CN103697840A - Virtual box closing verification method in casting process - Google Patents

Virtual box closing verification method in casting process Download PDF

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Publication number
CN103697840A
CN103697840A CN201310731641.XA CN201310731641A CN103697840A CN 103697840 A CN103697840 A CN 103697840A CN 201310731641 A CN201310731641 A CN 201310731641A CN 103697840 A CN103697840 A CN 103697840A
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CN
China
Prior art keywords
core
size
verification method
die cavity
gap
Prior art date
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Pending
Application number
CN201310731641.XA
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Chinese (zh)
Inventor
郭小利
唐钟雪
何启良
谢厚霓
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.)
Kocel Group Co Ltd
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Kocel Group 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 Kocel Group Co Ltd filed Critical Kocel Group Co Ltd
Priority to CN201310731641.XA priority Critical patent/CN103697840A/en
Publication of CN103697840A publication Critical patent/CN103697840A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a box closing verification method, in particular to a virtual box closing verification method in a casting process, wherein the virtual box closing verification method is used for judging possible mistakes or defects existing in core molding of a sand core and a mold cavity. The method comprises the steps of establishing a cube with a size which is consistent with the size of a sand box in three-dimensional software, differencing the cube and an outer skin model and establishing the cavity; in the process of sand core movement, assembling the core head of the sand core at a core head positioning position in the cavity, setting a key frame at the position and producing a movement animation; starting an interference detection mode and a gap detection mode of the software; under the situation that the sizes are correctly matched, assembling the core head at the core head positioning position in a reasonable way that the size of a gap meets the requirement; when the size of the sand core is not matched with the size of the cavity, making a judgment according to two situations. The virtual box closing verification method in the casting process has the advantages that the method is unique, the mold rejection rate is reduced, the production cost is saved and the goals of smoothly setting the core and closing the box are realized.

Description

Virtual mould assembling verification method in a kind of casting process
Technical field
The present invention relates to a kind of mould assembling verification method, especially relate to a kind of for judging the virtual mould assembling verification method in wrong or not enough a kind of casting process that core and die cavity may exist in cored-up mould.
Background technology
When cast product adopts cored-up mould, in die cavity, conventionally need to place a plurality of cores, the designing quality of core and die cavity is subject to size, core location, pattern draft, model scale etc. compared with multifactor impact.And in traditional cored-up mould, core digital-to-analogue is mated checking with die cavity digital-to-analogue, designed rear direct mfg. moulding die, can not find in advance the wrong or not enough of design, in actual production, easily there is following problem: 1) core and cavity dimension design mistake, that reduced scale adds is inconsistent, it is unreasonable to mate, and causes product size bigger than normal or less than normal; 2) design of core shape is incorrect, and lower core process has interference, stops situation, cannot play core mould assembling.
Up to the present, also there is no a kind of method that overcomes above-mentioned defect.
Summary of the invention
The object of the invention is to overcome the defect of prior art, a kind of method uniqueness is provided, reduces mould scrappage, thus the virtual mould assembling verification method in a kind of casting process of the smoothly lower core mould assembling of realization that saves production cost.
The present invention realizes by the following method:
A virtual mould assembling verification method in casting process, is characterized in that: the method comprises the steps:
A. in three-dimensional software, set up and sandbox cube of the same size, ask poor with crust model, set up die cavity;
B. the sand core head of core is assembled to the place, core print location in above-mentioned die cavity, setting position key frame, makes motion animation herein;
C. in the process of described core motion, open software and interfere detecting pattern and gap detection pattern, the in the situation that of the correct coupling of size, described sand core head is assembled to place, described core print location, and the gap length at position, gap meets the requirements, and is rationally;
When d. the size of described core and the size of die cavity are not mated, judge in two kinds of situation;
Described two kinds of situations are as follows:
A. described core size is bigger than normal, runs into interference and collision in motion process, is interfering the automatic stop motion in position, and high brightness demonstration colliding part, can judge that core or die cavity exist dimensional problem;
B. described core size is less than normal, and excesssive gap between die cavity, at position, gap high brightness, shows excesssive gap position, can judge that core or die cavity exist dimensional problem;
Described three-dimensional software is NX software.
The present invention has following effect:
1) method is unique, by virtual emulation, simulate, in the design phase, just can find the above-mentioned mistake that may exist or problem, carrying out in time core and cavity design revises, avoid making a mistake in follow-up practical operation, thereby realize smoothly lower core mould assembling: the virtual mould assembling verification method in a kind of casting process provided by the invention, adopt virtual software to interfere inspection side, its detection method is: core is positioned in die cavity in assembling mode, in moving process, enable the gap detection pattern of software and interfere detecting pattern, when detecting gap or interfering, core stops mobile, light form shows gap or interferes position.Thereby find out size gap or interference and collision between core and die cavity, carry out in time core and cavity design and revise.
2) reduce mould scrappage, save production cost: method provided by the invention is compared with direct mfg. moulding die after traditional design completes, and the mould that method provided by the invention can reduce to cause such as does over again, reprocesses at the workload.And can simulate mistake or the problem of finding existence in design, time update design proposal, reduces mould scrappage, saves production cost.
Accompanying drawing explanation
Fig. 1 interferes detection figure in mould assembling process of the present invention.
Embodiment
A virtual mould assembling verification method in casting process, as shown in Figure 1: the method comprises the steps:
A. in three-dimensional software, set up and sandbox cube of the same size, ask poor with crust model, set up die cavity 2;
B. the core print sand core head of core 34 being assembled in above-mentioned die cavity 2 is located 5 places, and setting position key frame, makes motion animation herein;
C. in the process of described core 3 motions, open software and interfere detecting pattern and gap detection pattern, the in the situation that of the correct coupling of size, described sand core head 4 is assembled to described core print and locates 5 places, and the gap length at position, gap 7 meets the requirements, be rationally;
When d. the size of described core 3 is not mated with the size of die cavity 2, judge in two kinds of situation.
Described two kinds of situations are as follows:
A. described core 3 sizes are bigger than normal, run into interference and collision in motion process, interfering the position automatic stop motion in 6 places, and high brightness demonstration colliding part, can judge that core or die cavity exist dimensional problem;
B. described core 3 sizes are less than normal, and excesssive gap between die cavity 2, and at position, gap, 7 place's high brightness show excesssive gap position, can judge that core or die cavity exist dimensional problem.
Described three-dimensional software is NX software.

Claims (3)

1. the virtual mould assembling verification method in casting process, is characterized in that: the method comprises the steps:
A. in three-dimensional software, set up and sandbox cube of the same size, ask poor with crust model, set up die cavity (2);
B. the core print location (5) sand core head of core (3) (4) being assembled in above-mentioned die cavity (2) is located, and setting position key frame, makes motion animation herein;
C. in the process of described core (3) motion, open software and interfere detecting pattern and gap detection pattern, the in the situation that of the correct coupling of size, described sand core head (4) is assembled to described core print location (5) and locates, and the gap length of position, gap (7) meets the requirements, be rationally;
When d. the size of described core (3) is not mated with the size of die cavity (2), judge in two kinds of situation.
2. the virtual mould assembling verification method in a kind of casting process as claimed in claim 1, is characterized in that: described two kinds of situations are as follows:
A. described core (3) size is bigger than normal, runs into interference and collision in motion process, is interfering position (6) to locate automatic stop motion, and high brightness demonstration colliding part, can judge that core or die cavity exist dimensional problem;
B. described core (3) size is less than normal, and excesssive gap between die cavity (2), locates high brightness show excesssive gap position in position, gap (7), can judge that core or die cavity exist dimensional problem.
3. the virtual mould assembling verification method in a kind of casting process as claimed in claim 1, is characterized in that: described three-dimensional software is NX software.
CN201310731641.XA 2013-12-27 2013-12-27 Virtual box closing verification method in casting process Pending CN103697840A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310731641.XA CN103697840A (en) 2013-12-27 2013-12-27 Virtual box closing verification method in casting process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310731641.XA CN103697840A (en) 2013-12-27 2013-12-27 Virtual box closing verification method in casting process

Publications (1)

Publication Number Publication Date
CN103697840A true CN103697840A (en) 2014-04-02

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CN201310731641.XA Pending CN103697840A (en) 2013-12-27 2013-12-27 Virtual box closing verification method in casting process

Country Status (1)

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CN (1) CN103697840A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105354357A (en) * 2015-09-29 2016-02-24 共享装备股份有限公司 Three-dimensional casting process verification method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101054881A (en) * 2007-03-21 2007-10-17 丁祎 Automobile gate glass lifter quick design system
JP2009039777A (en) * 2007-08-10 2009-02-26 Union Parts Kogyo:Kk Core molding method and core molding device
CN101592939A (en) * 2008-05-29 2009-12-02 上海电气集团股份有限公司 Based on the five-axle number control machine tool modeling of UG and the method for virtual assembling
CN102354148A (en) * 2011-08-22 2012-02-15 亿森(上海)模具有限公司 Method for carrying out interference inspection on moulds based on assembling
CN103418752A (en) * 2013-09-03 2013-12-04 宁夏共享集团有限责任公司 Method for locating ultrahigh circular sand core

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101054881A (en) * 2007-03-21 2007-10-17 丁祎 Automobile gate glass lifter quick design system
JP2009039777A (en) * 2007-08-10 2009-02-26 Union Parts Kogyo:Kk Core molding method and core molding device
CN101592939A (en) * 2008-05-29 2009-12-02 上海电气集团股份有限公司 Based on the five-axle number control machine tool modeling of UG and the method for virtual assembling
CN102354148A (en) * 2011-08-22 2012-02-15 亿森(上海)模具有限公司 Method for carrying out interference inspection on moulds based on assembling
CN103418752A (en) * 2013-09-03 2013-12-04 宁夏共享集团有限责任公司 Method for locating ultrahigh circular sand core

Non-Patent Citations (3)

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Title
张侃楞: "基于UG的4J34柴油机机体压铸模设计", 《模具制造》, no. 12, 31 December 2008 (2008-12-31) *
方志平: "侧架CAD/CAE/CAM技术研究", 《中国优秀博硕士学位论文全文数据库(硕士)(工程科技I辑)》, 15 January 2006 (2006-01-15) *
李学锋: "《注射模具设计与制造》", 31 January 2010, article "模具运动仿真和干涉检查", pages: 371 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105354357A (en) * 2015-09-29 2016-02-24 共享装备股份有限公司 Three-dimensional casting process verification method

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Application publication date: 20140402