CN102541109A - Method for manufacturing satellite star surface temperature-control multilayer - Google Patents
Method for manufacturing satellite star surface temperature-control multilayer Download PDFInfo
- Publication number
- CN102541109A CN102541109A CN2011104171674A CN201110417167A CN102541109A CN 102541109 A CN102541109 A CN 102541109A CN 2011104171674 A CN2011104171674 A CN 2011104171674A CN 201110417167 A CN201110417167 A CN 201110417167A CN 102541109 A CN102541109 A CN 102541109A
- Authority
- CN
- China
- Prior art keywords
- multilayer
- satellite star
- temperature control
- satellite
- star catalogue
- 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
Images
Abstract
The invention discloses a method for manufacturing a satellite star surface temperature-control multilayer, which comprises the following steps: drawing a pattern of a two-dimensional temperature-control multilayer; transmitting the pattern to a numerical control cutting machine tool; and cutting the multilayer material according to the transmitted patterns at the proportion of 1 to 1, mask-packing and sewing to obtain the multilayer final product, wherein the step of drawing the pattern of the two-dimensional temperature-control multilayer comprises two ways, including a multilayer two-dimension expanding step based on three-dimension model of a to-be-covered part of the satellite star surface and a combined drawing step of a two-dimension pattern based on the to-be-covered part of the satellite star surface. Compared with the prior art, the sampling of real objects is partially replaced by electronic design of the temperature-control multilayer pattern, so that the sampling time of the real objects is shortened by over 80 percent. Meanwhile, the pure manual work is replaced by the automatic manufacturing process of the temperature-control multilayer, and the total efficiency of manufacturing and installing the multilayer is improved by over 50 percent.
Description
Technical field
Field of thermal insulation of the present invention is specifically related to a kind of manufacturing approach of temperature control multilayer of satellite star catalogue.
Background technology
Violent to the space environment temperature variation, for guaranteeing satellite instrument, equipment operate as normal, must carry out heat control to satellite, require usually temperature in the satellite cabin is controlled at 0～40 ℃, then there is stricter requirement at some instrument or position.The thermal control technology can be divided into the passive heat control technology and initiatively heat control is technological; The temperature control multilayer material is superimposed by the wall of the reflection horizon of high reflectance and lower thermal conductivity usually and forms; Can form very high thermal resistance to the irradiation hot-fluid; Having good heat-proof quality, is the most frequently used passive type thermal control means.
What existing star catalogue temperature control multilayer was made employing all is to be main method for making with the manual operations, and roughly flow process is following: 1. earlier make pattern according to the pattern of design drawing with kraft; 2. be that the material object sampling on the details is checked and accomplished to star with pattern; 3. according to sampling result in kind, make the multilayer model with steel plate paper; 4. use model cutting on multilayer material, blanking, form the multilayer semi-manufacture; 5. accomplish the outer facial mask of bag of multilayer and make formation multilayer finished product.
Making by hand with sample circuit in kind is that the traditional fabrication mode of characteristic feature exists following deficiency: sampling process 1. in kind need take satellite assembly main line time 2-3 days, and sampling operation can reduce the Product Safety in total process of assembling; 2. it is lower to make efficient by hand, needs to make pattern, model and multilayer, and working load is heavy, the cycle is long, and labour intensity is big.
Cause the reason of above deficiency: 1. loss of learning on the part multilayer drawing, the pin positional information is incomplete, and position of opening and dimension information are inaccurate, therefore need earlier according to the drawing making pattern and broadcast TV programs by satellite and check; 2. only rely on jack board (like wallpaper cutter, scissors) etc. to carry out multilayer and make, lack making apparatus and corresponding process efficiently.
Therefore; Need on the one hand, true-to-size multilayer drawing design complete to reduce sampling in kind on the star through key element; On the other hand need be through introducing sophisticated equipment, optimizing and make flow process; Minimizing improves temperature control multilayer make efficiency in the human input of aspects such as paper pattern forming, sample making and multilayer cutting.
Summary of the invention
Based on the problems referred to above, the object of the present invention is to provide a kind of efficient, method that high-quality is made satellite star catalogue temperature control multilayer, being intended to digitizing, robotization means is that to replace with material object sampling, manual operations be the traditional handicraft of core for the new process of core.
