CN101763066A - Management system of numerical control machining tool typical parts of complex parts of airplane and method - Google Patents
Management system of numerical control machining tool typical parts of complex parts of airplane and method Download PDFInfo
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Abstract
The invention provides a management system of numerical control machining tool typical parts of complex parts of an airplane and a method. The system comprises a semantics model defining module facing to the three-dimensional parameterization of the typical parts, a typical parts storeroom management module and a semantics model explaining module. The method comprises the processes of defining, memorizing and explaining the semantics model. The invention can effectively manage the parts type and the assembled parts type typical parts of the numerical control machining tool of the complex parts of the airplane, provides support to quickly design the numerical control machining tool, and can be popularized and applied to the design field of the other mechanical products.
Description
Technical field
The present invention relates to a kind of management system and method for numerical control machining tool typical parts.It not only can represent and manage complex parts or subassembly quasi-representative structural member in the numerical control machining tool design, also can be applied to simultaneously the standard component or the typical parts digital management in other Design of Mechanical Product field, belong to the standard component digital management field of Design of Mechanical Product.
Background technology
In aircraft development was produced, the cycle that technological equipment designs and makes was long, was to shorten frock design and manufacturing cycle, the various special-purpose typical parts of a large amount of uses in tool structure.In recent years, the widespread use in aircraft manufacturing along with CNC processing technology and equipment, the development of numerical control machining tool become the important content that the aircraft digital control processing is prepared, and need to use a large amount of standard component and typical parts in the numerical control machining tool design process equally.Current, the development of numerical control machining tool has realized being undertaken by three dimensional CAD system fully, comprise development special-purpose, have certain intelligentized specialized three dimensional CAD system or a general three dimensional CAD system.But no matter be general or special purpose three dimensional CAD system, whether possessing numerical control machining tool typical parts storehouse and management system thereof will directly influence the design efficiency of these CAD system.
About the digital management of typical parts, carried out years of researches both at home and abroad, many technology have successively been proposed, wherein the most representative is sequencing and parametric technology.
The sequencing technology is meant uses the generator program that each quasi-representative spare is worked out in secondary development language that CAD system provides or custom command, it is input as the physical dimension parameter of typical parts, the typical parts storehouse of being developed can be regarded the set of one group of tlv triple as, comprises typical parts type, such typical parts generator program, such typical parts parameter list.Use this technology, can develop typical parts storehouse with arbitrary shape and structure.But owing to need on stream for the special generator program of each quasi-representative spare establishment, so the development amount is big, to the expansion and the maintenance cost height in typical parts storehouse.
The parametric modeling function of directly utilizing CAD system to provide is provided parametric technology, develops and manages the parameterized model of each quasi-representative spare alternately; When calling, use typical parts physical dimension driving parameters model, generate the typical parts of required specification, wherein " model management " and " driving parameter " directly provided by the CAD system platform, and " parameter management " needs exploitation specially.Therefore, utilize this technology to carry out the exploitation of typical parts storehouse, difficulty and workload are all little.But owing to directly deposit the parameterized model of all kinds of typical parts in the typical parts storehouse, data volume is big; Simultaneously, be subjected to the restriction of the inherent constraint condition of geometric model, the shape facility of middle different size typical parts of the same type can not have big variation, and structure can not be too complicated.Therefore, this technology be used for that kind quantity is few more, shape and the not too complicated typical parts storehouse exploitation of structure.
Numerical control machining tool typical parts can be divided into part and subassembly two classes by its version, wherein subassembly quasi-representative spare can improve the design efficiency of numerical control machining tool more, so subassembly quasi-representative spare has occupied major part and structure is comparatively complicated, from the above, adopt sequencing and parametric technology all to be difficult to comparatively convenient and effective management that realizes for numerical control machining tool typical parts.
Summary of the invention
In order to solve traditional typical parts management system and method complexity, the not easy care and the effective problem of complex management part class and subassembly quasi-representative spare, realization is for effective management of numerical control machining tool typical parts, the invention provides a cover management system of numerical control machining tool typical parts and a method, realize management for complicated typical parts in the numerical control machining tool design.
The present invention seeks to be achieved through the following technical solutions:
Management system of numerical control machining tool typical parts of complex parts of airplane comprises:
Towards the three-dimensional parameterized semantic model definition module of typical parts: numerical control machining tool typical parts is carried out definition and analysis towards three-dimensional parameterized driving, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts.
