CN101989263A - Method for realizing automatic data reconfiguration between isomeric systems - Google Patents

Method for realizing automatic data reconfiguration between isomeric systems Download PDF

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Publication number
CN101989263A
CN101989263A CN2009100556543A CN200910055654A CN101989263A CN 101989263 A CN101989263 A CN 101989263A CN 2009100556543 A CN2009100556543 A CN 2009100556543A CN 200910055654 A CN200910055654 A CN 200910055654A CN 101989263 A CN101989263 A CN 101989263A
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China
Prior art keywords
data
design data
design
importing
ecms
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CN2009100556543A
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Chinese (zh)
Inventor
何梅
朱靓
韩志芳
陈刚
曹卫梅
陈丽娜
张旭松
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Commercial Aircraft Corp of China Ltd
Shanghai Aircraft Design and Research Institute Commercial Aircraft Corporation of China Ltd
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Commercial Aircraft Corp of China Ltd
Shanghai Aircraft Design and Research Institute Commercial Aircraft Corporation of China Ltd
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Application filed by Commercial Aircraft Corp of China Ltd, Shanghai Aircraft Design and Research Institute Commercial Aircraft Corporation of China Ltd filed Critical Commercial Aircraft Corp of China Ltd
Priority to CN2009100556543A priority Critical patent/CN101989263A/en
Publication of CN101989263A publication Critical patent/CN101989263A/en
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Abstract

The invention discloses a method for realizing automatic data reconfiguration between a first system and a second system which are isomeric. The method comprises the following steps of: a, exporting design data from one first system; and b, importing the exported data into the second system, and automatically reconfiguring the design data in the importing process; wherein, the design data comprises symmetrical component data and/or standard component data. Accordingly, the design data can be imported into the second system, such as an engineering configuration management system, from the first system, such as an engineering data synergic design and check system, in due time, and data reconfiguration can be performed in the second system according to imported data.

Description

A kind of data automatic reconfiguration method between heterogeneous system
Technical field
The present invention relates to the digital management of information, relate in particular to a kind of data automatic reconfiguration method between heterogeneous system.
Background technology
In manufacturing and designing in the project of a lot of aircrafts, heterogeneous system each other between project data collaborative design and careful label systems (VPM) and the engineering configuration management system (ECMS), and, in original project data collaborative design and careful label system, product structure information does not embody the information of some standard components and symmetrical part.
Therefore, need a kind of new data automatic reconfiguration method that is used between heterogeneous system, solve above-mentioned technical matters.
Summary of the invention
In order to solve the aforementioned problems in the prior, the present invention proposes, and the degree of ripeness of data in VPM reaches after 100%, trigger automatically and ECMS between real-time synchronous transmission, based on the data that VPM sends, ECMS is reconstructed the data on it.
According to an aspect of the present invention, provide a kind of at isomery first system and second system between realize the method for data automatic reconfiguration, may further comprise the steps: a. is derived design data by one first system; B. described second system is arrived in the data importing of being derived, and in importing process, described design data is carried out automatic reconfiguration; Wherein, described design data comprises symmetrical event data and/or standard component data.
Wherein, also comprised before described step a: i. judges whether the degree of ripeness of described design data reaches 100%; Described step a also comprises: if-degree of ripeness of described design data reaches 100%, then described design data derived by described first system.
Wherein, described first system is project data collaborative design and careful label system, and described second system is an engineering configuration management system.
Wherein, before described step a, and after described step I, also comprise:, then described design data is examined label if the degree of ripeness of described design data reaches 100%; If described design data is by described careful label, then the person liable for described design data provides a notice, and it is used for notice described design data is sent to described second system; Described step a also comprises: based on the instruction of described person liable's input, described design data is derived by described first system.
Wherein, described step b comprises: if-the described design data that imports comprises symmetrical event data, then generates and corresponding second half the symmetrical event data of described symmetrical event data automatically.
Adopt method provided by the invention, can be in due course be second system of example with design data from being that first system of example imports to engineering configuration management system with project data collaborative design and careful label system, and in second system, carry out data reconstruction according to importing data.
Description of drawings
By reading below in conjunction with the description of accompanying drawing to indefiniteness embodiment, other purpose of the present invention, feature and advantage will become more obvious and outstanding.Wherein, same or analogous Reference numeral is represented same or analogous device or steps characteristic.
Fig. 1 is two heterogeneous system synoptic diagram according to a specific embodiment of the present invention;
Fig. 2 is the method flow diagram of realizing the data automatic reconfiguration between heterogeneous system according to a specific embodiment of the present invention.
Embodiment
Exemplified embodiment of the present invention will describe in detail in following content with reference to the accompanying drawings.Under the situation that does not depart from spirit of the present invention and scope, those skilled in the art can implement these or other improvement of the present invention and variation.
Two heterogeneous system synoptic diagram according to a specific embodiment of the present invention have been shown among Fig. 1, wherein, with project data collaborative design and careful label systems (VPM) an indefiniteness example as first system, and with the indefiniteness example of engineering configuration management system (ECMS) as second system.
Followingly the flow process of a kind of data automatic reconfiguration method between heterogeneous system provided by the invention is described in detail with reference to Fig. 2 and in conjunction with Fig. 1.This method starts from step S20.
Figure B2009100556543D0000031
The derivation of design data in the VPM system
Data that design data discussed herein is for example newly-built or change data.Step S20 preferably carries out with a fixing cycle repeatedly at one group of design data, also, judges periodically whether the degree of ripeness of one group of design data reaches 100%.If reach 100%, then, this group design data examines the label flow process for triggering one.
Examine the label flow process if this design data has been passed through this, then point out the related responsibility personnel to carry out data and derive operation.
According to this person liable's instruction, in step S21, this design data is derived from the VPM system.
Preferably, above-mentioned careful label flow process is a unit at each node on the product tree, and also, each node of product structure passes through flow process separately among the VPM.Correspondingly, the derivation of design data is a unit with a node equally.
Those skilled in the art understand, the above-mentioned mode by person liable's input instruction is the example that the present invention is used to realize the final a kind of indefiniteness that derives of data, in fact, after having passed through careful label flow process corresponding to one group of design data of a node, VPM system 1 can be automatically with its derivation.
At each node, the information that derives in the VPM system 1 comprises following, and these information are also referred to as design data in this article:
1. the attribute information of parts node object;
2. the attribute information of the patterns and drawings data objects such as 3D/2D related with parts;
3. the attribute information of objects such as technological document, Engineering Order (EO), Bill of Material (BOM);
4. the physical file of above-mentioned various pattern file, technological document etc.;
5. the related information between parts and the document;
6. the structural relation of parts node and subordinate's parts node.
According to a specific embodiment of the present invention, when from VPM system 1, deriving design data among the step S21, be that all information the physical file all are described with single xml file except that 4 in above-mentioned six kinds of information, and the physical file that this xml file is relevant with all is compressed in the compressed format files, for example the jar formatted file.
Figure B2009100556543D0000041
The importing of design data in ECMS 2
Typically, in the present invention, the design data that is derived by VPM system 1 will import to ECMS 2 by integrated interface interface (WEB interface or Command Line Interface).And,, the design data that derives is transferred to the network at ECMS 2 places by mobile memory medium if when the network physical at ECMS 2 places disconnects.
Wherein,, then generate automatically and corresponding second half the symmetrical event data of symmetrical event data that imports, thereby make completeization of product structure among the ECMS 2 if the design data that imports comprises symmetrical event data.
ECMS 2 when importing design data by VPM system 1 at every turn, and automatically generated data imports record, and every data importing record of generation comprises the information shown in the table 1:
Sequence number Property Name Describe Remarks
1 Data number Data number
2 Data name Data name
3 Versions of data Versions of data
4 Data Update user Data Update user
5 Passing time Passing time
6 Transmit mode Transmit mode
7 Remarks Remarks
Advantageously, the present invention also is provided for data are imported the graphic user interface that record is inquired about, and the user can inquire about the historical record of all data importings by the such graphic user interface of visit.
Design data is followed following rule in the importing at ECMS 2 places:
1) identification of product structure: precedingly address, it is unit with the parts node that VPM system 1 derives design data, simultaneously, gives related document information and component structural information.But, the component structural information in the design data that derives for reference only, ECMS 2 is as the criterion with the content of the engineering material inventory file of parts node and sets up product structure when importing design data.
2) correspondence of data object: the design data that VPM system 1 derives has comprised parts node object, geometric pattern design document and multiple other document object.ECMS 2 is when importing these objects, common parts node object importing is portion (Part) object in the product library, the parts node importing of standard component type is standard component thesaurus Part object, the importing of geometric pattern design document is the EPM file based on the Windchill platform, and other document importing is the WT file based on the Windchill platform.In addition, EPM file and WT file respectively with its associated Part object storage at product library or standard component thesaurus.
3) the version rule of correspondence: when the design data in the VPM system 1 imports to ECMS 2, handle according to the version scheme of ECMS 2 (being the Windchill platform), and the version identifier of use and VPM system 1 identical version sequence number.When not having object version to exist among the ECMS, original version is revised operation, thereby create an indicated release, when importing first version, a newly-built A version object in ECMS 2 then.When having had the object of indicated release among the ECMS 2, the at first little version of original version is carried out the operation that detects, checks in.
4) attributes object rule: the attribute of configuration data should be realized from VPM system 1 and Bill of Material (BOM) the mode that obtains simultaneously in integrated interface.The attribute of product component is as the criterion with the property value in the Bill of Material (BOM).All are decided to be necessary attribute and must provide in the data description XML of export file in ECMS 2, for attribute not necessarily in ECMS 2, if do not provide in the data description XML file of deriving, then ECMS 2 is with the default property value in the use attribute definition.
5) type of parts is assert rule: each the parts type in the VPM system 1 must clearly be specified all parts node types information all corresponding to the appointment parts type among the ECMS 2 in the data description XML file of VPM system 1 export.The division of parts type can be followed rule existing or that occur from now on.
6) the identification rule of Doctype: each Doctype in the VPM system 1 comprises the soft type and the segmentation type of EPM file and WT file all corresponding to the specified documents type among the ECMS 2.Must clearly specify all document objects in the data description XML file of VPM export is appointment segmentation types of EPM file or WT file.
Figure B2009100556543D0000051
Packet that VPM system 1 derives (design data that exists with certain form that promptly derives) and data description XML file specification
The packet that VPM system 1 derives is the compressed file that comprises data description XML and related physical file, for example jar form compressed file.The data description XML file that VPM system 1 derives comprises the description to following data object:
Parts node object: Part;
Component structural association: PartUse;
Parts document associations: ReletedDocument;
CAD document object: CADDocument;
Document object: Document.
The data sync inspection of VPM system 1 and ECMS 2
VPM system 1 is by customization, the data sync inventory of the numbering title of all documents (comprising the pattern file) under the output appointed product structure subtree, version, file size etc., ECMS 2 provides the Web interface to upload the data sync inventory, data to 2 of VPM systems 1, ECMS are carried out sync check, and generate the sync check report.
Though it is above main to be described to the data flow direction of ECMS system by the VPM system; but the present invention is not limited to this data flow direction; those skilled in the art can be under the prerequisite that does not break away from spirit of the present invention; according to explanation herein; apply the present invention to other data flow direction, and still fall into the protection domain that claims limited of enclosing.
More than the specific embodiment of the present invention is described.Need to prove that the present invention is not limited to above-mentioned specific implementations, those skilled in the art can make various modification or modification within the scope of the appended claims.

Claims (5)

1. method that realizes the data automatic reconfiguration between first system of isomery and second system may further comprise the steps:
A. design data is derived by one first system;
B. described second system is arrived in the data importing of being derived, and in importing process, described design data is carried out automatic reconfiguration;
Wherein, described design data comprises symmetrical event data and/or standard component data.
2. method according to claim 1 wherein, also comprised before described step a:
Whether the degree of ripeness of i. judging described design data reaches 100%;
Described step a also comprises:
If the degree of ripeness of-described design data reaches 100%, then described design data is derived by described first system.
3. method according to claim 1 and 2, wherein, described first system is project data collaborative design and careful label system, described second system is an engineering configuration management system.
4. method according to claim 2 wherein, before described step a, and also comprises after described step I:
If the degree of ripeness of described design data reaches 100%, then described design data is examined label;
If described design data is by described careful label, then the person liable for described design data provides a notice, and it is used for notice described design data is sent to described second system;
Described step a also comprises:
Based on the instruction of described person liable's input, described design data is derived by described first system.
5. method according to claim 1, wherein, described step b comprises:
If the described design data of-importing comprises symmetrical event data, then generate and corresponding second half the symmetrical event data of described symmetrical event data automatically.
CN2009100556543A 2009-07-30 2009-07-30 Method for realizing automatic data reconfiguration between isomeric systems Pending CN101989263A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104021002A (en) * 2014-06-19 2014-09-03 盐城工学院 Method for storing PDM system standard components
CN108416137A (en) * 2018-03-02 2018-08-17 沈阳飞机工业(集团)有限公司 It is divided and the method for tracking in a kind of aircraft manufacturing convenient for simplifying expression standard component

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104021002A (en) * 2014-06-19 2014-09-03 盐城工学院 Method for storing PDM system standard components
CN104021002B (en) * 2014-06-19 2017-03-29 盐城工学院 A kind of PDM system standards part storage method
CN108416137A (en) * 2018-03-02 2018-08-17 沈阳飞机工业(集团)有限公司 It is divided and the method for tracking in a kind of aircraft manufacturing convenient for simplifying expression standard component

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Application publication date: 20110323