing number;
taking the position of the main figure number as a base point, scanning a drawing, calculating the distance of the blank area along the scanning direction when the blank area is scanned, if the distance of the blank area is greater than a set boundary value, converting the scanning direction, continuing to scan by taking the position of the main figure number as the base point, and continuing to scan when contents are scanned;
when a blank area is scanned, calculating a blank area distance by taking the boundary position of a non-blank area and the blank area as a starting point, and if the blank area distance is greater than a set boundary value, taking the boundary position as the main image boundary point;
when the scanning is finished, connecting the boundary points of the main graph to form a closed graph, and taking the enclosed closed graph as the boundary of the main graph;
and extracting the content in the boundary of the main graph to form the main graph.
3. The method of claim 2, further comprising a content determination step after the content is scanned;
judging whether the content is a subgraph number or not;
if so, taking the boundary of the content as the main graph boundary, and changing the scanning direction to continue scanning;
if not, continuing to scan.
4. The method of generating a work order in an aircraft manufacturing retrofit of claim 1 wherein extracting the sub-graph comprises:
identifying the subgraph drawing code and the position code in the main graph;
positioning the sub-image position according to the sub-image position code, scanning the drawing by taking the position of the drawing code of the sub-image as a base point, calculating the distance of a blank area along the scanning direction when the blank area is scanned, if the distance of the blank area is greater than a set boundary value, converting the scanning direction, continuing to scan by taking the position of the sub-image number as the base point, and continuing to scan when the content is scanned;
when a blank area is scanned, calculating a blank area distance by taking the boundary position of a non-blank area and the blank area as a starting point, and if the blank area distance is greater than a set boundary value, taking the boundary position as the sub-image boundary point;
when the scanning is finished, connecting the boundary points of the subgraphs to form a closed graph, and taking the enclosed closed graph as the boundary of the subgraph;
and extracting the content in the boundary of the subgraph to form the subgraph.
5. The method of generating a work order in aircraft manufacturing and converting as claimed in claim 1, wherein parsing the list of aircraft manufacturing and converting ranges to obtain parsed data comprises the steps of:
positioning a target page of the aircraft manufacturing and modifying range list through tag information;
reading the content in the target page one by one to obtain structured data;
and when an empty line is read in the target page, completing the content analysis in the target page to obtain the analysis data.
6. The method of generating a work order in aircraft manufacturing retrofitting according to claim 1, characterized in that it further comprises a work range determining step:
reading the analysis data, and acquiring working range data in the analysis data;
and determining the main graph work sheet and the sub graph work sheet corresponding to the working range according to the working range data.
7. A work order generation system in aircraft manufacturing retrofitting, comprising:
the modification range list analysis module is used for analyzing the aircraft manufacturing modification range list to obtain analysis data;
the main graph extraction module is used for extracting a main graph in an aircraft manufacturing modification design drawing;
the main picture information analysis module is used for reading the main picture information in the main picture and generating a corresponding main picture work sheet;
the main picture work order writing module is used for writing the main picture information corresponding to the analysis data into the main picture work order;
the subgraph extraction module is used for acquiring subgraph information contained in the main graph and extracting the subgraph;
the subgraph information analysis module is used for reading the subgraph information in the subgraph and generating a corresponding subgraph work list;
a sub-graph information writing module used for writing the sub-graph information corresponding to the analysis data into the sub-graph work sheet;
the structural relationship generation module is used for generating the association relationship between the main graph and the subgraph and generating the association relationship between the main graph work order and the subgraph work order according to the association relationship between the main graph and the subgraph;
and the analysis data writing module is used for writing analysis data corresponding to the main graph work sheet and the sub graph work sheet into the main graph work sheet and the sub graph work sheet respectively, so that the main graph work sheet and the sub graph work sheet are generated.
8. The work order generation system in aircraft manufacturing retrofitting according to claim 7, further comprising a storage module,
the main graph, the subgraph, the main graph work list and the subgraph work list are stored;
structuring data of main pictures and sub-pictures and main picture work orders and sub-picture work orders in the structuring module;
and the modification range list analysis module obtains analysis data.
9. The system of claim 7, further comprising a test job management system configured to read the main graph information and the sub graph information obtained by the main graph data parsing module and the sub graph data parsing module, and associate the required test job information with the work order.
10. The system of claim 7, further comprising a document management module configured to upload, import, process approval, version management, and store the drawing and modification range manifest document required in the aircraft manufacturing modification.
CN202210676896.XA 2022-06-16 2022-06-16 Method and system for generating work order in aircraft manufacturing and modifying Active CN114756976B (en)

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