CN106897515A - Component assembling method and device - Google Patents

Component assembling method and device Download PDF

Info

Publication number
CN106897515A
CN106897515A CN201710093277.7A CN201710093277A CN106897515A CN 106897515 A CN106897515 A CN 106897515A CN 201710093277 A CN201710093277 A CN 201710093277A CN 106897515 A CN106897515 A CN 106897515A
Authority
CN
China
Prior art keywords
deformation
assembly
attachment point
deformation part
spare parts
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.)
Pending
Application number
CN201710093277.7A
Other languages
Chinese (zh)
Inventor
吴幸
刘飞
肖旭
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Caxa Technology Co Ltd
Original Assignee
Caxa Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Caxa Technology Co Ltd filed Critical Caxa Technology Co Ltd
Priority to CN201710093277.7A priority Critical patent/CN106897515A/en
Publication of CN106897515A publication Critical patent/CN106897515A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Evolutionary Computation (AREA)
  • Computer Hardware Design (AREA)
  • General Engineering & Computer Science (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Computational Mathematics (AREA)
  • Automatic Assembly (AREA)

Abstract

The invention discloses a kind of component assembling method and device.Wherein, the method includes:Acquisition multiple is to be installed to replace the spare parts, wherein, each one size distortion parameter of correspondence that replaces the spare parts to be installed;The deformation part for replacing the spare parts to be installed is generated according to size distortion parameter, multiple deformation parts are obtained;The multiple deformation parts of traversal are assembled the deformation part for adhering to Point matching, obtain the assembly of multiple deformation parts, wherein, it is provided with attachment point in deformation part.The present invention solves the less efficient technical problem of component assembly.