A kind of manufacturing approach of satellite star catalogue temperature control multilayer; May further comprise the steps: draw two-dimentional temperature control multilayer pattern, this pattern is sent to numerical control cutting lathe, uses multilayer material to carry out cutting, carry out envelope film and making to obtain above-mentioned multilayer finished product again with 1: 1 ratio according to transmitting pattern; Wherein, The pattern step of drawing two-dimentional temperature control multilayer comprises dual mode, promptly based on satellite star catalogue face wait to coat the position three-dimensional model the multilayer two-dimension deployment step or wait that based on satellite star catalogue face the two-dimentional drawing that coats the position makes up the step of drafting;
Wherein, the said multilayer two-dimension deployment step of waiting to coat the three-dimensional model at position based on satellite star catalogue face mainly comprises:
Step 1: set up and wait to coat the three-dimensional model at position, this three-dimensional model is the multilayer surface model;
Step 2: said three-dimensional model is launched into the plurality of sub piece, and the panel beating module in the utilization 3 d modeling software is launched into said three-dimensional model n X-Y scheme piece of n >=1;
Step 3: sub-piece splicing; If n >=2 then need are stitched together the X-Y scheme piece according to border syntople in the said three-dimensional model; Again in the measure two dimensional graph block with the corresponding critical size of said three-dimensional model; And compare with the measurement result of said three-dimensional model, error need be controlled in 1 ‰;
Step 4: add flange, lap joint process surplus;
Saidly wait that based on satellite star catalogue face the two-dimentional drawing that coats the position makes up the step of drafting, mainly comprises:
Step a: on hardening the basis of composition in the satellite cabin, in conjunction with multilayer coat, the technical requirement of scrap (bridge), draw and obtain the outline that the satellite star catalogue waits to coat the position multi-layer graphical;
Step b: on the basis of the multilayer drawing that step a obtains, in conjunction with the pin layout of satellite star catalogue temperature control multilayer, the relevant position of profile diagram adds pin hole outside, forms the multi-layer graphical that comprises outline and pin hole;
Step c: on the multi-layer graphical basis that comprises outline and pin hole that step b obtains; Initial conditions according to instrument installation diagram, instrument profile atlas, waveguide installation diagram and cable installation diagram; Dodge the drafting in hole, the size of dodging the hole is actual 1.05 times of need dodge the object corresponding size on the satellite star catalogue;
Steps d: on the basis of the multilayer drawing that step c obtains, the actual conditions when broadcasting TV programs by satellite sampling, installation according to multilayer increase corresponding technology cutting opening.
Preferably, before above-mentioned cutting step, utilize kraft to carry out pre-cut earlier to confirm pattern and to wait to coat the matching at position.
Wherein, set up in the step 1 and wait that the three-dimensional model that coats the position is meant that the utilization 3 d modeling software carries out the curved surface modeling of temperature control multilayer according to multilayer coating position actual conditions, the surface model of being set up intactly covers the coating position of multilayer.
Wherein, the 3 d modeling software described in the step 2 is Pro/Engineer, Solidworks, CATIA.
Wherein, after interpolation flange in the step 4 and overlap joint are meant that the multilayer two-dimension figure forms, add flange and overlap joint surplus at the outline place, the flange amount is about 25mm, and amount of lap is about 30mm.
Wherein, reality described in the step c need be dodged object and comprises instrument and waveguide.
Wherein, the broadcast TV programs by satellite sampling, the actual conditions when installing of said multilayer is meant that multilayer delivers to the root that is installed on the plate of cabin from the instrument head cover, and head dimensions is greater than root.
The manufacturing approach of satellite star catalogue temperature control multilayer of the present invention, the electronization design part replacement sampling in kind through temperature control multilayer drawing is shortened more than 80% sample time in kind; Simultaneously, the automated production flow process of temperature control multilayer has substituted pure hand labour, and multilayer is made and installed total efficiency and improves more than 50%.
Description of drawings
Fig. 1 is the process chart of the manufacturing approach of satellite star catalogue temperature control multilayer of the present invention.
