CN109454900A - A kind of carbon fiber tubular member forming method - Google Patents
A kind of carbon fiber tubular member forming method Download PDFInfo
- Publication number
- CN109454900A CN109454900A CN201811262305.4A CN201811262305A CN109454900A CN 109454900 A CN109454900 A CN 109454900A CN 201811262305 A CN201811262305 A CN 201811262305A CN 109454900 A CN109454900 A CN 109454900A
- Authority
- CN
- China
- Prior art keywords
- layer
- carbon fiber
- tubular member
- resin
- plastic tube
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2023/00—Tubular articles
Abstract
The invention discloses a kind of carbon fiber tubular member forming methods, the carbon fiber tubular member molding includes the following steps are as follows: the pre-processing of S1, thermal contractible plastic tube layer carry out the second separation layer of coating in thermal contractible plastic tube layer surfaces externally and internally and carries out the first separation layer of coating in die surface.S2, carbon fibre material are immersed in solution, then carry out the laying of prepreg.A certain amount of resin is sucked out from carbon fibre material layer laminate block under conditions of certain temperature and pressure in S3, pre-suction adhesive process, so that the resin content of layer of carbon fiber material is controlled.The present invention is shunk under conditions of high temperature automatically by thermal contractible plastic tube layer, resin softens layer of carbon fiber material in the event of high temperatures simultaneously, pyrocondensation institute's plastic pipe layer, which is shunk, uniformly presses to layer of carbon fiber material, so that resin levelling, achieve the effect that keep article surface smooth, is suitble to be widely popularized and use.
Description
Technical field
The present invention relates to carbon fiber pipe processing technique field, specially a kind of carbon fiber tubular member forming method.
Background technique
Carbon fiber pipe is also known as carbon fibre pipe, also referred to as carbon pipe, carbon fibre tube, is using carbon fibre composite pre-immersion benzene second
Dilute heated solidification pultrusion (twine and scratch) of base alkyd resin forms.During processed, it can be produced by different molds various
Profile, such as: the carbon fiber round tube of different size, the square tube of different size, the sheet material of different size and other profiles: making
Also it can wrap 3K during making and carry out surfactant package beautification etc..
Previous carbon fiber pipe forming method during processing, molding tube surfaces will appear compression it is uneven to
There is the phenomenon of fold injustice, in the past during being heating and curing, resin outflow can to produce between carbon fiber pipe and mold
Life is adhered, low so as to cause demoulding efficiency, and the spoilage occurred is higher, therefore, it is proposed that a kind of carbon fiber cast
Part forming method.
Summary of the invention
The purpose of the present invention is to provide a kind of carbon fiber tubular member forming method, solve proposed in background technique at
It is uneven to the phenomenon of fold injustice, in the past during being heating and curing, resin occur that the tube surfaces of type will appear compression
Outflow, can make between carbon fiber pipe and mold generate be adhered, it is low so as to cause demoulding efficiency, and occur spoilage compared with
High problem.
To achieve the above object, the invention provides the following technical scheme: a kind of carbon fiber tubular member forming method, the carbon
The molding of fiber tubular member includes the following steps are as follows:
The pre-processing of S1, thermal contractible plastic tube layer, thermal contractible plastic tube layer surfaces externally and internally carry out coating the second separation layer and
Die surface carries out the first separation layer of coating.
S2, carbon fibre material are immersed in solution, then carry out the laying of prepreg.
S3, pre-suction adhesive process are sucked out certain under conditions of certain temperature and pressure from carbon fibre material layer laminate block
The resin of amount, so that the resin content of layer of carbon fiber material is controlled.
S4, pyrocondensation technique, in the case where heated, the resin in layer of carbon fiber material can soften, while thermal contraction plastic expects pipe
Layer can be shunk in the case where heated, and thermal contractible plastic tube layer, which is shunk, to apply pressure to layer of carbon fiber material, so that the tree of flowing
Rouge levelling in the case where pressure.
S5, cure process after heat-shrink tube contraction, continue to increase temperature, resin is in higher temperatures in hot-press equipment
Start to solidify under the conditions of degree, so that the shape that the generation between layer of carbon fiber material is fixed, while can be with during cured
Air molecule existing between carbon fibre material is removed using layer of auxiliary material.