Description

Component assembling method and device
Technical field
The present invention relates to Graphing of Engineering field, in particular to a kind of component assembling method and device.
Background technology
CAD (Computer Aided Design) software plays more and more important role in R & D of complex. A variety of CAD softwares are currently there are, almost Assembly design can be carried out per a CAD software.But to big number When being designed according to the Complex Assembly body of capacity, traditional manual assembly method efficiency is not substantially high.Than if any a kind of assembly Changing several parts therein will become another assembly, if allowing designer to replace by hand every time, it will expend Substantial amounts of time and efforts.
At present, there is two ways for most of CAD softwares design assembly:
(1) single part is assembled one by one by designer.
(2) by the way of risk management.This method is applied to part and changes little serial part.Such as one dress There are 10 parts in part, only one or two part needs to replace every time, it is only necessary to be hidden unwanted part.If The number of parts replaced is needed every time more, and this mode will seem not enough.And this mode substantially assembly is prior Install, it is impossible to embody the assembling process between each part.The category of Intelligent assembly is not belonging to by this way.
There is following a few point defects for the design present situation of assembly:
(1) parametrization and reusability of model be not high.The different part of only size similar to some shapes, designer Need to make substantial amounts of repeated labor to go to change accessory size, design cost is high, and the design cycle is long.
(2) intelligence degree of assembling is inadequate.At present, many enterprises are all to enter luggage to single part by designer Match somebody with somebody, workload is big, and operating process is very cumbersome.Therefore, the time that assembling process spends is a lot, and the cycle is long, is also easy to make assembling Error.
(3) need to repeat to draw engineering drawing and fill in BOM tables.Engineering drawing and BOM tables are manufactured and detection part as enterprise Foundation, the processing to part is most important.Devote a tremendous amount of time repetition every time to draw engineering drawing and fill out BOM tables, not only Efficiency is low and error-prone.
For the less efficient problem of above-mentioned component assembly, effective solution is not yet proposed at present.
The content of the invention
A kind of component assembling method and device are the embodiment of the invention provides, it is less efficient at least to solve component assembly Technical problem.
A kind of one side according to embodiments of the present invention, there is provided component assembling method, including:Obtain multiple to be assembled Part, wherein, each described one size distortion parameter of correspondence that replaces the spare parts to be installed;According to size distortion parameter generation The deformation part for replacing the spare parts to be installed, obtains multiple deformation parts;The multiple deformation parts of traversal will adhere to Point matching The deformation part is assembled, and obtains the assembly of multiple deformation parts, wherein, set in the deformation part State attachment point.
Further, the multiple deformation parts of the traversal are assembled the deformation part for adhering to Point matching, The assembly for obtaining multiple deformation parts includes:Multiple deformation parts are traveled through, is possible to carry out adhering to Point matching The deformation part is added in Assembly part set, it is impossible to adhere to the deformation part of Point matching added to not In Assembly part set;Traversal is described without the set that replaces the spare parts, by it is described without replace the spare parts the deformation part in gathering with it is described Deformation part in Assembly part set carries out attachment Point matching to obtain the assembly.
Further, the multiple deformation parts of traversal, are possible to the deformation part for carrying out adhering to Point matching Added in Assembly part set, it is impossible to which the deformation part for adhere to Point matching is added to without the set that replaces the spare parts Include:Order according to the multiple deformation part travels through multiple deformation parts successively, to deformation part each described Perform following steps:Whether Assembly part set described in judging is empty;In the case where the collection of Assembly part is combined into sky, Part will currently be deformed to be added in the Assembly part set;In the case where the Assembly part set is not for sky, The attachment point of the deformation part in Assembly part set described in traversal, judges whether attached with the current deformation part The attachment point of Point matching;Exist and the current deformation in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of the attachment Point matching of part, the current deformation part is added to the Assembly part set In;In the absence of the attachment point with the current deformation part in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of matching, by the current deformation part added to described without in the set that replaces the spare parts.
Further, without the set that replaces the spare parts described in the traversal, by the deformation part without in the set that replaces the spare parts Carry out attachment Point matching with the deformation part in the Assembly part set is included with obtaining the assembly:It is described without In the case of set replace the spare parts not for sky, according to it is described without the order for deforming part in the set that replaces the spare parts travel through successively it is described not Deformation part in Assembly part set, following steps are performed to deforming part each described:Assembly part collection described in traversal The attachment point of the deformation part in conjunction, judges whether the attachment point with the attachment Point matching of currently deformation part;Described There is the attachment with the attachment Point matching of the current deformation part in the attachment point of the deformation part in Assembly part set In the case of point, by the current deformation part from described without being deleted in the set that replaces the spare parts, and by the current deformation part Added in the Assembly part set.
Further, it is described obtain it is multiple it is to be installed replace the spare parts before, methods described also includes:Parts library is set up, wherein, The parts library includes:Multiple standardized element models, attachment point is provided with the standardized element model;Each described standard The corresponding engineering drawing of part model;The corresponding parameter list of each described standardized element model, the parameter list includes the mark The size distortion parameter of quasi- part model, the size distortion parameter is used for the size for indicating to change the standardized element model.
Further, the deformation part for adhering to Point matching is entered into luggage in the multiple deformation parts of the traversal Match somebody with somebody, obtain after the assembly of multiple deformation parts, methods described also includes:According to the correspondence that replaces the spare parts to be installed each described The size distortion parameter update the engineering drawing for replacing the spare parts to be installed and BOM tables.
Another aspect according to embodiments of the present invention, additionally provides a kind of component assembling apparatus, including:Acquiring unit, uses In obtaining, multiple is to be installed to replace the spare parts, wherein, each described one size distortion parameter of correspondence that replaces the spare parts to be installed;Generation unit, uses In the deformation part for replacing the spare parts to be installed is generated according to the size distortion parameter, multiple deformation parts are obtained;Assembling Unit, is assembled the deformation part for adhering to Point matching for traveling through multiple deformation parts, is obtained described in multiple Deform the assembly of part, wherein, it is provided with the attachment point in the deformation part.
Further, the assembly unit includes:First matching module, for traveling through multiple deformation parts, by energy The deformation part for enough carrying out adhering to Point matching is added in Assembly part set, it is impossible to adhere to the institute of Point matching Deformation part is stated to be added to without in the set that replaces the spare parts;Second matching module, it is described without the set that replaces the spare parts for traveling through, by institute State without the deformation part in deformation part and the Assembly part set in the set that replaces the spare parts adhere to Point matching with Obtain the assembly.
Further, first matching module includes:First spider module, for according to the multiple deformation part Order travels through multiple deformation parts successively, to deforming the step shown in the part following submodule of execution each described:First Judging submodule, for judging whether the Assembly part set is empty;First addition submodule, for having been assembled described In the case that part collection is combined into sky, will currently deform part and be added in the Assembly part set;Second judging submodule, In the case of in the Assembly part set not for sky, the attached of part is deformed in Assembly part set described in traversal A little, judge whether the attachment point with the attachment Point matching of the current deformation part;Second addition submodule, for Exist in the attachment point of the deformation part in the Assembly part set and the attachment Point matching of the current deformation part In the case of attachment point, the current deformation part is added in the Assembly part set;3rd addition submodule, uses In the absence of the attachment point with the current deformation part in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of matching, by the current deformation part added to described without in the set that replaces the spare parts.