Embodiment
Be further described below in conjunction with the manufacturing approach of accompanying drawing satellite star catalogue temperature control multilayer of the present invention.
Shown in Figure 1; The manufacturing approach of satellite star catalogue temperature control multilayer of the present invention; Comprise the pattern of drawing two-dimentional temperature control multilayer, this pattern is sent to numerical control cutting lathe, uses multilayer material to carry out cutting, carry out envelope film and making to obtain step (hereinafter to be referred as sub-process III) such as above-mentioned multilayer finished product again with 1: 1 ratio according to transmitting pattern; Wherein, The pattern step of drawing two-dimentional temperature control multilayer comprises dual mode, promptly based on satellite star catalogue face wait to coat the position three-dimensional model multilayer two-dimension deployment step (hereinafter to be referred as sub-process I) or wait that based on satellite star catalogue face the two-dimentional drawing that coats the position makes up the step (hereinafter to be referred as sub-process II) of drafting.
Sub-process III
The operation steps of sub-process III is following:
Step 1: drawing conversion, cut-parts composing, numerical control programming, the utilization special software is corresponding cut-parts with electronic switch; And, be utilized as target with the optimization of material according to used raw-material size (like the kraft width is that 1.8m, length are not limit, and the multilayer material width is that 1.2m, length are 4.5m), and carry out the composing of cut-parts, form the figure that sets type; Then composing figure is converted into numerical control program;
Step 2: with numerical control cutting lathe (like the GTXL of U.S. Ge Bai company) cutting kraft; With kraft is starting material; On numerical control cutting lathe, carry out the cutting operation, obtain the ox-hide pattern of multilayer and on pattern, mark corresponding information such as figure number with the numerical control program that obtains in the step 1;
Step 3: broadcast TV programs by satellite and check, to satellite, check, check around key elements such as outline, pin hole position, position of opening and size, process-cut processing, and suggestion for revision is identified at the ox-hide pattern with the ox-hide pattern that obtains in the step 2;
Step 4: judging whether needs to revise the multilayer drawing, if the multilayer drawing needs to revise, then gets into step 5 (plate is counter to be asked with interpreting blueprints, and revisions on drawings is also accomplished numerical control programming); If the multilayer drawing does not need to revise, then get into step 6 (with numerical control cutting lathe cutting multilayer);
Step 5: plate is counter to be asked with interpreting blueprints; Revisions on drawings is also accomplished numerical control programming, and the multiwall kraft appearance for needs are revised is then carried out the counter of pattern with the interpreting blueprints plate and asked; Formation meets the multilayer drawing of satellite actual conditions, and has worked out numerical control program according to flow process in the book process step 1;
Step 6: with numerical control cutting lathe cutting multilayer, be starting material, on numerical control cutting lathe, carry out the cutting operation, obtain the multilayer semi-manufacture and on semi-manufacture, marking corresponding information such as figure number with numerical control program with the multilayer;
Step 7: multilayer envelope film, make, according to technical requirement, facial mask and facial mask and multilayer be sewed together on multilayer outsourcing bread can form the multilayer finished product.
Sub-process I
Sub-process I is applicable to that multilayer is coated on the situation on the three-dimensional profile, and operation steps is following:
Step 1: set up and wait to coat the three-dimensional model at position, coat the position actual conditions according to multilayer, the utilization 3 d modeling software carries out the curved surface modeling of temperature control multilayer, and the surface model of being set up need intactly cover the coating position of multilayer;
Step 2: model is launched into the plurality of sub piece, and the panel beating module among the utilization 3 d modeling software Pro/Engineer is launched into the individual X-Y scheme piece of n (n >=1) with the multilayer surface model;
Step 3: the splicing of sub-piece, at first, if n >=2 then need are stitched together the X-Y scheme piece according to border syntople in the three-dimensional model; Then, with the corresponding critical size of three-dimensional surface model, and compare with the measurement result of three-dimensional surface model in the measure two dimensional graph block, error need be controlled in 1 ‰;
Step 4: add flange, lap joint process surplus, after the multilayer two-dimension figure forms, add flange and overlap joint surplus at the outline place according to the technology experience, generally speaking, the flange amount is about 25mm, and amount of lap is about 30mm; So far, can form the two-dimentional drawing of the multilayer that is coated on the complex three-dimensional profile.