S6, releasing process, during cured, thermal contractible plastic tube layer softens into rubbery elastic in the event of high temperatures
Body can be demoulded directly by the first separation layer and the second separation layer, and the process generation of demoulding is avoided to be adhered.
As a kind of preferred embodiment of the invention, first separation layer and the second separation layer are non-silicon demoulding
Oxidant layer.
As a kind of preferred embodiment of the invention, the layer of auxiliary material is vacuum bag.
As a kind of preferred embodiment of the invention, the hot-pressing thermal that the curing process uses is standby for autoclave.
As a kind of preferred embodiment of the invention, the mold is column steel die.
As a kind of preferred embodiment of the invention, the predip solution is vinylbenzyl alkyd resin solution.
Compared with prior art, beneficial effects of the present invention are as follows:
1. carbon fiber tubular member forming method of the invention is shunk under conditions of high temperature, together automatically by thermal contractible plastic tube layer
When layer of carbon fiber material resin softens in the event of high temperatures, pyrocondensation institute's plastic pipe layer shrink layer of carbon fiber material is carried out it is equal
Even pressure, so that resin levelling, achievees the effect that keep article surface smooth.
2. carbon fiber tubular member forming method of the invention, is provided with the first separation layer and carbon by the outer surface of mold
Fibrous material layer surface is provided with the second separation layer, so that avoiding the occurrence of being convenient in demoulding after hardening and being adhered phenomenon, influences to give birth to
The qualification rate and efficiency of production.
3. carbon fiber tubular member forming method of the invention is vacuum bag by layer of auxiliary material, so that in cured mistake
It is capable of providing vacuum state in journey, the air molecule of institute's band in material is taken away, avoids solidifying the influence by air.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is pyrocondensation schematic diagram in the embodiment of the present invention.
In figure: 1 mold, 2 first separation layers, 3 layer of carbon fiber material, 4 second separation layers, 5 thermal contractible plastic tube layer, 6 auxiliary
Material layer.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
Referring to Fig. 1, the present invention provides a kind of technical solution: a kind of carbon fiber tubular member forming method: the carbon fiber
Tubular member molding includes the following steps are as follows:
The pre-processing of S1, thermal contractible plastic tube layer, 5 surfaces externally and internally of thermal contractible plastic tube layer carry out coating the second separation layer 3 and
The first separation layer 2 of coating is carried out on 1 surface of mold.
S2, carbon fibre material are immersed in solution, then carry out the laying of prepreg.
S3, pre-suction adhesive process are sucked out one from 3 lamination block of layer of carbon fiber material under conditions of certain temperature and pressure
Quantitative resin avoids the excessive subsequent technique of content from needing to increase suction so that the resin content of layer of carbon fiber material 3 is controlled
Glue material causes trouble.
S4, pyrocondensation technique, in the case where heated, the resin in layer of carbon fiber material can soften, while thermal contraction plastic expects pipe
Layer 5 can be shunk in the case where heated, and thermal contractible plastic tube layer 5, which is shunk, to apply pressure to layer of carbon fiber material, so that flowing
Resin levelling in the case where pressure, so that pipe profile surface after molding is smooth.
S5, cure process after heat-shrink tube contraction, continue to increase temperature, resin is in higher temperatures in hot-press equipment
Start to solidify under the conditions of degree, so that the shape that the generation between layer of carbon fiber material 3 is fixed, while can be with during cured
Air molecule existing between carbon fibre material is removed using layer of auxiliary material 6, air molecule is avoided to cause solidification
It influences.
S6, releasing process, during cured, thermal contractible plastic tube layer 5 softens into rubbery state bullet in the event of high temperatures
Property body, can directly be demoulded by the first separation layer 2 and the second separation layer 4, avoid demoulding process generation be adhered.
In the present embodiment, the first separation layer 2 and the second separation layer 4 are non-silicon releasing agent layer, and layer of auxiliary material 6 is true
Empty bag, the hot-pressing thermal that curing process uses is standby for autoclave, and mold 1 is column steel die, and predip solution is poly- for vinylbenzyl
Rouge resin solution.