Further, second matching module includes:Second spider module, for gathering not without replacing the spare parts described In the case of for sky, traveled through successively according to the order without deformation part in the set that replaces the spare parts described without the set that replaces the spare parts In deformation part, perform step shown in following submodule to deforming part each described:3rd judging submodule, for time The attachment point of the deformation part gone through in the Assembly part set, judges whether and the attachment point for currently deforming part The attachment point matched somebody with somebody;4th addition submodule, for existing in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of the attachment Point matching of the current deformation part, will the current part that deforms from described unassembled Deleted in part set, and the current deformation part is added in the Assembly part set.
In embodiments of the present invention, there is the to be installed of correspondingly-sized deformation parameter and replace the spare parts in acquisition, then each is to be assembled Part assigns corresponding deformation parameter, generation and the corresponding multiple deformation parts that replace the spare parts to be installed, then multiple by traveling through again Deformation part, according to the attachment point for being set on deformation part in advance, the deformation part that there is matching relationship to attachment point is carried out Assembling, obtains the assembly being made up of multiple deformation part.Using the present invention, treat Assembly part and obtained by size distortion parameter To deformation part, the matching further according to attachment point is assembled to deformation part, can automatically complete part from being generated to dress The process matched somebody with somebody, and accelerate the process of assembling, particularly big to some data capacities, the assembly of part high recycling rate, energy Design efficiency is enough significantly improved, the less efficient technical problem of component assembly is solved.
Brief description of the drawings
Accompanying drawing described herein is used for providing a further understanding of the present invention, constitutes the part of the application, this hair Bright schematic description and description does not constitute inappropriate limitation of the present invention for explaining the present invention.In the accompanying drawings:
Fig. 1 is the flow chart of component assembling method according to embodiments of the present invention;
Fig. 2 is the flow chart one of a kind of optional preassembled method according to embodiments of the present invention;
Fig. 3 is the flow chart one of the method for a kind of optional follow-up assembling according to embodiments of the present invention;
Fig. 4 is the schematic diagram of a kind of optional parts library according to embodiments of the present invention;
Fig. 5 is the flow chart of the method for a kind of optional structure parts library according to embodiments of the present invention;
Fig. 6 is the flow chart of a kind of optional Automated assembly according to embodiments of the present invention;
Fig. 7 is the flowchart 2 of a kind of optional prepackage method of completing the square according to embodiments of the present invention;
Fig. 8 is the flowchart 2 of a kind of optional follow-up assembly method according to embodiments of the present invention;
Fig. 9 is the flow chart of a kind of optional automation component assembling method according to embodiments of the present invention;
Figure 10 is a kind of schematic diagram of component assembling apparatus according to embodiments of the present invention.
Specific embodiment
In order that those skilled in the art more fully understand the present invention program, below in conjunction with the embodiment of the present invention Accompanying drawing, is clearly and completely described to the technical scheme in the embodiment of the present invention, it is clear that described embodiment is only The embodiment of a part of the invention, rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill people The every other embodiment that member is obtained under the premise of creative work is not made, should all belong to the model of present invention protection Enclose.
It should be noted that term " first ", " in description and claims of this specification and above-mentioned accompanying drawing Two " it is etc. for distinguishing similar object, without for describing specific order or precedence.It should be appreciated that so using Data can exchange in the appropriate case, so as to embodiments of the invention described herein can with except illustrating herein or Order beyond those of description is implemented.Additionally, term " comprising " and " having " and their any deformation, it is intended that cover Lid is non-exclusive to be included, for example, the process, method, system, product or the equipment that contain series of steps or unit are not necessarily limited to Those steps or unit clearly listed, but may include not list clearly or for these processes, method, product Or other intrinsic steps of equipment or unit.
First, the part noun or term for occurring during being described to the embodiment of the present application are applied to following solution Release:
CAD:English full name is Computer Aided Design, and Chinese is CAD, refers to utilize Computer and its graphics device help designer to be designed work.
CAD diagram paper:Refer to the CAD using AutoCAD softwares or CAXA softwares, it is total according to engineering project The pattern of the making such as body layout, the outer shape of building, internal arrangement, structure construction, material way and equipment, construction.
According to embodiments of the present invention, there is provided a kind of component assembling method embodiment, it is necessary to explanation, in the stream of accompanying drawing The step of journey is illustrated can perform in the such as one group computer system of computer executable instructions, and, although in stream Logical order is shown in journey figure, but in some cases, can be with shown or described different from order execution herein The step of.
Fig. 1 is the flow chart of component assembling method according to embodiments of the present invention, as shown in figure 1, the method is including as follows Step:
Step S102, acquisition multiple is to be installed to replace the spare parts, wherein, each one size distortion parameter of correspondence that replaces the spare parts to be installed;
Step S104, the deformation part for replacing the spare parts to be installed is generated according to size distortion parameter, obtains multiple deformation parts;
Step S106, the multiple deformation parts of traversal are assembled the deformation part for adhering to Point matching, obtain multiple deformations The assembly of part, wherein, it is provided with attachment point in deformation part.
According to above-mentioned steps, there is the to be installed of correspondingly-sized deformation parameter and replace the spare parts in acquisition, then each to be installed is replaced the spare parts Corresponding deformation parameter, generation and the corresponding multiple deformation parts that replace the spare parts to be installed are assigned, then again by traveling through multiple deformations Part, according to the attachment point for being set on deformation part in advance, the deformation part that there is matching relationship to attachment point is assembled, Obtain the assembly being made up of multiple deformation part.Using the present invention, treat Assembly part and become by size distortion parameter Shape part, the matching further according to attachment point is assembled to deformation part, can automatically complete part from being generated to assembling Process, and accelerate the speed of assembling, particularly big to some data capacities, the assembly of part high recycling rate, Neng Gouming It is aobvious to improve design efficiency, solve the less efficient technical problem of component assembly.
In the scheme that step S102 is provided, to be installed replacing the spare parts can be drawn by CAD software, need to be assembled Part model, for example, to be installed replacing the spare parts can be the bolt part drawn by CAD software, or nut part.Size distortion Parameter can be with each corresponding, parameter for changing accessory size to be assembled that replaces the spare parts to be installed, can be by size distortion Parameter changes the size for replacing the spare parts to be installed, for example, can by the length of screw rod in size distortion parameter change bolt part, The thickness of screw rod, or by the internal diameter of size distortion parameter change nut part.
Alternatively, the embodiment of the present invention can set up parts library, wherein, can record multiple soft by CAD in parts library To be installed the replacing the spare parts and each corresponding size distortion parameter that replaces the spare parts to be installed of part drafting.After parts library is set up, the present invention Embodiment can treat Assembly part and be stored by parts library, facilitate the use the parts library and quickly and easily find institute The to be installed of acquisition is needed to replace the spare parts.
Above-mentioned steps S102, by directly being searched from parts library and can obtain multiple to be installed replace the spare parts and each is treated The size distortion parameter of Assembly part.
Step S104 provide scheme in, deformation part be treat Assembly part assign correspondingly-sized deformation parameter after by According to the part obtained by new size, for example, it is to be installed replace the spare parts be bolt in the case of, accurately limited by size distortion parameter The parameter such as the length of screw rod in bolt and the radius of screw rod is determined, after the deformation corresponding with the length and radius can be obtained Bolt part.
In the scheme that step S106 is provided, attachment point can be used to indicate that the relation between deformation part, if deformation zero Attachment Point matching between part, the then deformation part for adhering to Point matching is combined on the position of attachment point, such that it is able to using attached The assembling a little completed to deforming part, assembly is obtained.Wherein, assembly can be by multiple parts and between constraint The entirety that composition of relations is formed.In practical application scene, can set corresponding in the block position of each deformation part in advance Attachment point, by traveling through the attachment points on multiple deformation parts, the deformation part for adhering to Point matching is assembled, become The assembly of shape part.
Alternatively, the block position on each deformation part sets one or more attachment point, and each attachment point can With the unique title of correspondence.The title of the attachment point of the multiple deformation parts with restriction relation can be with identical, the multiple changes of traversal The attachment point of shape part, title identical attachment point is matched, to realize being assembled multiple deformation part.
Used as a kind of alternatively embodiment, the multiple deformation parts of traversal are assembled the deformation part for adhering to Point matching, The assembly for obtaining multiple deformation parts can include:The multiple deformation parts of traversal, are possible to the deformation for carrying out adhering to Point matching Part is added in Assembly part set, it is impossible to which the deformation part for adhere to Point matching is added to without the set that replaces the spare parts In;Traversal is without the set that replaces the spare parts, the deformation zero in deformation part and Assembly part set in gathering without replacing the spare parts Part carries out attachment Point matching to obtain assembly.
Specifically, multiple assemblies for deforming parts are obtained assemble the deformation part for adhering to Point matching, can be with By traveling through multiple deformation parts, the deformation part that will adhere to Point matching is added in Assembly part set, by attachment point not During the deformation part of matching is added to without replacing the spare parts, the pre-assembled to deforming part is completed;Then travel through without the collection that replaces the spare parts Deformation part in conjunction, will be carried out attached without the deformation part in deformation part and the Assembly part set in the set that replaces the spare parts Point matching, the follow-up assembling to deforming part is completed, so as to obtain being assembled according to attachment Point matching, assembly is obtained. Using the present invention, by pre-assembled and follow-up assembling, the deformation part under different situations is assembled respectively, it is possible to achieve right Deform the Automated assembly of part, accelerate the speed of assembling, improve the speed of assembling.
Fig. 2 is the flow chart one of a kind of optional preassembled method according to embodiments of the present invention, as shown in Fig. 2 in advance Assembling process can be described as:
After multiple deformation parts are traveled through successively according to the order of multiple deformation part, each deformation part is performed as follows Step:
Step S202, judges whether Assembly part set is empty;
Step S204, in the case where Assembly part collection is combined into sky, will currently deform part added to Assembly part In set;
Step S206, in the case where Assembly part set is not for sky, the deformation zero in traversal Assembly part set The attachment point of part, judges whether the attachment point with the attachment Point matching of currently deformation part;
Step S208, exists attached with current deformation part in the attachment point of the deformation part in Assembly part set In the case of the attachment point of Point matching, will currently deform part and be added in Assembly part set;
Step S210, does not exist and current deformation part in the attachment point of the deformation part in Assembly part set In the case of adhering to the attachment point of Point matching, current deformation part is added to without in the set that replaces the spare parts.
By above-mentioned steps, it is being possible to carry out the deformation part for adhering to Point matching added to Assembly part set, will The deformation part of Point matching can not be carried out adhering to added to the Cheng Qian that crosses without the set that replaces the spare parts, first according to multiple deformation part Put in order multiple deformation parts that travel through successively, then judge whether Assembly part set is empty, if Assembly part collection is combined into , then be added to the deformation part of current traversal in the set of Assembly part by sky, if Assembly part set is not sky, also Need to detect whether the attachment point of the deformation part in Assembly part set matches with the deformation part of current traversal, assemble In the case that the attachment point of the deformation part in part set does not exist the attachment Point matching with current deformation part, by current time The deformation part gone through be added to without replace the spare parts set in, in Assembly part set deformation part attachment point with it is current In the case of deforming the attachment Point matching of part, in the deformation part addition Assembly part set that will currently travel through, so that can It is added in Assembly part set with the deformation part that will adhere to Point matching exactly, by the unmatched deformation part of attachment point Added in without the set that replaces the spare parts, the Accurate classification to deforming part, and the deformation part for completing attachment Point matching are realized Pre-assembled process, can also as procedure described above complete Automated assembly.
Fig. 3 is the flow chart one of the method for a kind of optional follow-up assembling according to embodiments of the present invention, as shown in figure 3, Deformation part is stored in without set and the Assembly part set of replacing the spare parts, wherein, Assembly part set includes having filled The deformation part matched somebody with somebody, without replacing the spare parts, set includes knocked-down deformation part, be not empty feelings without the set that replaces the spare parts Under condition, traveled through successively without the deformation part in the set that replaces the spare parts according to without the order for deforming part in the set that replaces the spare parts, it is right Each deformation part performs following steps:
Step S302, the attachment point of the deformation part in traversal Assembly part set, judges whether and currently becomes The attachment point of the attachment Point matching of shape part;
Step S304, exists attached with current deformation part in the attachment point of the deformation part in Assembly part set In the case of the attachment point of Point matching, will currently deform deletion in part never Assembly part set, and will currently deform zero Part is added in Assembly part set.
In above-mentioned steps, first judge whether include knocked-down deformation part without in the set that replaces the spare parts, if unassembled There is knocked-down deformation part in part set, then traveled through successively according to the order without the deformation part in the set that replaces the spare parts Without the deformation part in the set that replaces the spare parts, step S302 is then performed, by traveling through the deformation zero in Assembly part set The attachment point of part, in the attachment point and Assembly part set without the deformation part in the set that replaces the spare parts of the current traversal of judgement The attachment point of deformation part whether match, if the match is successful, perform step S304, will without the set that replaces the spare parts in it is current Deleted in the never Assembly part set of deformation part, and the deformation part is added in Assembly part set;If matching is lost Lose, then skip this and continue to travel through other deformation parts without in replacing the spare parts without the deformation part in the set that replaces the spare parts.In warp Cross after traveling through without being not still sky in the set that replaces the spare parts, also exist as in Assembly part set and deform part, then re-execute Step S302, until being sky without the set that replaces the spare parts, completes to without the assembling for deforming part in the set that replaces the spare parts, being assembled Body.By above-mentioned follow-up assemble flow, it is possible to achieve to being carried out again by still knocked-down deformation part after pre-assembled process Assembling, to cause that all of deformation part can complete assembling, obtains assembly.
As an optional embodiment, obtain it is multiple it is to be installed replace the spare parts before, the embodiment can also include:Set up Parts library, wherein, parts library includes:Multiple standardized element models, attachment point is provided with standardized element model;Each standard The corresponding engineering drawing of part model;Each corresponding parameter list of standardized element model, parameter list includes standardized element model Size distortion parameter, size distortion parameter is used for the size for indicating to change standardized element model.
Specifically, before to be installed replacing the spare parts is obtained, the parts library of storage parts information to be assembled is set up, is wrapped in database Multiple standardized element models are included, each corresponding engineering drawing of standardized element model, and each corresponding ginseng of standardized element model Number table, wherein, attachment point is provided with each standardized element model, each corresponding parameter list of standardized element model includes The size distortion parameter of standardized element model.Using the above embodiment of the present invention, replaced the spare parts by pre-building that storage is to be installed Database, be easy to obtain it is to be installed replace the spare parts, can accelerate to obtain the speed for replacing the spare parts to be installed.
As an optional embodiment, the deformation part for adhering to Point matching is entered into luggage in the multiple deformation parts of traversal Match somebody with somebody, obtain after the assembly of multiple deformation parts, the embodiment can also include:According to each corresponding chi that replaces the spare parts to be installed Very little deformation parameter updates the engineering drawing for replacing the spare parts to be installed and BOM tables.
It should be noted that engineering drawing is a kind of two-dimensional diagram or picture the architectural drawing, structure chart, the machinery system that describe Figure, electric installation drawing and pipeline drawing.BOM tables, full name is Bill of Material, and Chinese is BOM, is meter The product structure data file that calculation machine can be recognized.
Alternatively, engineering drawing and BOM tables be by the corresponding size distortion parameter determination that replaces the spare parts to be installed, according to incoming size Deformation parameter driving is to be installed to replace the spare parts, and generates the new engineering drawing for replacing the spare parts to be installed and BOM tables.Using the above embodiment of the present invention Renewal project figure and BOM tables, without repeating to draw engineering drawing, without repeating to fill in BOM tables, so as to reduce the work of designer Measure, accelerate to draw engineering drawing, fill in the speed of BOM tables, and increase the accuracy drawn engineering drawing and fill in BOM tables, it is real Now generation engineering drawing and the automation of BOM tables, can significantly improve design efficiency.
Present invention also offers a kind of preferred embodiment, the preferred embodiment provides a kind of intelligence dress in knowledge based storehouse Method of completing the square, the method can include three below part:
1. set up and indicate storehouse or parts library.
2. Automated assembly.
3. engineering drawing and BOM tables are generated.
Fig. 4 is the schematic diagram of a kind of optional parts library according to embodiments of the present invention, as shown in figure 4, the parts library can To include:Multiple standardized element models 41, the corresponding engineering drawing 43 of each standardized element, and the corresponding ginseng of each standardized element Number table 45.
Fig. 5 is the flow chart of the method for a kind of optional structure parts library according to embodiments of the present invention, as shown in figure 5, The method comprises the following steps:
Step S502, draws standardized element model.
As an optional embodiment, all to be installed under assembly is replaced the spare parts, draw a set of standardized element model.
Optionally, standardized element model can be three-dimensional part model.
Step S504, adds the size distortion parameter of standardized element model.
An optional embodiment, by the quantitative information variable design in standardized element model, by the ginseng of standardized element model Number is converted to the size distortion parameter that can be adjusted, and then assigns different parameter values to the size distortion parameter again, so that it may To obtain the series of transformations part of different size and shape.
Step S506, sets up size distortion parameter list.
In an optional embodiment, a size distortion parameter list is added to each standardized element model, in parameter The corresponding multiple size distortion parameters of each standardized element model are enumerated in table.
Step S508, is each deformation part addition attachment point.
It should be noted that attachment point is used to represent the relation between deformation part, if the attachment point between deformation part Matching, the then deformation part for adhering to Point matching is combined on the position of attachment point, such that it is able to be completed to deformation using attachment point The assembling of part, obtains assembly.
Step S510, draws the corresponding engineering drawing of standardized element model.
In above-mentioned steps, by setting up standardized element model, the corresponding engineering drawing of standardized element model, and standard zero The corresponding parameter list of part model, can obtain the accurate description parts library for replacing the spare parts to be installed.
Fig. 6 is the flow chart of a kind of optional Automated assembly according to embodiments of the present invention, as shown in fig. 6, the method Comprise the following steps:
Step S602, imports size distortion parameter list.
It should be noted that in size distortion parameter list should comprising it is all it is to be installed replace the spare parts, and each to be installed replaces the spare parts Size distortion parameter.
Step S604, travels through size distortion parameter list.
Alternatively, size distortion parameter list is traveled through, by the standardized element model for replacing the spare parts to be installed by size distortion parameter, Obtain the deformation part for replacing the spare parts to be installed.
Alternatively, traversing operation circulation carry out, until in size distortion parameter list overall dimension deformation parameter all exist it is right The deformation part for replacing the spare parts to be installed answered.
Step S606, the attachment point of traversal deformation part.
Alternatively, while deformation part is generated by step S604, the attachment point on traversal deformation part judges to become Whether the attachment point between shape part matches, and the part for adhering to Point matching is assembled if Point matching is adhered to, and be put into In Assembly part set, son assembling is completed.
Step S608, completes general assembly.
As an optional embodiment, the attachment point that each height is loaded onto is traveled through, complete general assembly.
It should be noted that general assembly can be divided into two parts, respectively pre-assembled and follow-up assembling, can complete Preassembled deformation part is put into Assembly part set, cannot be completed preassembled deformation part and is put into unassembled zero In part set.In follow-up assembling process, Assembly part set is once traveled through and without the set that replaces the spare parts, carry out attachment point With completion general assembly.
Fig. 7 is the flowchart 2 of a kind of optional prepackage method of completing the square according to embodiments of the present invention, as shown in fig. 7, the party Method comprises the following steps:
Step S702, the multiple deformation parts of traversal.
Step S704, judges whether Assembly part set is empty.
Alternatively, if Assembly part collection is combined into sky, step S706 is performed;If Assembly part set is not sky, Perform step S708.
Step S706, deformation part is added in Assembly part set.
Step S708, the attachment point of the deformation part in traversal Assembly part set, judges whether and currently becomes Shape part adheres to the attachment point of Point matching.
Alternatively, if in the presence of the attachment point for adhering to Point matching with current deformation part, performing step S710;If not existing Attachment point with current deformation part adheres to Point matching, then perform step S712.
Step S710, part completes assembling, in adding it to Assembly part set.
Alternatively, if the attachment point of the deformation part in Assembly part set is present and current deformation part attachment point The attachment point matched somebody with somebody, then will currently deform part added in Assembly part set, complete with part in Assembly part set Into pre-assembled.
Step S712, part does not complete assembling, adds it to without in the set that replaces the spare parts.
Alternatively, if the attachment point of the deformation part in Assembly part set does not exist and current deformation part attachment point , then be added to current deformation part without in the set that replaces the spare parts by the attachment point of matching.
Fig. 8 is the flowchart 2 of a kind of optional follow-up assembly method according to embodiments of the present invention, as shown in figure 8, should Method comprises the following steps:
Step S802, judges whether without the set that replaces the spare parts be empty.
If being sky without the set that replaces the spare parts, assembling is completed;If set is not sky without replacing the spare parts, step is performed S804。
Step S804, traversal the set of Assembly part in deformation part attachment point, judge whether with currently The attachment point of the attachment Point matching of deformation part.
It should be noted that the set of Assembly part is traveled through in step S804, can be by step S8041 and step S8043 is realized, comprised the following steps that:
, it is necessary to being numbered without the deformation part in the set that replaces the spare parts before execution step S8041.
Alternatively, by without the deformation part in the set that replaces the spare parts, put in order according to deformation part, successively according to 1, The order of the 2nd, 3 ... N, is numbered to each deformation part.
Step S8041, deformation part is extracted according to number order, while setting a variable i, initial value is 0.
Step S8042, judges whether the numbering of extracted deformation part is more than the value of variable i.If being more than, perform Step S8043, otherwise returns and performs step S802.
Step S8043, judges to whether there is and the current deformation part attachment point for being extracted in Assembly part set The part matched somebody with somebody.If in the presence of execution step S806;If not existing, return to step S8042 after adding 1 to variable i.
Step S806, deletes, and will currently deform zero in the current deformation part never Assembly part set that will be extracted Part is added in Assembly part set.The return to step S802 after step S806 is performed.
Alternatively, the generation of engineering drawing and BOM tables is according to incoming size distortion driving parameter standardized element model Corresponding engineering drawing and BOM tables, so as to generate the corresponding engineering drawing of new model and BOM tables.
Fig. 9 is the flow chart of a kind of optional automation component assembling method according to embodiments of the present invention, such as Fig. 6 institutes Show, the method comprises the following steps:
Step S902, reads the name and parameter for replacing the spare parts to be installed.
Step S904, searches corresponding part in parts library.
Alternatively, according to the name and parameter for replacing the spare parts to be installed, corresponding standardized element model is searched in parts library With size distortion parameter.
Step S906, obtains deforming part.
Standardized element model and size distortion parameter according to being searched from database obtain deforming part.
Step S908, renewal project figure.
Step S910, adheres to Point matching, carries out pre-assembled.
Whether step S912, detection pre-assembled completes.
If pre-assembled is completed, step S914 is performed;If pre-assembled is not completed, step S902 is performed.
Step S914, adheres to Point matching, is subsequently assembled.
Whether step S916, detection son assembling completes.
If son assembling is completed, step S918 is performed;If son assembling is not completed, step S914 is performed.
Step S918, completes general assembly.
Step S920, generates engineering drawing and BOM tables.
Using the above embodiment of the present invention, the reusability of part model can be improved, be generated according to size distortion parameter and become Shape part model does not need designer to repaint model, or modification moulded dimension by hand, saves the plenty of time.