Sub-process II
Sub-process II is applicable to that multilayer is coated on the situation on the two dimensional surface, and operation steps is following:
Step 1: draw the multi-layer graphical outline, harden the basis of composition in the satellite cabin on, combine multilayer coating, scrap (bridge) technical requirement, obtain the outline of multi-layer graphical;
Step 2: add pin hole, on the basis of the multilayer drawing that step 1 obtains, in conjunction with satellite star catalogue temperature control multilayer pin layout, the relevant position of profile diagram adds pin hole outside, forms the multi-layer graphical that comprises outline and pin hole;
Step 3: add and dodge the hole, on the basis of the multilayer drawing that step 2 obtains,, on diagram, dodge the drafting in hole according to initial conditions such as instrument installation diagram, instrument profile atlas, waveguide installation diagram and cable installations diagram; Generally speaking, the size of dodging the hole is 1.05 times that reality need be dodged object (like instrument, waveguide) corresponding size;
Step 4: add the technology cutting opening; On the basis of the multilayer drawing that step 3 obtains; Consider the actual conditions (need deliver to the root that is installed on the plate of cabin like multilayer, and head dimensions being greater than root) when multilayer is broadcast TV programs by satellite sampling, installation, increase corresponding technology cutting opening from the instrument head cover; So far, can accomplish the drawing that is coated on the multilayer on the two dimensional surface.
Although the preceding text specific embodiments of the invention has given to describe in detail and explanation; But what should indicate is; We can carry out various equivalences to above-mentioned embodiment according to conception of the present invention and change and modification; When the function that it produced does not exceed spiritual that instructions and accompanying drawing contain yet, all should be within protection scope of the present invention.
Claims (7)
1. the manufacturing approach of a satellite star catalogue temperature control multilayer; May further comprise the steps: draw two-dimentional temperature control multilayer pattern, this pattern is sent to numerical control cutting lathe, uses multilayer material to carry out cutting, carry out envelope film and making to obtain above-mentioned multilayer finished product again with 1: 1 ratio according to transmitting pattern; Wherein, The pattern step of drawing two-dimentional temperature control multilayer comprises dual mode, promptly based on satellite star catalogue face wait to coat the position three-dimensional model the multilayer two-dimension deployment step or wait that based on satellite star catalogue face the two-dimentional drawing that coats the position makes up the step of drafting;
Wherein, the said multilayer two-dimension deployment step of waiting to coat the three-dimensional model at position based on satellite star catalogue face mainly comprises:
Step 1: set up and wait to coat the three-dimensional model at position, this three-dimensional model is the multilayer surface model;
Step 2: said three-dimensional model is launched into the plurality of sub piece, and the panel beating module in the utilization 3 d modeling software is launched into said three-dimensional model n X-Y scheme piece of n >=1;
Step 3: sub-piece splicing; If n >=2 then need are stitched together the X-Y scheme piece according to border syntople in the said three-dimensional model; Again in the measure two dimensional graph block with the corresponding critical size of said three-dimensional model; And compare with the measurement result of said three-dimensional model, error need be controlled in 1 ‰;
Step 4: add flange, lap joint process surplus;
Saidly wait that based on satellite star catalogue face the two-dimentional drawing that coats the position makes up the step of drafting, mainly comprises:
Step a: on hardening the basis of composition in the satellite cabin, in conjunction with multilayer coat, the technical requirement of scrap (bridge), draw and obtain the outline that the satellite star catalogue waits to coat the position multi-layer graphical;
Step b: on the basis of the multilayer drawing that step a obtains, in conjunction with the pin layout of satellite star catalogue temperature control multilayer, the relevant position of profile diagram adds pin hole outside, forms the multi-layer graphical that comprises outline and pin hole;
Step c: on the multi-layer graphical basis that comprises outline and pin hole that step b obtains; Initial conditions according to instrument installation diagram, instrument profile atlas, waveguide installation diagram and cable installation diagram; Dodge the drafting in hole, the size of dodging the hole is actual 1.05 times of need dodge the object corresponding size on the satellite star catalogue;
Steps d: on the basis of the multilayer drawing that step c obtains, the actual conditions when broadcasting TV programs by satellite sampling, installation according to multilayer increase corresponding technology cutting opening.