In conclusion temperature needed for pre-suction adhesive process, pyrocondensation technique and cure process in the present invention, so that logical
It crosses layer of carbon fiber material 3 and different thermal contractible plastic tube material determines, inhale adhesive process and need stationary temperature, in technical process
In can directly be demoulded by the first separation layer 2 and the second 4 layers of isolation, avoid the process generation of demoulding from being adhered, Er Qiere
Contracting technique makes pressure uniform, so that softening resin can be driven plain, avoids material surface appearance after molding rough
Phenomenon is produced by the technique, so that qualification rate and efficiency can be promoted effectively.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from spirit of the invention or
In the case where essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that fall within the meaning and scope of the equivalent elements of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (6)
1. a kind of carbon fiber tubular member forming method, it is characterised in that: the carbon fiber tubular member molding includes the following steps are as follows:
The pre-processing of S1, thermal contractible plastic tube layer, thermal contractible plastic tube layer surfaces externally and internally carry out coating the second separation layer and
Die surface carries out the first separation layer of coating.
S2, carbon fibre material are immersed in solution, then carry out the laying of prepreg.
S3, pre-suction adhesive process are sucked out a certain amount of under conditions of certain temperature and pressure from carbon fibre material layer laminate block
Resin, so that the resin content of layer of carbon fiber material is controlled.
S4, pyrocondensation technique, in the case where heated, the resin in layer of carbon fiber material can soften, while thermal contractible plastic tube layer exists
It can be shunk in the case where heated, thermal contractible plastic tube layer, which is shunk, to apply pressure to layer of carbon fiber material, so that the resin of flowing exists
Levelling in the case where pressure.
S5, cure process after heat-shrink tube contraction, continue to increase temperature, resin is in higher temperature item in hot-press equipment
Start to solidify under part, so that the shape that the generation between layer of carbon fiber material is fixed, while can use during cured
Layer of auxiliary material is removed air molecule existing between carbon fibre material.
S6, releasing process, during cured, thermal contractible plastic tube layer softens into rubbery elastomers in the event of high temperatures,
It can directly be demoulded by the first separation layer and the second separation layer, the process generation of demoulding is avoided to be adhered.
2. a kind of carbon fiber tubular member forming method according to claim 1, it is characterised in that: first separation layer and
Second separation layer is non-silicon releasing agent layer.
3. a kind of carbon fiber tubular member forming method according to claim 1, it is characterised in that: the layer of auxiliary material is
Vacuum bag.
4. a kind of carbon fiber tubular member forming method according to claim 1, it is characterised in that: the curing process uses
Hot-pressing thermal it is standby be autoclave.
5. a kind of carbon fiber tubular member forming method according to claim 1, it is characterised in that: the mold is column steel
Molding jig.
6. a kind of carbon fiber tubular member forming method according to claim 1, it is characterised in that: the predip solution is benzene
The dilute base alkyd resin solution of second.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811262305.4A CN109454900A (en) | 2018-10-27 | 2018-10-27 | A kind of carbon fiber tubular member forming method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811262305.4A CN109454900A (en) | 2018-10-27 | 2018-10-27 | A kind of carbon fiber tubular member forming method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109454900A true CN109454900A (en) | 2019-03-12 |
Family
ID=65608649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811262305.4A Pending CN109454900A (en) | 2018-10-27 | 2018-10-27 | A kind of carbon fiber tubular member forming method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109454900A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110303695A (en) * | 2019-07-06 | 2019-10-08 | 朱亚鹏 | A kind of carbon fiber pipe molding machine and carbon fiber pipe |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120119060A1 (en) * | 2009-05-07 | 2012-05-17 | Eads Deutschland Gmbh | Device for Shaping a Workpiece |
