CN103886134A - Position changing method of zero-component three-dimensional model - Google Patents

Position changing method of zero-component three-dimensional model Download PDF

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Publication number
CN103886134A
CN103886134A CN201410065513.0A CN201410065513A CN103886134A CN 103886134 A CN103886134 A CN 103886134A CN 201410065513 A CN201410065513 A CN 201410065513A CN 103886134 A CN103886134 A CN 103886134A
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CN
China
Prior art keywords
spare part
zero
component
model
dimensional model
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Pending
Application number
CN201410065513.0A
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Chinese (zh)
Inventor
王军
万世明
何万飞
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Chengdu Aircraft Industrial Group Co Ltd
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Chengdu Aircraft Industrial Group Co Ltd
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Application filed by Chengdu Aircraft Industrial Group Co Ltd filed Critical Chengdu Aircraft Industrial Group Co Ltd
Priority to CN201410065513.0A priority Critical patent/CN103886134A/en
Publication of CN103886134A publication Critical patent/CN103886134A/en
Pending legal-status Critical Current

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Abstract

The invention provides a position changing method of a zero-component three-dimensional model and aims to solve the problem that a position changing method of the zero-component three-dimensional model is quite troublesome in operation, less prone to causing errors and the like in the prior art. The position changing method includes adopting CATIA software to build a three-dimensional model of a zero component; before building the zero-component model, establishing a zero-component axis system, creating a structure sketch and an entity model of the zero component in the axis system, and maintaining all data and constraints of the zero-component model to only be related with the zero-component axis system during modeling; if coordinate position of the zero-component three-dimensional model need to be changed, double-clicking and editing the zero-component axis system to establish new coordinate position for the zero-component axis system according to the position needed to be changed, and refreshing. The position changing method has the advantages that when the coordinate position of the zero component needs to be changed, the zero-component model can be quickly changed to the new coordinate position only by modifying and editing the zero-component axis system, and the modeling process of the zero component is fully retained and can be used for reference, so that repeated design is avoided.

Description

The evolution method of spare part three-dimensional model
Technical field
The present invention relates to a kind of CATIA of employing software and set up the method for spare part three-dimensional model, specially refer to a kind of evolution method of spare part three-dimensional model.
Background technology
Adopt CATIA software to set up in product or parts three-dimensional model process, the shape and structure that usually can run into some spare part is basic identical, still, and the different situation of coordinate position in three-dimensional model.For example, the briquetting of fixing a certain part, after the coordinate position of part changes, the position of briquetting also will change.Due to the change of coordinate position, the modeling process of these similar spare parts cannot reuse, and needs modification or this all modeling again step by step.Certainly, can utilize the coordinate position of CATIA software " location conversion " function and " super copy " this type component of Functional change, then, more as required model of parts be modified.But, adopting behind " location conversion " coordinate transforming position, while revising the aspect of model before conversion, model can be got back to the position before conversion automatically, need to again carry out " location conversion ".And adopting " super copy " coordinate transforming position, map function is very loaded down with trivial details, and easily makes mistakes.Obviously, it is very loaded down with trivial details that the evolution method of prior art spare part three-dimensional model exists operation, and the problem such as easily make mistakes.
Summary of the invention
Very loaded down with trivial details for solving the operation that the evolution method of prior art spare part three-dimensional model exists, and the problem such as easily make mistakes, the present invention proposes a kind of evolution method of spare part three-dimensional model.The evolution method of spare part three-dimensional model of the present invention adopts CATIA software to set up the three-dimensional model of spare part, it is characterized in that, setting up before spare part model, select summit of a part being associated with spare part model yet to be built or intersection point as initial point, select seamed edge of a part being associated with spare part model yet to be built or axis as X-axis, and set up a spare part axle with this and be; In spare part axle system, set up structure sketch and the solid model of spare part, and in modeling process, keep all data of spare part model only associated with spare part axle system with constraint; While converting the coordinate position of spare part three-dimensional model as need, double-click, edit spare part axle system, new coordinate position is set up in the position of the required conversion of spare part axle system foundation, refresh rear spare part three-dimensional model and be converted into new coordinate position with spare part axle system; Describedly spare part axle system is set up to new coordinate position according to the position of required conversion refer to using the summit of a part associated therewith or the position of intersection point behind spare part model transferring position as the initial point of new spare part axle system, the X-axis using the seamed edge of a part associated therewith behind spare part model transferring position or axis as new spare part axle system.
The useful technique effect of the evolution method of spare part three-dimensional model of the present invention is need to convert the coordinate position of spare part time, only need to revise, edit spare part axle system, spare part model is by extremely new coordinate position of Fast transforms, the modeling process of spare part all remains and can use, avoid design iterations, repeated the troublesome operation of modeling, improved design setting model efficiency.
Accompanying drawing explanation
Accompanying drawing 1 is the schematic diagram before the evolution embodiment of the method evolution of spare part three-dimensional model of the present invention;
Accompanying drawing 2 is the schematic diagram after the evolution embodiment of the method evolution of spare part three-dimensional model of the present invention.
Below in conjunction with the drawings and specific embodiments, the evolution method of spare part three-dimensional model of the present invention is further described.
Embodiment
Accompanying drawing 1 is the schematic diagram before the evolution embodiment of the method evolution of spare part three-dimensional model of the present invention, accompanying drawing 2 is the schematic diagram after the evolution embodiment of the method evolution of spare part three-dimensional model of the present invention, in figure, 1 is briquetting, 2 is clamping arm I, 3 is part I, and 4 is clamping arm II, and 5 is part II.In the present embodiment, the briquetting model designing, is fixed on desired location by clamping arm I by part I.Now, because design needs, briquetting, from evolution shown in accompanying drawing 1 to position shown in accompanying drawing 2, is fixed on to desired location by clamping arm II by part II.Now adopt the evolution method of spare part three-dimensional model of the present invention to convert the coordinate position of briquetting.The evolution method of spare part three-dimensional model according to the present invention, adopt CATIA software to set up the three-dimensional model of spare part, it is characterized in that, setting up before spare part model, select summit of a part being associated with spare part model yet to be built or intersection point as initial point, select seamed edge of a part being associated with spare part model yet to be built or axis as X-axis, and set up a spare part axle with this and be; In spare part axle system, set up structure sketch and the solid model of spare part, and in modeling process, keep all data of spare part model only associated with spare part axle system with constraint; While converting the coordinate position of spare part three-dimensional model as need, double-click, edit spare part axle system, new coordinate position is set up in the position of the required conversion of spare part axle system foundation, refresh rear spare part three-dimensional model and be converted into new coordinate position with spare part axle system; Describedly spare part axle system is set up to new coordinate position according to the position of required conversion refer to using the summit of a part associated therewith or the position of intersection point behind spare part model transferring position as the initial point of new spare part axle system, the X-axis using the seamed edge of a part associated therewith behind spare part model transferring position or axis as new spare part axle system.
In the present embodiment, the summit in the longitudinal outside of the selected clamping arm I being associated with briquetting, as the initial point of spare part coordinate system, selects the longitudinal outer seamed edge of clamping arm I as X-axis, builds thus X, Y, Z spare part coordinate system.In X, Y, Z spare part coordinate system, set up structure sketch and the solid model of spare part, and in modeling process, keep all data of spare part model only associated with spare part axle system with constraint.Arrive this, fixed mechanism (comprising briquetting and the clamping arm I) modeling to part I completes.In the time the three-dimensional model of briquetting need to being converted to part II fixing, double-click, edit X, Y, Z shaft parts system, select the clamping arm II that is associated with briquetting outside longitudinally summit as the initial point of new spare part coordinate system, select the longitudinal outer seamed edge of clamping arm II as X-axis, build thus new X`, Y`, Z` spare part axle system, by spare part axle, system sets up new coordinate position according to required shifting one's position, and the three-dimensional model that refreshes rear briquetting is converted into new coordinate position with X`, Y`, Z` spare part axle system.Now, the modeling process of briquetting all remains and can use, and has avoided design iterations, has repeated the troublesome operation of modeling, has improved design setting model efficiency.
Obviously, the useful technique effect of the evolution method of spare part three-dimensional model of the present invention is need to convert the coordinate position of spare part time, only need to revise, edit spare part axle system, spare part model is by extremely new coordinate position of Fast transforms, the modeling process of spare part all remains and can use, avoid design iterations, repeated the troublesome operation of modeling, improved design setting model efficiency.

Claims (1)

1. the evolution method of a spare part three-dimensional model, adopt CATIA software to set up the three-dimensional model of spare part, it is characterized in that, setting up before spare part model, select summit of a part being associated with spare part model yet to be built or intersection point as initial point, select seamed edge of a part being associated with spare part model yet to be built or axis as X-axis, and set up a spare part axle with this and be; In spare part axle system, set up structure sketch and the solid model of spare part, and in modeling process, keep all data of spare part model only associated with spare part axle system with constraint; While converting the coordinate position of spare part three-dimensional model as need, double-click, edit spare part axle system, new coordinate position is set up in the position of the required conversion of spare part axle system foundation, refresh rear spare part three-dimensional model and be converted into new coordinate position with spare part axle system; Describedly spare part axle system is set up to new coordinate position according to the position of required conversion refer to using the summit of a part associated therewith or the position of intersection point behind spare part model transferring position as the initial point of new spare part axle system, the X-axis using the seamed edge of a part associated therewith behind spare part model transferring position or axis as new spare part axle system.
CN201410065513.0A 2014-02-26 2014-02-26 Position changing method of zero-component three-dimensional model Pending CN103886134A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410065513.0A CN103886134A (en) 2014-02-26 2014-02-26 Position changing method of zero-component three-dimensional model

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410065513.0A CN103886134A (en) 2014-02-26 2014-02-26 Position changing method of zero-component three-dimensional model

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CN103886134A true CN103886134A (en) 2014-06-25

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104809690A (en) * 2015-04-10 2015-07-29 西北工业大学 Intelligent fusing method for multiple rough drawings
CN105404714A (en) * 2015-10-28 2016-03-16 北京海颐威工程技术有限公司 Method and apparatus for in-place modification of member position in modeling software
CN111767604A (en) * 2020-05-15 2020-10-13 成都飞机工业(集团)有限责任公司 Fastener mounting point creating method based on CATIA knowledge engineering technology

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
徐磊: "基于30模型的船体分段检测系统的设计与实现", 《中国优秀硕士学位论文全文数据库 信息科技辑》 *
王晓康 等: "航空企业经济模具及其应用", 《航空制造技术》 *
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104809690A (en) * 2015-04-10 2015-07-29 西北工业大学 Intelligent fusing method for multiple rough drawings
CN104809690B (en) * 2015-04-10 2017-10-27 西北工业大学 A kind of intelligent method for fusing of many sketches
CN105404714A (en) * 2015-10-28 2016-03-16 北京海颐威工程技术有限公司 Method and apparatus for in-place modification of member position in modeling software
CN105404714B (en) * 2015-10-28 2019-01-15 北京瀚方伟业工程技术有限公司 A kind of method and apparatus for modifying member position in place in modeling software
CN111767604A (en) * 2020-05-15 2020-10-13 成都飞机工业(集团)有限责任公司 Fastener mounting point creating method based on CATIA knowledge engineering technology
CN111767604B (en) * 2020-05-15 2022-06-14 成都飞机工业(集团)有限责任公司 Fastener mounting point creating method based on CATIA knowledge engineering technology

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Application publication date: 20140625