2. the manufacturing approach of satellite star catalogue temperature control multilayer as claimed in claim 1 wherein, before said cutting step, utilizes kraft to carry out pre-cut to confirm pattern and to wait to coat the matching at position earlier.
3. the manufacturing approach of satellite star catalogue temperature control multilayer as claimed in claim 1; Wherein, Set up in the step 1 and wait that the three-dimensional model that coats the position is meant according to multilayer coating position actual conditions; The utilization 3 d modeling software carries out the curved surface modeling of temperature control multilayer, and the surface model of being set up intactly covers the coating position of multilayer.
4. the manufacturing approach of satellite star catalogue temperature control multilayer as claimed in claim 1, wherein, the 3 d modeling software described in the step 2 is Pro/Engineer, Solidworks, CATIA.
5. the manufacturing approach of satellite star catalogue temperature control multilayer as claimed in claim 1; Wherein, after interpolation flange in the step 4 and overlap joint are meant that the multilayer two-dimension figure forms, add flange and overlap joint surplus at the outline place; The flange amount is about 25mm, and amount of lap is about 30mm.
6. like the manufacturing approach of each described satellite star catalogue temperature control multilayer of claim 1-5, wherein, reality described in the step c need be dodged object and comprise instrument and waveguide.
7. like the manufacturing approach of each described satellite star catalogue temperature control multilayer of claim 1-5, wherein, the broadcast TV programs by satellite sampling, the actual conditions when installing of said multilayer is meant that multilayer delivers to the root that is installed on the plate of cabin from the instrument head cover, and head dimensions is greater than root.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110417167.4A CN102541109B (en) | 2011-12-14 | 2011-12-14 | Method for manufacturing satellite star surface temperature-control multilayer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110417167.4A CN102541109B (en) | 2011-12-14 | 2011-12-14 | Method for manufacturing satellite star surface temperature-control multilayer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102541109A true CN102541109A (en) | 2012-07-04 |
| CN102541109B CN102541109B (en) | 2014-08-13 |
Family
ID=46348193
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110417167.4A Active CN102541109B (en) | 2011-12-14 | 2011-12-14 | Method for manufacturing satellite star surface temperature-control multilayer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102541109B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617238A (en) * | 2013-11-26 | 2014-03-05 | 北京卫星环境工程研究所 | Digital manufacturing method for complex shape surface high-temperature three-dimensional protecting cover for satellite |
| CN109801039A (en) * | 2019-01-28 | 2019-05-24 | 北京卫星环境工程研究所 | The production processing time matrix method of spacecraft heat-control multilayer |
| CN110910488A (en) * | 2019-11-05 | 2020-03-24 | 北京工业大学 | Method and system for intelligent splicing and virtual restoration of scattered components of historic building |
| CN112015139A (en) * | 2020-09-01 | 2020-12-01 | 北京卫星环境工程研究所 | Method, device, equipment and storage medium for automatically manufacturing thermal control multilayer of spacecraft |
| CN112848363A (en) * | 2021-01-05 | 2021-05-28 | 北京卫星环境工程研究所 | Unfolding design method for spacecraft thermal control multilayer model |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0335302A (en) * | 1989-06-30 | 1991-02-15 | Osaka Kiko Co Ltd | Picture reproducing device for workpiece |
| CN1740932A (en) * | 2005-09-14 | 2006-03-01 | 山东大学 | Intelligent control system for digital control machine tool and control method thereof |
| CN101274577A (en) * | 2008-04-09 | 2008-10-01 | 徐鸿斌 | Digital simplified molding process for sculpture sample manuscript |
| CN101786200A (en) * | 2010-02-26 | 2010-07-28 | 华中科技大学 | Method for projection-type laser etching on free curved surface |
-
2011
- 2011-12-14 CN CN201110417167.4A patent/CN102541109B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0335302A (en) * | 1989-06-30 | 1991-02-15 | Osaka Kiko Co Ltd | Picture reproducing device for workpiece |