Using the above embodiment of the present invention, each part model is assembled one by one by hand without designer, in very great Cheng The design cycle is reduced on degree, and reduces the probability of error.
Using the above embodiment of the present invention, without repeating to draw engineering drawing and filling in BOM tables.
A kind of the above embodiment of the present invention, there is provided assembly method faster, more excellent, more intelligent, makes part from generation To assembling, ultimately produce engineering drawing and BOM tables fully achieve automation.Particularly big to some data capacities, part repeats profit With rate assembly high, the present invention can significantly improve design efficiency, be that enterprise saves more manpower and financial resources.
According to embodiments of the present invention, a kind of component assembling apparatus embodiment is additionally provided, it is necessary to explanation, part dress Can be used for performing the component assembling method in the embodiment of the present invention with device, the component assembling method in the embodiment of the present invention can Performed with the component assembling apparatus.
Figure 10 is a kind of schematic diagram of component assembling apparatus according to embodiments of the present invention, and as shown in Figure 10, the device can To include:Acquiring unit 103, for obtaining, multiple is to be installed to replace the spare parts, wherein, each one size distortion of correspondence that replaces the spare parts to be installed Parameter;Generation unit 105, for generating the deformation part for replacing the spare parts to be installed according to size distortion parameter, obtains multiple deformations zero Part;Assembly unit 107, is assembled the deformation part for adhering to Point matching for traveling through multiple deformation parts, obtains multiple changes The assembly of shape part, wherein, it is provided with attachment point in deformation part.
It should be noted that the acquiring unit 103 in the embodiment can be used for performing the step in the embodiment of the present application S102, the generation unit 105 in the embodiment can be used for performing the step S104 in the embodiment of the present application, in the embodiment Assembly unit 107 can be used for performing the step S106 in the embodiment of the present application.Above-mentioned module is realized with corresponding step Example is identical with application scenarios, but is not limited to above-described embodiment disclosure of that.
By above-described embodiment, there is the to be installed of correspondingly-sized deformation parameter and replace the spare parts in acquisition, then by each to be assembled zero Part assigns corresponding deformation parameter, generation and the corresponding multiple deformation parts that replace the spare parts to be installed, then again by traveling through multiple change Shape part, according to the attachment point for being set on deformation part in advance, the deformation part that there is matching relationship to attachment point enters luggage Match somebody with somebody, obtain the assembly being made up of multiple deformation part.Using the present invention, treat Assembly part and obtained by size distortion parameter Deformation part, the matching further according to attachment point is assembled to deformation part, can automatically complete part from being generated to assembling Process, and accelerate the process of assembling, particularly big to some data capacities, the assembly of part high recycling rate can Design efficiency is significantly improved, the less efficient technical problem of component assembly is solved.
Used as a kind of optional embodiment, assembly unit can include:First matching module, for traveling through multiple deformations zero Part, the deformation part for being possible to carry out adhering to Point matching is added in Assembly part set, it is impossible to carry out attachment Point matching Deformation part be added to without replace the spare parts set in;Second matching module, for traveling through without the set that replaces the spare parts, will be unassembled Deformation part in part set carries out attachment Point matching to obtain assembly with the deformation part in Assembly part set.
In a kind of optional embodiment, the first matching module can include:First spider module, for becoming according to multiple The order of shape part travels through multiple deformation parts successively, and the step shown in following submodule is performed to each deformation part:First Judging submodule, for judging whether Assembly part set is empty;First addition submodule, in Assembly part set In the case of for sky, will currently deform part and be added in Assembly part set;Second judging submodule, for assembling Part set not for sky in the case of, traversal Assembly part set in deformation part attachment point, judge whether with The attachment point of the attachment Point matching of current deformation part;Second addition submodule, for the deformation in Assembly part set In the case of there is the attachment point with the attachment Point matching of current deformation part in the attachment point of part, current deformation part is added In adding to Assembly part set;3rd addition submodule, for the attachment point of the deformation part in Assembly part set In in the absence of with the attachment point of the attachment Point matching of current deformation part in the case of, will currently deform part added to unassembled In part set.
Used as an optional embodiment, the second matching module can include:Second spider module, for unassembled zero In the case that part set is not for sky, traveled through successively without the set that replaces the spare parts according to without the order for deforming part in the set that replaces the spare parts In deformation part, the step shown in following submodule is performed to each deformation part:3rd judging submodule, for traveling through The attachment point of the deformation part in Assembly part set, judges whether the attachment with the attachment Point matching of currently deformation part Point;4th addition submodule, for existing and current deformation zero in the attachment point of the deformation part in Assembly part set In the case of the attachment point of the attachment Point matching of part, will currently deform deletion in part never Assembly part set, and will be current Deformation part is added in Assembly part set.
Used as a kind of optional embodiment, before acquiring unit, the embodiment can also include:Module is built, is used for Parts library is set up, wherein, parts library includes:Multiple standardized element models, attachment point is provided with standardized element model;Each The corresponding engineering drawing of standardized element model;Each corresponding parameter list of standardized element model, parameter list includes standardized element mould The size distortion parameter of type, size distortion parameter is used for the size for indicating to change standardized element model.
An optional embodiment, after assembly unit, the embodiment can also include:Update module, for according to Each corresponding size distortion parameter that replaces the spare parts to be installed updates the engineering drawing for replacing the spare parts to be installed and BOM tables.
The embodiments of the present invention are for illustration only, and the quality of embodiment is not represented.
In the above embodiment of the present invention, the description to each embodiment all emphasizes particularly on different fields, and does not have in certain embodiment The part of detailed description, may refer to the associated description of other embodiment.
In several embodiments provided herein, it should be understood that disclosed technology contents, can be by other Mode is realized.Wherein, device embodiment described above is only schematical, such as division of described unit, Ke Yiwei A kind of division of logic function, can there is other dividing mode when actually realizing, such as multiple units or component can combine or Person is desirably integrated into another system, or some features can be ignored, or does not perform.Another, shown or discussed is mutual Between coupling or direct-coupling or communication connection can be the INDIRECT COUPLING or communication link of unit or module by some interfaces Connect, can be electrical or other forms.
The unit that is illustrated as separating component can be or may not be it is physically separate, it is aobvious as unit The part for showing can be or may not be physical location, you can with positioned at a place, or can also be distributed to multiple On unit.Some or all of unit therein can be according to the actual needs selected to realize the purpose of this embodiment scheme.
In addition, during each functional unit in each embodiment of the invention can be integrated in a processing unit, it is also possible to It is that unit is individually physically present, it is also possible to which two or more units are integrated in a unit.Above-mentioned integrated list Unit can both be realized in the form of hardware, it would however also be possible to employ the form of SFU software functional unit is realized.
If the integrated unit is to realize in the form of SFU software functional unit and as independent production marketing or use When, can store in a computer read/write memory medium.Based on such understanding, technical scheme is substantially The part for being contributed to prior art in other words or all or part of the technical scheme can be in the form of software products Embody, the computer software product is stored in a storage medium, including some instructions are used to so that a computer Equipment (can be personal computer, server or network equipment etc.) perform each embodiment methods described of the invention whole or Part steps.And foregoing storage medium includes:USB flash disk, read-only storage (ROM, Read-Only Memory), arbitrary access are deposited Reservoir (RAM, Random Access Memory), mobile hard disk, magnetic disc or CD etc. are various can be with store program codes Medium.
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art For member, under the premise without departing from the principles of the invention, some improvements and modifications can also be made, these improvements and modifications also should It is considered as protection scope of the present invention.

Claims (10)

1. a kind of component assembling method, it is characterised in that including:
Acquisition multiple is to be installed to replace the spare parts, wherein, each described one size distortion parameter of correspondence that replaces the spare parts to be installed;
The deformation part for replacing the spare parts to be installed is generated according to the size distortion parameter, multiple deformation parts are obtained;
The multiple deformation parts of traversal are assembled the deformation part for adhering to Point matching, obtain multiple deformations zero The assembly of part, wherein, it is provided with the attachment point in the deformation part.
2. method according to claim 1, it is characterised in that the multiple deformation parts of the traversal will adhere to Point matching The deformation part assembled, the assemblies for obtaining multiple deformation parts include:
Multiple deformation parts are traveled through, the deformation part for being possible to carry out adhering to Point matching is added to Assembly part collection In conjunction, it is impossible to which the deformation part for adhere to Point matching is added to without in the set that replaces the spare parts;
Traversal is described without the set that replaces the spare parts, by the deformation part and the Assembly part collection without in the set that replaces the spare parts Deformation part in conjunction carries out attachment Point matching to obtain the assembly.
3. method according to claim 2, it is characterised in that the multiple deformation parts of the traversal, is possible to carry out The deformation part for adhering to Point matching is added in Assembly part set, it is impossible to adhere to the deformation of Point matching Part is added to be included without the set that replaces the spare parts:
Order according to the multiple deformation part travels through multiple deformation parts successively, is performed to deforming part each described Following steps:
Whether Assembly part set described in judging is empty;
In the case where the collection of Assembly part is combined into sky, will currently deform part and be added to the Assembly part set In;
In the case where the Assembly part set is not for sky, the attached of part is deformed in Assembly part set described in traversal A little, judge whether the attachment point with the attachment Point matching of the current deformation part;
There is the attachment point with the current deformation part in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of matching, the current deformation part is added in the Assembly part set;
In the absence of the attachment with the current deformation part in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of Point matching, by the current deformation part added to described without in the set that replaces the spare parts.
4. method according to claim 2, it is characterised in that without the set that replaces the spare parts described in the traversal, will described in not Deformation part in Assembly part set carries out attachment Point matching to obtain with the deformation part in the Assembly part set The assembly includes:
In the case of described set without replacing the spare parts not for sky, according to described without the order for deforming part in the set that replaces the spare parts The deformation part without in the set that replaces the spare parts is traveled through successively, and following steps are performed to deforming part each described:
The attachment point of the deformation part in Assembly part set described in traversal, judges whether attached with currently deformation part The attachment point of Point matching;
There is the attachment point with the current deformation part in the attachment point of the deformation part in the Assembly part set In the case of the attachment point of matching, by the current deformation part from described without deletion in the set that replaces the spare parts, and described will work as Preceding deformation part is added in the Assembly part set.
5. method according to any one of claim 1 to 4, it is characterised in that obtain multiple to be installed replace the spare parts described Before, methods described also includes:
Parts library is set up, wherein, the parts library includes:
Multiple standardized element models, attachment point is provided with the standardized element model;
The corresponding engineering drawing of each described standardized element model;
The corresponding parameter list of each described standardized element model, the parameter list includes that the size of the standardized element model becomes Shape parameter, the size distortion parameter is used for the size for indicating to change the standardized element model.
6. method according to any one of claim 1 to 4, it is characterised in that in the multiple deformations zero of the traversal Part is assembled the deformation part for adhering to Point matching, after obtaining the assemblies of multiple deformation parts, the side Method also includes:
According to the corresponding size distortion parameter that replaces the spare parts to be installed each described update the engineering drawing for replacing the spare parts to be installed and BOM tables.
7. a kind of component assembling apparatus, it is characterised in that including:
Acquiring unit, for obtaining, multiple is to be installed to replace the spare parts, wherein, each described one size distortion ginseng of correspondence that replaces the spare parts to be installed Number;
Generation unit, for generating the deformation part for replacing the spare parts to be installed according to the size distortion parameter, obtains multiple institutes State deformation part;
Assembly unit, is assembled the deformation part for adhering to Point matching for traveling through multiple deformation parts, is obtained The assembly of multiple deformation parts, wherein, it is provided with the attachment point in the deformation part.
8. device according to claim 7, it is characterised in that the assembly unit includes:
First matching module, for traveling through multiple deformation parts, is possible to the deformation part for carrying out adhering to Point matching Added in Assembly part set, it is impossible to which the deformation part for adhere to Point matching is added to without the set that replaces the spare parts In;
Second matching module, it is described without the set that replaces the spare parts for traveling through, by the deformation part without in the set that replaces the spare parts Attachment Point matching is carried out to obtain the assembly with the deformation part in the Assembly part set.
9. device according to claim 8, it is characterised in that first matching module includes:
First spider module, travels through multiple deformation parts, to every successively for the order according to the multiple deformation part The individual deformation part performs the step shown in following submodule:
First judging submodule, for judging whether the Assembly part set is empty;
First addition submodule, in the case of being combined into sky in the collection of Assembly part, will currently deform part and be added to In the Assembly part set;
Second judging submodule, in the case of in the Assembly part set not for sky, Assembly part described in traversal The attachment point of the deformation part in set, judges whether the attachment point with the attachment Point matching of the current deformation part;
Second addition submodule, works as existing in the attachment point of the deformation part in the Assembly part set with described In the case of the attachment point of the attachment Point matching of preceding deformation part, by the current deformation part added to the Assembly part In set;
3rd addition submodule, in the Assembly part set deformation part attachment point in do not exist with it is described In the case of the attachment point of the attachment Point matching of current deformation part, the current deformation part is added to described unassembled zero In part set.
10. device according to claim 8, it is characterised in that second matching module includes:
Second spider module, in the case of described set without replacing the spare parts not for sky, according to described without the collection that replaces the spare parts The order for deforming part in conjunction travels through the deformation part without in the set that replaces the spare parts successively, is held to deforming part each described Step shown in the following submodule of row:
3rd judging submodule, the attachment point for traveling through the deformation part in the Assembly part set, judges whether to deposit In the attachment point with the attachment Point matching of current deformation part;
4th addition submodule, works as existing in the attachment point of the deformation part in the Assembly part set with described In the case of the attachment point of the attachment Point matching of preceding deformation part, by the current deformation part from described without the set that replaces the spare parts Middle deletion, and the current deformation part is added in the Assembly part set.
CN201710093277.7A 2017-02-21 2017-02-21 Component assembling method and device Pending CN106897515A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710093277.7A CN106897515A (en) 2017-02-21 2017-02-21 Component assembling method and device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710093277.7A CN106897515A (en) 2017-02-21 2017-02-21 Component assembling method and device

Publications (1)

Publication Number Publication Date
CN106897515A true CN106897515A (en) 2017-06-27

Family

ID=59185685

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710093277.7A Pending CN106897515A (en) 2017-02-21 2017-02-21 Component assembling method and device

Country Status (1)

Country Link
CN (1) CN106897515A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109408918A (en) * 2018-10-11 2019-03-01 上海航天精密机械研究所 A kind of Alternative Collaborative Manufacturing method based on digital transfer

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103838915A (en) * 2014-01-09 2014-06-04 华北电力大学 Rapid serialization modeling method for mechanical component or complete machine
US8773945B1 (en) * 2013-03-13 2014-07-08 The United States Of America As Represented By The Secretary Of The Navy Apparatus for turbulent boundary layer control and flow noise reduction
CN104657554A (en) * 2015-02-10 2015-05-27 北京宇航系统工程研究所 Rapid rocket three-dimensional model design information extraction system
CN106127863A (en) * 2016-06-30 2016-11-16 滁州市科创模具制造有限公司 A kind of refrigerator foaming die series design system and method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8773945B1 (en) * 2013-03-13 2014-07-08 The United States Of America As Represented By The Secretary Of The Navy Apparatus for turbulent boundary layer control and flow noise reduction
CN103838915A (en) * 2014-01-09 2014-06-04 华北电力大学 Rapid serialization modeling method for mechanical component or complete machine
CN104657554A (en) * 2015-02-10 2015-05-27 北京宇航系统工程研究所 Rapid rocket three-dimensional model design information extraction system
CN106127863A (en) * 2016-06-30 2016-11-16 滁州市科创模具制造有限公司 A kind of refrigerator foaming die series design system and method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
冯亮亮: "CAD/PDM系统一体化产品快速设计研究与应用", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109408918A (en) * 2018-10-11 2019-03-01 上海航天精密机械研究所 A kind of Alternative Collaborative Manufacturing method based on digital transfer

Similar Documents

Publication Publication Date Title
Gyulassy et al. Efficient computation of Morse-Smale complexes for three-dimensional scalar functions
CN105549548B (en) Three-dimensional assembly technique generation method and generating means
CN104462155B (en) A kind of method for building up and device of point of interest set membership
CN105677648B (en) A kind of Combo discovering method and system based on label propagation algorithm
CN108595763A (en) Die assembly design method based on model index technology
CN102184299B (en) Model conversion method and system from CAD (Computer Aided Design) system to three-dimensional checking system
CN103389683A (en) CAM (computer-aided manufacturing) system of high-power thick-plate numerical control laser cutting machine and method
CN104573185B (en) The processing method and processing device of High-sped Trains index
CN104392037B (en) City scene parameterization modeling system
CN104820733B (en) A kind of bullet train demand meta-model method for building up and device
CN108959694A (en) A kind of BIM geometrical model construction method of big scale of construction complex building
CN109766605A (en) Method for building up in kind with the power distribution network full information mathematical model of value linkage
CN106021733B (en) A kind of fast custom design service system of production line
CN113312369A (en) Multi-scale map database cascading updating method based on unique identification code
CN109359355B (en) Design implementation method of standard structure module
CN106408435A (en) Process compiling system and process compiling method
CN105426590A (en) Machining process feature tree and construction method thereof
CN106682816A (en) Feature-basedthree-dimensional machiningtechnology layout system and method
CN114238488A (en) Multi-professional digital fruit integration and data interaction method and system
CN114746815A (en) Method for creating a digital twin of a facility or device
CN103077255B (en) Identification method and system for 3D (three-dimensional) model of nuclear power station
CN107967582A (en) The bill-of-material structure generation method and device of product
CN106897515A (en) Component assembling method and device
CN111881578B (en) Graph database based mechanical product digital twin model layered modeling method
CN116521921B (en) Configuration and query method of data model in three-dimensional visual scene

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20170627

RJ01 Rejection of invention patent application after publication