CN103302843A - Making method of plate-shaped fiber reinforced product - Google Patents
Making method of plate-shaped fiber reinforced product Download PDFInfo
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- CN103302843A CN103302843A CN2012100580169A CN201210058016A CN103302843A CN 103302843 A CN103302843 A CN 103302843A CN 2012100580169 A CN2012100580169 A CN 2012100580169A CN 201210058016 A CN201210058016 A CN 201210058016A CN 103302843 A CN103302843 A CN 103302843A
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Abstract
A making method of a plate-shaped fiber reinforced product includes the following steps: 1, preparing a first fiber reinforcing material and a second fiber reinforcing material, wherein the first fiber reinforcing material has at least one first through hole; 2, laminating the first fiber reinforcing material and the second fiber reinforcing material in a die, wherein the die having a protruding portion which can be inserted to the first through hole; and 3, heating the die for the combination hardening of the first fiber reinforcing material and the second fiber reinforcing material in the die to form the plate-shaped fiber reinforced product, and taking the plate-shaped fiber reinforced product out of the die, wherein the plate-shaped fiber reinforced product has a depressed portion corresponding to the first through hole. The method comprising the above steps has the advantages of process simplification, process time shortening, processing cost reduction, material waste reduction and material cost reduction.
Description
Technical field
The present invention relates to a kind of manufacture method of fibre strengthening product, particularly relate to a kind of manufacture method of tabular fibre strengthening product.
Background technology
Consult Fig. 1,2, the manufacture method of existing tabular carbon fiber-reinforced product carry out step 11 before this, with several pieces carbon fibre initial rinse fabric 101 stacked being attached in the hot pressing die 102; Next, carry out step 12, the hot pressing die 102 that is pasted with described carbon fibre initial rinse fabric 101 is heated to 150 ℃, make the epoxy resin reaction in the described carbon fibre initial rinse fabric 101, and make tabular carbon fiber-reinforced semi-finished product 103, these tabular carbon fiber-reinforced semi-finished product 103 comprise a body 104, and a clamping part 105; Afterwards, carry out step 13, should take out from this hot pressing die 102 by tabular carbon fiber-reinforced semi-finished product 103; Then, shown in step 14, utilize the clamping part 105 of these tabular carbon fiber-reinforced semi-finished product 103 of anchor clamps 106 clampings, cooperate a processing apparatus 107 on the body 104 of these tabular carbon fiber-reinforced semi-finished product 103, be shaped predetermined hole, groove ... etc. architectural feature 108; Shown in step 15, again this clamping part 105 is removed at last, just can be obtained tabular carbon fiber-reinforced product 109.
Because, the manufacture method of existing tabular carbon fiber-reinforced product, must utilize additionally that processing apparatus 107 moulding are portalled, groove ... etc. architectural feature 108, also be convenient to add the clamping position in man-hour for fear of disfeaturing, therefore, essential extra this clamping part 105 that increases in the design of these tabular carbon fiber-reinforced semi-finished product 103, so, follow-up not only the need removed this clamping part 105, and cause the increase of whole process time and processing cost, the while also can be caused the waste of material and the increase of material cost.
Therefore, how effectively to simplify processing procedure, to shorten process time and processing cost, simultaneously, also can reduce waste and the material cost of material, become relevant dealer's effort target.
Summary of the invention
The object of the present invention is to provide and a kind ofly can simplify processing procedure, can also reduce the manufacture method of the tabular fibre strengthening product of waste of material simultaneously.
The manufacture method of the tabular fibre strengthening product of the present invention, comprise the following step: (A) prepare first a fibre strengthening material, and second fibre strengthening material, this the first fibre strengthening material has at least one first perforation, (B) this first fibre strengthening material and this second fibre strengthening material are laminated in the mould, this mould has a protuberance that can be placed through in this first perforation, and (C) heat this mould and this first fibre strengthening material that is laminated in this mould is combined with this second fibre strengthening material be hardened to a tabular fibre strengthening product, and certainly should take out by tabular fibre strengthening product in this mould, this tabular fibre strengthening product has one to depressed part that should the first perforation.
Another object of the present invention is to provide a kind of and can simplify processing procedure, can also reduce the manufacture method of the tabular fibre strengthening product of waste of material simultaneously.
The manufacture method of the tabular fibre strengthening product of the present invention, comprise the following step: (A) prepare first a fibre strengthening material, and second fibre strengthening material, this the first fibre strengthening material has at least one first perforation, (B) this first fibre strengthening material and this second fibre strengthening material are laminated into semi-finished product mutually, these semi-finished product have a body, and one to should first perforation and be formed at the shrinkage pool section of this body, (C) these semi-finished product are placed the mould that is heated to a forming temperature, make these semi-finished product in conjunction with being hardened to a tabular fibre strengthening product, this mould has a protuberance that can be placed through in this shrinkage pool section, and (D) should in this mould, take out by tabular fibre strengthening product, and this mould still is maintained at this forming temperature, and this tabular fibre strengthening product has one to depressed part that should shrinkage pool section.
The object of the invention to solve the technical problems also can be used in lower technical measures and further realize.
Preferably, the manufacture method of aforementioned tabular fibre strengthening product, wherein this second fibre strengthening material has second perforation that matches with the first perforation of this first fibre strengthening material, and the protuberance of this mould is to place this first perforation and this second perforation.
Preferably, the manufacture method of aforementioned tabular fibre strengthening product, wherein first of this first fibre strengthening material the perforation is identical with biperforate aperture of this second fibre strengthening material.
Preferably, the manufacture method of aforementioned tabular fibre strengthening product, wherein first of this first fibre strengthening material the perforation is different from biperforate aperture of this second fibre strengthening material.
Preferably, the manufacture method of aforementioned tabular fibre strengthening product, wherein this first fibre strengthening material and this second fibre strengthening material are to be selected from: carbon fiber, glass fibre, boron fibre or aramid fiber.
Preferably, the manufacture method of aforementioned tabular fibre strengthening product, wherein this forming temperature is between 120 ℃ to 200 ℃.
Beneficial effect of the present invention is: utilize the first mutually stacked fibre strengthening material and the second fibre strengthening material, the protuberance that cooperates this mould, and then straight forming goes out to have the tabular fibre strengthening product of this depressed part, not only can simplify processing procedure to shorten processing procedure time and processing cost, the waste that can also reduce material simultaneously and the generation of waste material are with the reduction material cost.
Description of drawings
Fig. 1 is a flow chart, and the manufacture method of existing tabular carbon fiber-reinforced product is described.
Fig. 2 is a schematic diagram, aid illustration Fig. 1.
Fig. 3 is a flow chart, and the first preferred embodiment of the manufacture method of the tabular carbon fiber-reinforced product of the present invention is described.
Fig. 4 is a schematic diagram, aid illustration Fig. 3.
Fig. 5 is a schematic diagram, and the second preferred embodiment of the manufacture method of the tabular carbon fiber-reinforced product of the present invention is described.
Fig. 6 is a schematic diagram, and the 3rd preferred embodiment of the manufacture method of the tabular carbon fiber-reinforced product of the present invention is described.
Fig. 7 is a schematic diagram, and the 4th preferred embodiment of the manufacture method of the tabular carbon fiber-reinforced product of the present invention is described.
Fig. 8 is a flow chart, and the 5th preferred embodiment of the manufacture method of the tabular carbon fiber-reinforced product of the present invention is described.
Fig. 9 is a schematic diagram, aid illustration Fig. 8.
The specific embodiment
The present invention is described in detail below in conjunction with drawings and Examples.
Before the present invention is described in detail, be noted that in the following description content, similarly assembly is to represent with identical numbering.
Consult Fig. 3,4, the first preferred embodiment of the manufacture method of the tabular fibre strengthening product 400 of the present invention, at first, shown in step 21, prepare one first fibre strengthening material 200, and one second fibre strengthening material 202, this first fibre strengthening material 200 has one first perforation 201.This first fibre strengthening material 200 is to be selected from this second fibre strengthening material 202: carbon fiber, glass fibre, boron fibre or aramid fiber, in the present embodiment, this first fibre strengthening material 200 is the carbon fibers that contain epoxy resin dipping with this second fibre strengthening material 202.
Next, shown in step 22, this first fibre strengthening material 200 is laminated in the mould 300 with this second fibre strengthening material 202, this mould 300 has a protuberance 301 that can be placed through in this first perforation 201.
Then, shown in step 23, heating this mould 300 makes this first fibre strengthening material 200 that is laminated in this mould 300 be hardened to a tabular fibre strengthening product 400 with these the second fibre strengthening material 202 combinations, and certainly should take out by tabular fibre strengthening product 400 in this mould 300, this tabular fibre strengthening product 400 has a pair of depressed part 401 that should the first perforation 201.In the present embodiment, this depressed part 401 is the kenels that are a groove.
Utilize the first mutually stacked fibre strengthening material 200 and the second fibre strengthening material 202, cooperate this mould 300 to have to be placed through the protuberance 301 in the first perforation 201 of this first fibre strengthening material 200, and then straight forming goes out to have the tabular fibre strengthening product 400 of this depressed part 401, not only can simplify processing procedure to shorten processing procedure time and processing cost, the waste that can also reduce material simultaneously and the generation of processing waste material are with the reduction material cost.
Consult Fig. 5, the second preferred embodiment of the manufacture method of the tabular fibre strengthening product 400 of the present invention, roughly be similar to this first preferred embodiment, different places are: this second fibre strengthening material 202 has one and matches with the first perforation 201 of this first fibre strengthening material 200 and the aperture is identical the second perforation 203, and the protuberance 301 of this mould 300 is to place this first perforation 201 and this second perforation 203.Make this tabular fibre strengthening product 400 that molds have a pair of should first perforation 201 and this second perforation 203, and be the depressed part 401 of through hole kenel.
Consult Fig. 6, the 3rd preferred embodiment of the manufacture method of the tabular fibre strengthening product 400 of the present invention, roughly be similar to this first preferred embodiment, different places are: this second fibre strengthening material 202 has one and matches from the first perforation 201 of this first fibre strengthening material 200 and the aperture is different the second perforation 203, and the protuberance 301 of this mould 300 is to place this first perforation 201 and this second perforation 203.Make this tabular fibre strengthening product 400 that molds have a pair of should first perforation 201 and this second perforation 203, and be the depressed part 401 of shoulder hole kenel.
Consult Fig. 7, the 4th preferred embodiment of the manufacture method of the tabular fibre strengthening product 400 of the present invention, roughly be similar to this first preferred embodiment, different places are: this first fibre strengthening material 200 has several the first perforation 201, and this mould 300 has several and is placed through the protuberance 301 of described the first perforation in 201.Make this tabular fibre strengthening product 400 that molds have several to should first perforation 201, and be the depressed part 401 of groove kenel.
Consult Fig. 8,9, the 5th preferred embodiment of the manufacture method of the tabular fibre strengthening product 400 of the present invention, at first, shown in step 31, prepare one first fibre strengthening material 200, and one second fibre strengthening material 202, this first fibre strengthening material 200 has one first perforation 201.In the present embodiment, this first fibre strengthening material 200 is the carbon fibers that contain epoxy resin dipping with this second fibre strengthening material 202.
Next, shown in step 32, this the first fibre strengthening material 200 and this second fibre strengthening material 202 are laminated into semi-finished product 204 mutually, and these semi-finished product 204 have a body 205, and a pair of should the first perforation 201 and be formed at the shrinkage pool section 206 of this body 205.
Then, shown in step 33, these semi-finished product 204 are placed the mould 300 that is heated to a forming temperature, make these semi-finished product 204 be hardened to a tabular fibre strengthening product 400, this mould 300 has a protuberance 301 that can be placed through in this shrinkage pool section 206, makes this tabular fibre strengthening product 400 that molds have a pair of depressed part 401 that should shrinkage pool section 206.The forming temperature of this mould 300 is between 120 ℃ to 200 ℃.In this preferred embodiment, the forming temperature of this mould 300 is between 150 ℃ to 180 ℃.
Then, shown in step 34, should in this mould 300, take out by tabular fibre strengthening product 400, and this mould 300 still is maintained at this forming temperature.
Because this preferred embodiment roughly is similar to this first preferred embodiment, therefore, except producing the effect identical with this first preferred embodiment, because this mould 300 is to continue to maintain this forming temperature, not only can reduce Repeat-heating and the time of cooling off this mould 300, more can avoid simultaneously in the first fibre strengthening material 200 and this second fibre strengthening material 202 adhesive agent (for example: epoxy resin) residual, save the cleaning time of this mould 300, therefore, more can significantly shorten manufacturing time and then lifting production capacity.
What this will specify be, for convenience of description, above-mentioned preferred embodiment all is to explain with one first fibre strengthening material 200 and one second fibre strengthening material 202, and in practical application, visual demand is adjusted the quantity of this first fibre strengthening material 200 and this second fibre strengthening material 202.
In sum, the manufacture method of the tabular fibre strengthening product 400 of the present invention, utilize the first mutually stacked fibre strengthening material 200 and the second fibre strengthening material 202, cooperate this mould 300 to have to be placed through the protuberance 301 in the first perforation 201 of this first fibre strengthening material 200, and then straight forming goes out to have the tabular fibre strengthening product 400 of this depressed part 401, not only can simplify processing procedure to shorten processing procedure time and processing cost, the waste that can also reduce simultaneously material and the generation of processing waste material are with the reduction material cost, so really can reach purpose of the present invention.
Claims (10)
1. the manufacture method of a tabular fibre strengthening product is characterized in that:
This manufacture method comprises: (A) prepare first a fibre strengthening material, and second fibre strengthening material, this the first fibre strengthening material has at least one first perforation, (B) this first fibre strengthening material and this second fibre strengthening material are laminated in the mould, this mould has a protuberance that can be placed through in this first perforation, and (C) heat this mould and this first fibre strengthening material that is laminated in this mould is combined with this second fibre strengthening material be hardened to a tabular fibre strengthening product, and certainly should take out by tabular fibre strengthening product in this mould, this tabular fibre strengthening product has one to depressed part that should the first perforation.
2. the manufacture method of described tabular fibre strengthening product according to claim 1, it is characterized in that: this second fibre strengthening material has second perforation that matches with the first perforation of this first fibre strengthening material, and the protuberance of this mould is to place this first perforation and this second perforation.
3. the manufacture method of described tabular fibre strengthening product according to claim 2, it is characterized in that: the first perforation of this first fibre strengthening material is identical with biperforate aperture of this second fibre strengthening material.
4. the manufacture method of described tabular fibre strengthening product according to claim 2, it is characterized in that: the first perforation of this first fibre strengthening material is different from biperforate aperture of this second fibre strengthening material.
5. the manufacture method of the described tabular fibre strengthening product of arbitrary claim in 4 according to claim 1, it is characterized in that: this first fibre strengthening material and this second fibre strengthening material are to be selected from: carbon fiber, glass fibre, boron fibre or aramid fiber.
6. the manufacture method of a tabular fibre strengthening product is characterized in that:
This manufacture method comprises: (A) prepare first a fibre strengthening material, and second fibre strengthening material, this the first fibre strengthening material has at least one first perforation, (B) this first fibre strengthening material and this second fibre strengthening material are laminated into semi-finished product mutually, these semi-finished product have a body, and one to should first perforation and be formed at the shrinkage pool section of this body, (C) these semi-finished product are placed the mould that is heated to a forming temperature, make these semi-finished product in conjunction with being hardened to a tabular fibre strengthening product, this mould has a protuberance that can be placed through in this shrinkage pool section, and (D) should in this mould, take out by tabular fibre strengthening product, and this mould still is maintained at this forming temperature, and this tabular fibre strengthening product has one to depressed part that should shrinkage pool section.
7. the manufacture method of described tabular fibre strengthening product according to claim 6, it is characterized in that: this second fibre strengthening material has second perforation that matches with the first perforation of this first fibre strengthening material, and the protuberance of this mould is to place this first perforation and this second perforation.
8. the manufacture method of described tabular fibre strengthening product according to claim 7, it is characterized in that: the first perforation of this first fibre strengthening material is different from biperforate aperture of this second fibre strengthening material.
9. the manufacture method of described tabular fibre strengthening product according to claim 7, it is characterized in that: the first perforation of this first fibre strengthening material is identical with biperforate aperture of this second fibre strengthening material.
10. according to claim 6 to the manufacture method of the described tabular fibre strengthening product of 9 arbitrary claims, it is characterized in that: this forming temperature is between 120 ℃ to 200 ℃.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210058016.9A CN103302843B (en) | 2012-03-07 | 2012-03-07 | The manufacture method of tabular fibre-reinforced products |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210058016.9A CN103302843B (en) | 2012-03-07 | 2012-03-07 | The manufacture method of tabular fibre-reinforced products |
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| Publication Number | Publication Date |
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| CN103302843A true CN103302843A (en) | 2013-09-18 |
| CN103302843B CN103302843B (en) | 2015-08-05 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201210058016.9A Expired - Fee Related CN103302843B (en) | 2012-03-07 | 2012-03-07 | The manufacture method of tabular fibre-reinforced products |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108162513A (en) * | 2016-08-10 | 2018-06-15 | 安徽美沃门窗科技有限公司 | A kind of manufacturing method of the bottom plate of window heat preservation platen |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04282224A (en) * | 1991-03-12 | 1992-10-07 | Matsushita Electric Ind Co Ltd | Air-pressure forming apparatus |
| JPH04284225A (en) * | 1991-03-13 | 1992-10-08 | Nitto Boseki Co Ltd | Molding method for fiber reinforced resin composite material |
| EP0634265A1 (en) * | 1993-07-14 | 1995-01-18 | General Electric Company | Thermoforming process |
| CN101417504A (en) * | 2008-11-25 | 2009-04-29 | 王赞山 | A kind of vacuum suction moulding technology |
| CN102211402A (en) * | 2011-05-23 | 2011-10-12 | 天津大学 | Fiber and surface-reinforced thermosetting foam plastic waste plate and preparation method thereof |
-
2012
- 2012-03-07 CN CN201210058016.9A patent/CN103302843B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04282224A (en) * | 1991-03-12 | 1992-10-07 | Matsushita Electric Ind Co Ltd | Air-pressure forming apparatus |
| JPH04284225A (en) * | 1991-03-13 | 1992-10-08 | Nitto Boseki Co Ltd | Molding method for fiber reinforced resin composite material |
| EP0634265A1 (en) * | 1993-07-14 | 1995-01-18 | General Electric Company | Thermoforming process |
| CN101417504A (en) * | 2008-11-25 | 2009-04-29 | 王赞山 | A kind of vacuum suction moulding technology |
| CN102211402A (en) * | 2011-05-23 | 2011-10-12 | 天津大学 | Fiber and surface-reinforced thermosetting foam plastic waste plate and preparation method thereof |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108162513A (en) * | 2016-08-10 | 2018-06-15 | 安徽美沃门窗科技有限公司 | A kind of manufacturing method of the bottom plate of window heat preservation platen |
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| CN103302843B (en) | 2015-08-05 |
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