| CN1740932A (en) * | 2005-09-14 | 2006-03-01 | 山东大学 | Intelligent control system for digital control machine tool and control method thereof |
| CN101274577A (en) * | 2008-04-09 | 2008-10-01 | 徐鸿斌 | Digital simplified molding process for sculpture sample manuscript |
| CN101786200A (en) * | 2010-02-26 | 2010-07-28 | 华中科技大学 | Method for projection-type laser etching on free curved surface |
Non-Patent Citations (1)
| Title |
|---|
| 卢万强: "《数控加工技术》", 1 August 2011, 背景理工大学出版社 * |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617238A (en) * | 2013-11-26 | 2014-03-05 | 北京卫星环境工程研究所 | Digital manufacturing method for complex shape surface high-temperature three-dimensional protecting cover for satellite |
| CN103617238B (en) * | 2013-11-26 | 2016-08-17 | 北京卫星环境工程研究所 | Satellite complicated surface high-temperature three-dimensional protective cover digitized manufacturing system method |
| CN109801039A (en) * | 2019-01-28 | 2019-05-24 | 北京卫星环境工程研究所 | The production processing time matrix method of spacecraft heat-control multilayer |
| CN109801039B (en) * | 2019-01-28 | 2021-06-22 | 北京卫星环境工程研究所 | Statistical method for manufacturing working hours of spacecraft thermal control multilayer |
| CN110910488A (en) * | 2019-11-05 | 2020-03-24 | 北京工业大学 | Method and system for intelligent splicing and virtual restoration of scattered components of historic building |
| CN112015139A (en) * | 2020-09-01 | 2020-12-01 | 北京卫星环境工程研究所 | Method, device, equipment and storage medium for automatically manufacturing thermal control multilayer of spacecraft |
| CN112848363A (en) * | 2021-01-05 | 2021-05-28 | 北京卫星环境工程研究所 | Unfolding design method for spacecraft thermal control multilayer model |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102541109B (en) | 2014-08-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102541109A (en) | Method for manufacturing satellite star surface temperature-control multilayer | |
| CN107256005B (en) | BIM technology-based steel bar numerical control machining method and equipment | |
| US8204619B2 (en) | Building construction software and system | |
| US20070244590A1 (en) | Computer-aided method of obtaining a ply model of a composite component | |
| CN102890749A (en) | Method and system for generating three-dimensional operation instruction for ship section manufacture | |
| CN102470610A (en) | Cad data processing device and cad data processing method | |
| CN106774170B (en) | A kind of generation system of three-dimensional mechanical processing technique | |
| CN102510667A (en) | CNC (Computer Numerical Control) board splitting production method without NPTH (Non Plating Through Hole) hole positioning | |
| CN104217063A (en) | Simulation design method for rolling hole patterns of steel rail | |
| CN109815540B (en) | Datum line layout method for space curve component | |
| CN102591808B (en) | System and method for DCS (distributed control system) hardware configuration based on Excel | |
| CN103473216A (en) | Excel-based product process planning method | |
| JP2003141191A (en) | Integrated database cad system | |
| CN110175648A (en) | The information communication method of Noninvasive is carried out to equipment using artificial intelligence cloud computing | |
| CN109801039A (en) | The production processing time matrix method of spacecraft heat-control multilayer | |
| CN108256162A (en) | A kind of aluminium smallpox adjustment distribution design system and method, terminal, storage medium | |
| CN107430475A (en) | Object adjusts instrument and object adjustment programme | |
| US11712904B2 (en) | Fabric printing on nested patterns, and associated print systems and products thereof | |
| JP5525497B2 (en) | Plant work support apparatus and plant work support method | |
| CN110587227B (en) | Production method of printed steel plate screen | |
| US20180108185A1 (en) | Method and computer system for virtually displaying images on carton boxes | |
| KR20130028393A (en) | Automatic output method for duct manufacturing drawing | |
| KR102011060B1 (en) | Method for automating the process of using by macro script | |
| TWI677798B (en) | Working range visualization device and method | |
| JP2006301729A (en) | Picture preparation method and picture preparation device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |