CN207509776U - A kind of advanced composite material (ACM) component molding mold - Google Patents

A kind of advanced composite material (ACM) component molding mold Download PDF

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Publication number
CN207509776U
CN207509776U CN201721646399.6U CN201721646399U CN207509776U CN 207509776 U CN207509776 U CN 207509776U CN 201721646399 U CN201721646399 U CN 201721646399U CN 207509776 U CN207509776 U CN 207509776U
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China
Prior art keywords
frame
template
composite material
acm
component
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Active
Application number
CN201721646399.6U
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Chinese (zh)
Inventor
江滨
刘丹
尚欢欢
欧阳羽林
江祎伟
吴旭
马成文
杨皓
何明
李国祥
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JIANGXI CHANGXING AVIATION EQUIPMENT CO Ltd
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JIANGXI CHANGXING AVIATION EQUIPMENT CO Ltd
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Priority to CN201721646399.6U priority Critical patent/CN207509776U/en
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Abstract

The utility model discloses a kind of advanced composite material (ACM) component molding molds, belong to molding die field, including being used for the template of forming part and being used to support the frame of template;Frame is located at the lower section of template, and template is connect by rivet with frame;The material of frame is configured to composite material.Composite material shaping mould disclosed in the utility model, it is consistent with the material of template by being configured to the material of frame, that is composite material, the thermal expansion coefficient of the frame of composite material and the template of composite material is made to become consistent, and then the influence for easily making the deformation between template and frame inconsistent in solidification of hot-press tank to component curing precision is reduced to minimum, so as to improve the precision of molding component, thus have the advantages that save cost, shorten the process-cycle, improve molding component precision.

Description

A kind of advanced composite material (ACM) component molding mold
Technical field
The utility model is related to molding die field, more particularly to a kind of advanced composite material (ACM) component molding mold.
Background technology
Composite product has that specific strength and specific modulus are high, designability is good, good insulating, excellent resistant to chemical etching The features such as property, mainly in high-technology fields applications such as space flight and aviation, defence and military, industry and high-end sport, particularly with Field of aerospace plays increasingly important role.
However, carrying out molding mold to composite product, in the prior art, mold is used for multiple times, aluminium chassis is with answering The template of condensation material easily deforms, and the precision of shaped article is caused to substantially reduce.Therefore, it is necessary to design one kind to carry The molding die of high shaped article precision.
Utility model content
It is the defects of in order to overcome the prior art, a kind of novel multiple the technical problem to be solved by the utility model is to propose Condensation material component molding mold, i.e. composite material consistent with the material of template by being configured to the material of frame, makes composite wood The thermal expansion coefficient of the frame of material and the template of composite material becomes consistent, and then easily makes template and frame in solidification of hot-press tank The inconsistent influence to component curing precision of deformation between frame is reduced to minimum, so as to improve the precision of molding component, because And have the advantages that save cost, shorten the process-cycle, improve molding component precision.
For this purpose, the utility model uses following technical scheme:
The utility model provides a kind of advanced composite material (ACM) component molding mold, including be used for forming part template and It is used to support the frame of the template;
The frame is located at the lower section of the template, and the template is connect by rivet with the frame;
The material of the frame is configured to composite material.
Optionally, the cross-sectional shape of the frame is rectangle;
The frame is equipped with multiple hollow outs for being used for loss of weight and air guide.
Optionally, the angle section for fixing the template and the frame is further included;
The angle section is between the template and the frame;
The angle section is fixedly connected by silica gel with the template;
The template, the angle section and the frame are fixedly connected by the rivet.
Optionally, the angle section is located at multiple junctions of the frame.
Optionally, the cross section of the angle section is L-shaped.
Optionally, the material of the angle section is configured to composite material.
Optionally, the composite material is configured to carbon fibre composite.
The beneficial effects of the utility model are:
A kind of advanced composite material (ACM) component molding mold provided by the utility model, by by the material of frame be configured to The material of template is consistent, i.e. composite material, and the thermal expansion coefficient of the frame of composite material and the template of composite material is made to become one It causes, and then the influence for easily making the deformation between template and frame inconsistent to component curing precision in solidification of hot-press tank reduces To minimum, so as to improve the precision of molding component, thus with saving cost, shortening process-cycle, raising molding component essence The advantages of spending.
Description of the drawings
Fig. 1 is that a kind of structure for advanced composite material (ACM) component molding mold that specific embodiment of the present invention provides is shown It is intended to;
Fig. 2 is a kind of structure diagram for advanced composite material (ACM) component that specific embodiment of the present invention provides.
In figure:
1st, template;2nd, frame;3rd, component;21st, hollow out.
Specific embodiment
Further illustrate the technical solution of the utility model below with reference to the accompanying drawings and specific embodiments.
Mold provided by the utility model can be adapted for manufacturing aircraft horizontal tail fin tip component, the material of the component For carbon fibre composite.Fig. 1 schematically illustrates a kind of advanced composite material (ACM) molding component mould provided by the utility model The structure diagram of tool, as shown in Figure 1.A kind of advanced composite material (ACM) component molding mold, the template 1 including being used for forming part With the frame 2 for being used to support template 1;Frame 2 is located at the lower section of template 1, and template 1 is connect by rivet with frame 2;Frame 2 Material is configured to composite material.In the prior art, the composite material that the template of use uses, frame using aluminum material, When mold is used for multiple times, when carrying out solidification of hot-press tank to composite element, due to the template thermal expansion different from frame Property and made up by the smaller silica gel of thermal expansion performance, it is clear that easily silica gel is made to come off, and aluminum frame and composite material Template cannot compensate deformation by silica gel well, and undesirable influence is caused on the precision of molding component.Therefore, based on Upper shortcoming, the utility model is consistent with the material of template 1 by being configured to the material of frame 2, i.e. composite material, makes compound The frame 2 of material and the thermal expansion coefficient of the template 1 of composite material become consistent, and then easily make template in solidification of hot-press tank The inconsistent influence to component curing precision of deformation between 1 and frame 2 is reduced to minimum, so as to improve the essence of molding component Degree, thus have the advantages that save cost, shorten the process-cycle, improve molding component precision.Wherein, in a particular application, type The upper surface of plate 1 is recessed forming part, and forming part is molding for placement member 3.Fig. 2 is the structure diagram of the component.
Preferably, the cross-sectional shape of frame 2 is rectangle;Frame 2 is equipped with multiple hollow outs for being used for loss of weight and air guide 21.Specifically, frame 2 is equipped with multiple hollow outs 21 for being used for air guide when loss of weight and solidification of hot-press tank, is conducive to hot-air Flowing, ensures the uniformity of heat distribution, and then can improve the precision of molding component.
In order to further fix template 1 and frame 2, it is preferable that further include the angle section for fixing template 1 and frame 2;Angle Material is between template 1 and frame 2;Angle section is fixedly connected by silica gel with template 1;By rivet by template 1, angle section and Frame 2 is fixedly connected.Specifically, angle section fixation is fitted in the back side of template 1 by silica gel first, wherein, angle section and type Be designed on plate 1 and frame 2 it is multiple be used for across the hole 4 of rivet, frame 2, angle section, Yi Jixing are then passed through by rivet Three is fixedly connected by the hole on plate 1, and hole 4 is adapted with rivet.
In order to further enhance the bearing capacity of 2 match plate 1 of frame, it is preferable that angle section is located at multiple junctions of frame 2. It is equipped in multiple junctions at 2 back side of frame for fixed angle section.
Preferably, the cross section of angle section is L-shaped.The angle section of L-type is consistent with the shape of the junction of frame 2, has more preferable Firm effect, improve frame 2 bearing capacity, be conducive to prolong the service life.
Preferably, the material of angle section is configured to composite material.
In above implementation, it is preferable that composite material is configured to carbon fibre composite.It is, frame 2, angle section and The material of template 1 is all configured to carbon fibre composite, and performance meets the requirement of covering curing molding.
By the way that the material of frame 2 is configured to composite material, the material of angle section and template 1 is also configured as composite material , wherein, composite material is specifically carbon fibre composite, i.e., by the global design of mold into the type plane materiel material of composite material, The weight of mold is alleviated, reduces manufacture cost, improves the formed precision of component, makes the deformation one of frame 2 and template 1 It causes, minimizes influence of the mold to the component curing deformation of composite material.
The utility model is described with reference to the preferred embodiments, and those skilled in the art know, is not departing from this reality In the case of with novel spirit and scope, various changes or equivalence replacement can be carried out to these features and embodiment.This reality It is not limited to the particular embodiment disclosed with novel, other embodiments fallen into claims hereof all belong to In the range of the utility model protection.

Claims (7)

1. a kind of advanced composite material (ACM) component molding mold, it is characterised in that:
Including being used for the template (1) of forming part and being used to support the frame (2) of the template (1);
The frame (2) is connect positioned at the lower section of the template (1), the template (1) by rivet with the frame (2);
The material of the frame (2) is configured to composite material.
2. a kind of advanced composite material (ACM) component molding mold as described in claim 1, it is characterised in that:
The cross-sectional shape of the frame (2) is rectangle;
The frame (2) is equipped with multiple hollow outs (21) for being used for loss of weight and air guide.
3. a kind of advanced composite material (ACM) component molding mold as claimed in claim 2, it is characterised in that:
Further include the angle section for fixing the template (1) and the frame (2);
The angle section is between the template (1) and the frame (2);
The angle section is fixedly connected by silica gel with the template (1);
The template (1), the angle section and the frame (2) are fixedly connected by the rivet.
4. a kind of advanced composite material (ACM) component molding mold as claimed in claim 3, it is characterised in that:
The angle section is located at multiple junctions of the frame (2).
5. a kind of advanced composite material (ACM) component molding mold as claimed in claim 3, it is characterised in that:
The cross section of the angle section is L-shaped.
6. a kind of advanced composite material (ACM) component molding mold as claimed in claim 3, it is characterised in that:
The material of the angle section is configured to composite material.
7. such as a kind of advanced composite material (ACM) component molding mold of claim 1 to 6 any one of them, it is characterised in that:
The composite material is configured to carbon fibre composite.
CN201721646399.6U 2017-11-30 2017-11-30 A kind of advanced composite material (ACM) component molding mold Active CN207509776U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721646399.6U CN207509776U (en) 2017-11-30 2017-11-30 A kind of advanced composite material (ACM) component molding mold

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721646399.6U CN207509776U (en) 2017-11-30 2017-11-30 A kind of advanced composite material (ACM) component molding mold

Publications (1)

Publication Number Publication Date
CN207509776U true CN207509776U (en) 2018-06-19

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Country Status (1)

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CN (1) CN207509776U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110308622A (en) * 2019-08-06 2019-10-08 宁波丽成超级树脂有限公司 A kind of high-accuracy carbon fiber platform of large size liquid crystal exposure sources
CN110561667A (en) * 2019-09-23 2019-12-13 东莞市康铭光电科技有限公司 sole forming die and metal 3D printing manufacturing method thereof

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110308622A (en) * 2019-08-06 2019-10-08 宁波丽成超级树脂有限公司 A kind of high-accuracy carbon fiber platform of large size liquid crystal exposure sources
CN110308622B (en) * 2019-08-06 2023-10-10 宁波丽成复合材料制品有限公司 High-precision carbon fiber platform for large-scale liquid crystal exposure equipment
CN110561667A (en) * 2019-09-23 2019-12-13 东莞市康铭光电科技有限公司 sole forming die and metal 3D printing manufacturing method thereof

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: Novel combined material component forming die

Effective date of registration: 20190926

Granted publication date: 20180619

Pledgee: Jingdezhen branch of Bank of Communications Co., Ltd.

Pledgor: JIANGXI CHANGXING AVIATION EQUIPMENT CO., LTD.

Registration number: Y2019360000011

PC01 Cancellation of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20201029

Granted publication date: 20180619

Pledgee: Jingdezhen branch of Bank of Communications Co.,Ltd.

Pledgor: JIANGXI CHANGXING AVIATION EQUIPMENT Co.,Ltd.

Registration number: Y2019360000011

PE01 Entry into force of the registration of the contract for pledge of patent right
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A new mold for composite components

Effective date of registration: 20201113

Granted publication date: 20180619

Pledgee: Jingdezhen branch of Bank of Communications Co.,Ltd.

Pledgor: JIANGXI CHANGXING AVIATION EQUIPMENT Co.,Ltd.

Registration number: Y2020980007898