The semantic model of described numerical control machining tool typical parts comprises parameter list, technical descriptioon, structure or three parts of shape, and wherein: parameter list comprises attribute list and parameter value table; Structure or shape comprise unit definition, contextual definition and edit definition; In described semantic model, can increase the out of Memory definition of typical parts, as positioning reference and typical parts synoptic diagram file etc.; And can define the set that the numerical control machining tool typical parts storehouse is all kinds of typical parts semantic models;
Semantic model explanation module: adopt unified explanation facility, will specify semantic model to form structurized three-dimensional modeling parameter, can be used as three dimensional CAD system input data through understanding at the numerical control machining tool typical parts semantic model;
Typical parts database management module: set up the tree-shaped Governance framework of Classification Management by type, realize warehouse-in, Classification Management and the query function of semantic model.
The semantic model BNF of described numerical control machining tool typical parts is defined as:
＜typical parts class 〉: :=＜class-mark〉＜type〉＜specification series〉＜attribute list〉＜the parameter value table〉＜definition of e unit〉＜edit definition〉＜contextual definition〉＜technical descriptioon 〉
＜class-mark 〉: :=CLA SS＜sequence number 〉:
＜type 〉: :=TYPE:＜navigation mark 〉
＜specification series 〉: :=SIZE:＜specification table〉[,＜specification table 〉]
.......
＜attribute list 〉: :=PARAM ETERS:＜attribute-name〉|＜navigation mark〉and,＜attribute-name〉|＜navigation mark 〉
＜parameter value table 〉: :=VALU ES:＜numerical value〉|＜specification〉and,＜numerical value〉|＜specification 〉
The definition of＜e unit 〉: :=PR IM IT IV ES:＜voxel〉|＜typical parts〉|＜complicated body 〉,＜voxel〉|＜typical parts〉|＜complicated body〉}
.......
＜edit definition 〉: :=ED IT:＜e unit sign〉(＜edit commands 〉,＜edit commands〉}),＜e unit sign〉(＜edit commands 〉,＜edit commands〉}) }
.......
＜contextual definition 〉: :=CON STRU CT:[＜typical parts sign 〉=]＜relational expression 〉
.......
＜illustrate: :=NO TE:＜text〉|＜text name 〉.
The numerical control machining tool typical parts of complex parts of airplane management method, step is as follows:
(1) semantic model definition: numerical control machining tool typical parts is carried out definition and analysis towards three-dimensional parameterized driving, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts.Its idiographic flow is as follows:
1. select the typical parts class-mark, this module provides the class-mark option;
2. select the typical parts type, select concrete typical parts type according to the typical parts class-mark;
3. select the typical parts specification series;
4. defined attribute, and add attribute list automatically, as be a plurality of attribute repeating steps 4.;
5. defined parameters value, and add the parameter value table automatically, as be the multiple parameter values repeating step 5.;
6. definition structure or shape unit, as be a plurality of unit definition repeating steps 6.;
7. combining unit definition information is carried out edit definition, as be a plurality of edit definition repeating steps 7.;
8. define the typical parts relation, can be sky;
9. define this module that finishes and generate typical parts semantic model data structure automatically.
(2) management in typical parts storehouse: adopt automatically and the mode that combines alternately, set up the tree-shaped Governance framework of Classification Management by type, realize the management in typical parts storehouse, operation such as comprise newly-built typical parts, inquiry, deletion and move; Simultaneously, realize storage and other corresponding operation of typical parts semantic model; Its idiographic flow is as follows:
1. the semantic model definition finishes, and behind the generative semantics model, enters the typical parts database management module;
2. the identification information according to typical parts in the semantic model carries out the coupling screening of typical parts storehouse, if there is similar typical parts type node, then be automatically positioned on this node, and prompting is set up the typical parts node with the typical parts identification information; Otherwise prompting is set up new typical parts type node and typical parts node automatically with the typical parts identification information;
3. after setting up the typical parts node automatically, the typical parts semantic model is then related with node automatically, and stores the relevant position in typical parts storehouse into;
4. after the typical parts node is set up, the rename that the user can the employing system provides, move, operation such as deletion carries out the typical parts node administration; Move and deletion action the corresponding memory location of the same execution of semantic model when carrying out mobile and deletion action;
5. as not adopting automatic semantic model warehouse-in, then the user can select typical parts to be subordinate to type node or newly-built type node and newly-built typical parts node alternately, all newly-built interactive operating systems are the initial title that is defaulted as the modification state with the typical parts identification information automatically all, and the user can make amendment and also can give tacit consent to;
(3) semantic model is explained: idiographic flow is as follows:
1. model is chosen, and according to the type of typical parts, extracts the semantic model of such typical parts from the numerical control machining tool typical parts storehouse;
2. model explanation comprises the definition of extracting each unit, and calculates the defined parameters of each unit; The extraction unit edit commands, and calculate each edit commands parameter; Extract each unit contextual definition; According to input specification, from the parameter value table of model, choose the corresponding parameters value, be three dimensional CAD system input data by the three-dimensional CAD data-interface at last.
Beneficial effect of the present invention: the present invention adopts such scheme, the present invention is directed to the structure and the features of shape of numerical control machining tool typical parts of complex parts of airplane, a kind of new effectively complex management part class or the modelling management method of subassembly quasi-representative spare are provided.Whole implement process is as follows: (1) carries out definition and analysis towards three-dimensional parameterized driving to numerical control machining tool typical parts, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts; (2) adopt automatically and the mode that combines alternately, set up the tree-shaped Governance framework of Classification Management by type, realize the management in typical parts storehouse, operation such as comprise newly-built typical parts, inquiry, deletion and move; Simultaneously, realize storage and other corresponding operation of typical parts semantic model; (3) adopt unified explanation facility, will specify semantic model to form structurized three-dimensional modeling parameter, can be used as three dimensional CAD system input data through understanding at the typical parts semantic model.System and method provided by the invention as subsystem application in " aircraft complex component digital control processing prepare (PrtRMP) system " in " frock generates subsystem fast " development, can provide effective typical parts storehouse to support for the design of aircraft complex component numerical control machining tool, especially the typical parts of subassembly type has improved the design efficiency and the quality of numerical control machining tool greatly.This system and method is towards three-dimensional parameterized driving, can embed professional three dimensional CAD system or three dimensional CAD system as the typical parts ADMINISTRATION SUBSYSTEM, except can be used for the typical parts management of aircraft complex component numerical control machining tool, management that also can wide popularization and application typical parts in other Design of Mechanical Product process, can effectively solve the deficiency of typical parts managerial ability in the existing three dimensional CAD system, reduce repeated workload to a greater extent, reduce deviser's working strength.
Description of drawings
Fig. 1 is the management system of numerical control machining tool typical parts of complex parts of airplane structural drawing;
Fig. 2 is towards the three-dimensional parameterized semantic model structure of typical parts;
Fig. 3 is towards the three-dimensional parameterized semantic model definition module realization flow of typical parts;
Fig. 4 is a typical parts database management module realization flow;
Fig. 5 is a semantic model explanation module realization flow.
Embodiment
Below in conjunction with accompanying drawing implementation process of the present invention is elaborated.
As shown in Figure 1, system of the present invention comprises three modules: towards the three-dimensional parameterized semantic model definition module of typical parts, typical parts database management module and semantic model explanation module.
Wherein towards the three-dimensional parameterized semantic model definition module of typical parts: be that numerical control machining tool typical parts is carried out definition and analysis towards three-dimensional parameterized driving, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts.
Make up the semantic model of the numerical control machining tool typical parts that generates, structure comprises parameter list, technical descriptioon, structure or three parts of shape as shown in Figure 2, and wherein, parameter list comprises attribute list and parameter value table; Structure or shape comprise unit definition, contextual definition and edit definition; In described semantic model, can increase the out of Memory definition of typical parts, as positioning reference and typical parts synoptic diagram file etc.; And can define the set that the numerical control machining tool typical parts storehouse is all kinds of typical parts semantic models.
The semantic model BNF that makes up the numerical control machining tool typical parts that generates is defined as follows:
＜typical parts class 〉: :=＜class-mark〉＜type〉＜specification series〉＜attribute list〉＜the parameter value table〉＜definition of e unit〉＜edit definition〉＜contextual definition〉＜technical descriptioon 〉
＜class-mark 〉: :=CLA SS＜sequence number 〉:
＜type 〉: :=TYPE:＜navigation mark 〉
＜specification series 〉: :=S IZE:＜specification table〉[,＜specification table 〉]
.......
＜attribute list 〉: :=PARAM ETERS:＜attribute-name〉|＜navigation mark〉and,＜attribute-name〉|＜navigation mark 〉
＜parameter value table 〉: :=VALU ES:＜numerical value〉|＜specification〉and,＜numerical value〉|＜specification 〉
The definition of＜e unit 〉: :=PR IM IT IV ES:＜voxel〉|＜typical parts〉|＜complicated body 〉,＜voxel〉|＜typical parts〉|＜complicated body〉}
.......
＜edit definition 〉: :=ED IT:＜e unit sign〉(＜edit commands 〉,＜edit commands〉}),＜e unit sign〉(＜edit commands 〉,＜edit commands〉}) }
.......
＜contextual definition 〉: :=CON STRU CT:[＜typical parts sign 〉=]＜relational expression 〉
.......
＜illustrate: :=NO TE:＜text〉|＜text name 〉.
Semantic model explanation module: adopt unified explanation facility, will specify semantic model to form structurized three-dimensional modeling parameter, can be used as three dimensional CAD system input data through understanding at the numerical control machining tool typical parts semantic model.
Typical parts database management module: set up the tree-shaped Governance framework of Classification Management by type, realize warehouse-in, Classification Management and the query function of semantic model.
The numerical control machining tool typical parts of complex parts of airplane management method, step is as follows:
(1) semantic model definition: numerical control machining tool typical parts is carried out definition and analysis towards three-dimensional parameterized driving, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts; Its idiographic flow is as shown in Figure 3:
1. select the typical parts class-mark, this module provides the class-mark option;
2. select the typical parts type, select concrete typical parts type according to the typical parts class-mark;
3. select the typical parts specification series;
4. defined attribute, and add attribute list automatically, as be a plurality of attribute repeating steps 4.;
5. defined parameters value, and add the parameter value table automatically, as be the multiple parameter values repeating step 5.;
6. definition structure or shape unit, as be a plurality of unit definition repeating steps 6.;
7. combining unit definition information is carried out edit definition, as be a plurality of edit definition repeating steps 7.;
8. define the typical parts relation, can be sky;
9. define this module that finishes and generate typical parts semantic model data structure automatically.
(2) management in typical parts storehouse: adopt automatically and the mode that combines alternately, set up the tree-shaped Governance framework of Classification Management by type, realize the management in typical parts storehouse, operation such as comprise newly-built typical parts, inquiry, deletion and move; Simultaneously, realize storage and other corresponding operation of typical parts semantic model; Its idiographic flow is as shown in Figure 4:
1. the semantic model definition finishes, and behind the generative semantics model, enters the typical parts database management module;
2. the identification information according to typical parts in the semantic model carries out the coupling screening of typical parts storehouse, if there is similar typical parts type node, then be automatically positioned on this node, and prompting is set up the typical parts node with the typical parts identification information; Otherwise prompting is set up new typical parts type node and typical parts node automatically with the typical parts identification information;
3. after setting up the typical parts node automatically, the typical parts semantic model is then related with node automatically, and stores the relevant position in typical parts storehouse into;
4. after the typical parts node is set up, the rename that the user can the employing system provides, move, operation such as deletion carries out the typical parts node administration; Move and deletion action the corresponding memory location of the same execution of semantic model when carrying out mobile and deletion action;
5. as not adopting automatic semantic model warehouse-in, then the user can select typical parts to be subordinate to type node or newly-built type node and newly-built typical parts node alternately, all newly-built interactive operating systems are the initial title that is defaulted as the modification state with the typical parts identification information automatically all, and the user can make amendment and also can give tacit consent to; (3) semantic model is explained: idiographic flow as shown in Figure 5:
1. model is chosen, and according to typical parts type (with " standard No. " definition), extracts the semantic model of such typical parts from the numerical control machining tool typical parts storehouse;
2. extract the definition of each unit, and calculate the defined parameters of each unit;
3. extraction unit edit commands, and calculate each edit commands parameter;
4. extract each unit contextual definition;
5. according to input specification, from the parameter value table of model, choose the corresponding parameters value
6. be three dimensional CAD system input data by the three-dimensional CAD data-interface.
Claims (3)
1. management system of numerical control machining tool typical parts of complex parts of airplane is characterized in that: comprising:
Towards the three-dimensional parameterized semantic model definition module of typical parts: numerical control machining tool typical parts is carried out definition and analysis towards three-dimensional parameterized driving, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts;
The semantic model of described numerical control machining tool typical parts comprises parameter list, technical descriptioon, structure or three parts of shape, and wherein, parameter list comprises attribute list and parameter value table; Structure or shape comprise unit definition, contextual definition and edit definition; In described semantic model, can increase the out of Memory definition of typical parts, as positioning reference and typical parts synoptic diagram file etc.; And can define the set that the numerical control machining tool typical parts storehouse is all kinds of typical parts semantic models;
Semantic model explanation module: adopt unified explanation facility, will specify semantic model to form structurized three-dimensional modeling parameter, can be used as three dimensional CAD system input data through understanding at the numerical control machining tool typical parts semantic model;
Typical parts database management module: set up the tree-shaped Governance framework of Classification Management by type, realize warehouse-in, Classification Management and the query function of semantic model.
2. management system of numerical control machining tool typical parts of complex parts of airplane according to claim 1 is characterized in that: the semantic model BNF of described numerical control machining tool typical parts is defined as:
＜typical parts class 〉: :=＜class-mark〉＜type〉＜specification series〉＜attribute list〉＜the parameter value table〉＜e unit
Definition〉＜edit definition〉＜contextual definition〉＜technical descriptioon 〉
＜class-mark 〉: :=CLA SS＜sequence number 〉:
＜type 〉: :=TYPE:＜navigation mark 〉
＜specification series 〉: :=SIZE:＜specification table〉[,＜specification table 〉]
.......
＜attribute list 〉: :=PARAM ETERS:＜attribute-name〉|＜navigation mark〉and,＜attribute-name〉|＜navigation mark 〉
＜parameter value table 〉: :=VALU ES:＜numerical value〉|＜specification〉and,＜numerical value〉|＜specification 〉
The definition of＜e unit 〉: :=PR IM IT IV ES:＜voxel〉|＜typical parts〉|＜complicated body 〉,＜voxel 〉
|＜typical parts〉|＜complicated body 〉
.......
＜edit definition 〉: :=ED IT:＜e unit sign〉(＜edit commands 〉,＜edit commands〉}),＜e
Unit's sign〉(＜edit commands 〉,＜edit commands〉}) }
.......
＜contextual definition 〉: :=CON STRU CT:[＜typical parts sign 〉=]＜relational expression 〉
.......
＜illustrate: :=NO TE:＜text〉|＜text name 〉.
3. numerical control machining tool typical parts of complex parts of airplane management method is characterized in that: under the step:
(1) semantic model definition: numerical control machining tool typical parts is carried out definition and analysis towards three-dimensional parameterized driving, employing standard BNF modelling represents that mode is described the three-dimensional parameterized driving defined parameters of typical parts, makes up the semantic model that forms numerical control machining tool typical parts; Its idiographic flow is as follows:
1. select the typical parts class-mark, this module provides the class-mark option;
2. select the typical parts type, select concrete typical parts type according to the typical parts class-mark;
3. select the typical parts specification series;
4. defined attribute, and add attribute list automatically, as be a plurality of attribute repeating steps 4.;
5. defined parameters value, and add the parameter value table automatically, as be the multiple parameter values repeating step 5.;
6. definition structure or shape unit, as be a plurality of unit definition repeating steps 6.;
7. combining unit definition information is carried out edit definition, as be a plurality of edit definition repeating steps 7.;
8. define the typical parts relation, can be sky;
9. define this module that finishes and generate typical parts semantic model data structure automatically;
(2) management in typical parts storehouse: adopt automatically and the mode that combines alternately, set up the tree-shaped Governance framework of Classification Management by type, realize the management in typical parts storehouse, operation such as comprise newly-built typical parts, inquiry, deletion and move; Simultaneously, realize storage and other corresponding operation of typical parts semantic model; Its idiographic flow is as follows:
1. the semantic model definition finishes, and behind the generative semantics model, enters the typical parts database management module;
2. the identification information according to typical parts in the semantic model carries out the coupling screening of typical parts storehouse, if there is similar typical parts type node, then be automatically positioned on this node, and prompting is set up the typical parts node with the typical parts identification information; Otherwise prompting is set up new typical parts type node and typical parts node automatically with the typical parts identification information;
3. after setting up the typical parts node automatically, the typical parts semantic model is then related with node automatically, and stores the relevant position in typical parts storehouse into;
4. after the typical parts node is set up, the rename that the user can the employing system provides, move, operation such as deletion carries out the typical parts node administration; Move and deletion action the corresponding memory location of the same execution of semantic model when carrying out mobile and deletion action;
5. as not adopting automatic semantic model warehouse-in, then the user can select typical parts to be subordinate to type node or newly-built type node and newly-built typical parts node alternately, all newly-built interactive operating systems are the initial title that is defaulted as the modification state with the typical parts identification information automatically all, and the user can make amendment and also can give tacit consent to;
(3) semantic model is explained: idiographic flow is as follows:
1. model is chosen, and according to the type of typical parts, extracts the semantic model of such typical parts from the numerical control machining tool typical parts storehouse;
2. model explanation comprises the definition of extracting each unit, and calculates the defined parameters of each unit; The extraction unit edit commands, and calculate each edit commands parameter; Extract each unit contextual definition; According to input specification, from the parameter value table of model, choose the corresponding parameters value, be three dimensional CAD system input data by the three-dimensional CAD data-interface at last.
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102456281A (en) * | 2010-10-25 | 2012-05-16 | 中国商用飞机有限责任公司 | Aircraft maintenance information processing method |
| CN102637221A (en) * | 2012-03-08 | 2012-08-15 | 沈阳飞机工业（集团）有限公司 | Multi-structure specification processing method of tool standard part |
| CN102637220A (en) * | 2012-03-08 | 2012-08-15 | 沈阳飞机工业（集团）有限公司 | Three-dimensional expansion semantic model of tool standard part |
| CN102982220A (en) * | 2012-12-25 | 2013-03-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Parametrization design method of first-level member of rib type part of airplane |
| CN103093031A (en) * | 2012-12-25 | 2013-05-08 | 中国航空工业集团公司沈阳飞机设计研究所 | Parametrization design method for aircraft skin wall panel part primary components |
| CN105095564A (en) * | 2015-06-18 | 2015-11-25 | 刘成学 | Data processing method and apparatus based on building information model |
| CN105988430A (en) * | 2015-01-30 | 2016-10-05 | 西门子（中国）有限公司 | Method and device for generating production process semantic model |
| CN107168964A (en) * | 2016-03-07 | 2017-09-15 | 济南兰光机电技术有限公司 | A kind of packaging detection result data storage method, querying method and system |
| CN107305362A (en) * | 2016-04-18 | 2017-10-31 | 秦皇岛烟草机械有限责任公司 | A kind of pipeline steel pipe system of processing based on three Dimensional CAD Design |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07182391A (en) * | 1993-12-24 | 1995-07-21 | Nissan Motor Co Ltd | Cad system for standard component data base |
-
2009
- 2009-12-15 CN CN 200910220760 patent/CN101763066B/en not_active Expired - Fee Related
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07182391A (en) * | 1993-12-24 | 1995-07-21 | Nissan Motor Co Ltd | Cad system for standard component data base |
Non-Patent Citations (4)
| Title |
|---|
| 张开富等: "《基于国产数据库的飞机典型结构件库设计与实现》", 《计算机辅助设计与图形学学报》 * |
| 朱春生: "《基于UG的飞机工装标准件库技术的研究与实现》", 《南京航空航天大学硕士学位论文》 * |
| 郑国磊等: "《飞机装配型架标准件模型化技术》", 《航空学报》 * |
| 钱玲玲: "《标准件库管理系统中的知识重用技术研究》", 《华中科技大学硕士学位论文》 * |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102456281A (en) * | 2010-10-25 | 2012-05-16 | 中国商用飞机有限责任公司 | Aircraft maintenance information processing method |
| CN102637221B (en) * | 2012-03-08 | 2014-02-26 | 沈阳飞机工业（集团）有限公司 | Multi-structure specification processing method of tool standard part |
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