| CN103273665A (en) * | 2013-06-14 | 2013-09-04 | 沈阳飞机工业（集团）有限公司 | Forming technology of square pipe part made of composite material |
| CN103978699A (en) * | 2014-05-14 | 2014-08-13 | 江西洪都航空工业集团有限责任公司 | Carbon fiber tube part forming method |
| CN104015376A (en) * | 2014-05-27 | 2014-09-03 | 上海迪诺克新材料科技有限公司 | Mixing and forming method of carbon fiber composite material |
| CN104441684A (en) * | 2014-12-18 | 2015-03-25 | 中国电子科技集团公司第三十九研究所 | After-treatment-free forming method of composite material tubes |
| CN105922607A (en) * | 2016-05-18 | 2016-09-07 | 中国电子科技集团公司电子科学研究院 | Forming method and device for composite material pipe fitting |
-
2018
- 2018-10-27 CN CN201811262305.4A patent/CN109454900A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120119060A1 (en) * | 2009-05-07 | 2012-05-17 | Eads Deutschland Gmbh | Device for Shaping a Workpiece |
| CN103273665A (en) * | 2013-06-14 | 2013-09-04 | 沈阳飞机工业（集团）有限公司 | Forming technology of square pipe part made of composite material |
| CN103978699A (en) * | 2014-05-14 | 2014-08-13 | 江西洪都航空工业集团有限责任公司 | Carbon fiber tube part forming method |
| CN104015376A (en) * | 2014-05-27 | 2014-09-03 | 上海迪诺克新材料科技有限公司 | Mixing and forming method of carbon fiber composite material |
| CN104441684A (en) * | 2014-12-18 | 2015-03-25 | 中国电子科技集团公司第三十九研究所 | After-treatment-free forming method of composite material tubes |
| CN105922607A (en) * | 2016-05-18 | 2016-09-07 | 中国电子科技集团公司电子科学研究院 | Forming method and device for composite material pipe fitting |
Non-Patent Citations (1)
| Title |
|---|
| 郭金树: "《复合材料可制造性技术》", 30 June 2009, 航空工业出版社 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110303695A (en) * | 2019-07-06 | 2019-10-08 | 朱亚鹏 | A kind of carbon fiber pipe molding machine and carbon fiber pipe |
| CN110303695B (en) * | 2019-07-06 | 2021-11-12 | 科泰思(中国)复合材料有限责任公司 | Carbon fiber tube forming device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104812556B (en) | Method for forming shaped preform | |
| CN109910208B (en) | Core die, preparation method thereof and forming method of composite material special pipe | |
| CN112536946B (en) | Composite material conical section forming die pressurized by using soft die | |
| CN112454938A (en) | Forming method of carbon fiber honeycomb sandwich composite material member | |
| CN106239929A (en) | A kind of making forming method of composite material pipe | |
| CN102230448A (en) | Wind power generator blade of bamboo fibre reinforced composite material and manufacture method thereof | |
| CN110978559A (en) | Preparation method of carbon fiber composite material part | |
| CN102555232A (en) | Process and device for multilayer bag pressing production of fibrous composite plates | |
| CN104015376A (en) | Mixing and forming method of carbon fiber composite material | |
| CN103958142A (en) | Preform manufacturing method and fiber-reinforced plastic molding manufacturing method | |
| CN107676814B (en) | Preparation method of composite material shell of embedded cable | |
| KR101447136B1 (en) | Method for Forming Fiber Reinforced Plastic Composite | |
| CN114261107B (en) | Composite material tubular beam and forming method thereof | |
| JP2008230020A (en) | Preform, its manufacturing method, and method for manufacturing frp | |
| CN109454900A (en) | A kind of carbon fiber tubular member forming method | |
| CN104589662A (en) | Core mold shell lamination molding method for carbon fiber bicycle parts and molding structure thereof | |
| CN110884168B (en) | Non-autoclave liquid forming device | |
| CN108115944A (en) | A kind of connection method of composite material pipe and metal pipe material | |
| CN104494165A (en) | Semi-soft die used for assisting racing boat moulding and one shot forming technology for racing boat | |
| JP2021030466A (en) | Method of producing fiber-reinforced resin molded product | |
| CN116394542A (en) | Square tube forming process by means of recycling die | |
| CN202251424U (en) | Polyurethane compound rubber roller | |
| CN115302815A (en) | Manufacturing method of special-shaped airplane frame upright post | |
| CN110948909B (en) | Forming method of square equal-section large-size composite material box | |
| JP2009214371A (en) | Method for manufacturing fiber-reinforced composite material and fiber-reinforced composite material, method for manufacturing integrated structural member and integrated structural member |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190312 |
|
| RJ01 | Rejection of invention patent application after publication |