KR20170096667A - Impregnation die for preparing unidirectional prepreg of fiber-reinforced thermoplastic resin - Google Patents
Impregnation die for preparing unidirectional prepreg of fiber-reinforced thermoplastic resin Download PDFInfo
- Publication number
- KR20170096667A KR20170096667A KR1020160018060A KR20160018060A KR20170096667A KR 20170096667 A KR20170096667 A KR 20170096667A KR 1020160018060 A KR1020160018060 A KR 1020160018060A KR 20160018060 A KR20160018060 A KR 20160018060A KR 20170096667 A KR20170096667 A KR 20170096667A
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- KR
- South Korea
- Prior art keywords
- prepreg
- fiber
- impregnation die
- thermoplastic resin
- reinforced thermoplastic
- Prior art date
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Classifications
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- 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
- B29C70/506—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands and impregnating by melting a solid material, e.g. sheet, powder, fibres
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
-
- 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
-
- 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
- B29C70/525—Component parts, details or accessories; Auxiliary operations
- B29C70/526—Pultrusion dies, e.g. dies with moving or rotating parts
-
- 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impregnation die for producing a unidirectional (UD) prepreg of a fiber-reinforced thermoplastic resin, and more particularly, to a method of molding a unidirectional prepreg, To a novel impregnation die for forming a unidirectional prepreg which is capable of increasing the width of the fiber and preventing the splitting between fibers to maintain the sheet shape of the prepreg by deforming the internal structure of the impregnation die for production to a bent shape .
The fiber-reinforced thermoplastic resin is lightweight and has excellent strength and is used in various industrial fields such as automobiles and electronic devices.
Prepregs for using such a fiber-reinforced thermoplastic resin are prepared by film lamination, impregnation die, and in-situ polymerization.
Among these methods, a film laminating process or an impregnating die is used in the case of a unidirectional prepreg (UD-prepreg). In the case of film laminating, a film manufacturing process is further required. In the case of using an impregnating die, The width of the product is not wide.
Thermoplastic resins having a higher viscosity than thermosetting resins have been subjected to various methods for achieving uniform fiber impregnation properties that affect quality and appearance due to their high viscosity characteristics. In particular, the prepreg of a thermoplastic resin may be required as a requirement that the expansion in the width direction is required depending on the application field.
However, it is known that the thermoplastic resin is difficult to maintain the shape of the prepreg because of the problem of splitting when it expands in the width direction in the process of discharging through the outlet of the impregnation die due to the relatively high viscosity.
Japanese Laid-Open Patent Application No. 1995-205307 discloses a method for forming a prepreg in a desired cross-sectional shape while running while running a long prepreg made of a thermoplastic resin containing reinforcing fibers such as carbon fibers, Wherein the molding die is continuous from the prepreg inlet to the prepreg outlet while the prepreg traveling passage is wound around the heating portion and the inside of the cooling portion respectively.
However, also in such a case, there is a problem in that splitting between fibers can not be avoided in the process of expanding in the width direction in the process of being discharged to the outlet of the impregnation die.
In order to solve the problems of the prior art as described above, it is an object of the present invention to manufacture a prepreg expanded in the width direction while preventing the splits appearing at the time of manufacturing the prepreg using the impregnation die of the fiber-reinforced thermoplastic resin.
It is therefore an object of the present invention to provide a impregnation die of a new structure which prevents the split from occurring while increasing the opening width of the fiber during preparation of the prepreg of the fiber reinforced thermoplastic resin.
In order to solve the above problems, the present invention provides an impregnation die for preparing a prepreg of a fiber-reinforced thermoplastic resin, wherein a prepreg discharge portion of the impregnation die is formed so as to have a concave- Provided is an impregnation die structure for manufacturing a unidirectional (UD) prepreg.
According to the present invention, the inner surface of the prepreg discharge portion of the impregnation die for preparing the prepreg of the fiber-reinforced thermoplastic resin is formed into a concave-convex shape so that the lip portion of the impregnation die for preparing the prepreg of the fiber- It is possible to manufacture a prepreg having a wide fiber width discharged from the impregnation die through an increase in the number of fibers while preventing a splitting phenomenon of the fiber even with a simple shape change to the discharge port .
1 is a schematic diagram conceptually showing the structure of a general unidirectional prepreg-producing impregnation die.
FIG. 2 is a conceptual view showing a splitting structure of fibers when the fiber width is increased when the impregnated die prepreg is manufactured in a conventional shape.
FIG. 3A illustrates an embodiment of the shape of the prepreg discharge portion of the impregnation die having the concavo-convex curved surface according to the present invention. In the case of the fiber having passed through the impregnation die, the prepreg is manufactured to have a wide width without splitting It is a conceptual drawing.
FIG. 3B is a view illustrating another embodiment of the shape of the prepreg discharge portion of the impregnation die having the concavo-convex curved surface according to the present invention.
FIG. 4A is a view showing the structure of the discharging portion of the impregnation die applied in the comparative example according to the present invention.
4B-4D are views showing various forms of an improved discharge structure of an impregnation die applied in an embodiment according to the present invention.
5A is a photograph of the appearance of a prepreg produced according to a comparative example of the present invention.
Figure 5b is a photograph of the appearance of a prepreg produced in accordance with an embodiment of the present invention.
Hereinafter, the present invention will be described in more detail as an embodiment.
In the impregnation die for producing a unidirectional prepreg of a fiber-reinforced thermoplastic resin, the prepreg discharge portion of the impregnation die has a protruding portion formed on the inner surface of the discharge portion, and the inner surface of the prepreg discharge portion is formed into a concave- ≪ / RTI >
Generally, an impregnation die is used to prepare a fiber-reinforced thermoplastic resin as a unidirectional prepreg. In this case, there is a disadvantage in that the fiber opening width of the fiber produced after passing through the resin outlet of the impregnation die is not wide. The reason for this is that the viscosity of the thermoplastic resin is high. For this purpose, impregnation dies of the type shown in Fig. 1 are used to ensure uniform impregnation properties affecting quality and appearance.
The impregnation die to which the present invention is applied has a
2, the
According to a preferred embodiment of the present invention, the
As described in the present invention, when the impregnated die
Figure 3a illustrates one embodiment of the shape of the
The present invention is characterized in that a convex-and-concave structure is formed on the
Other prepreg discharging units constructed by the method similar to that of FIG. 3A of the present invention may be configured as shown in FIG. 3B. The structure of FIG. 3B can be used in a more advanced structure as a preferred embodiment of the present invention.
The concavo-convex structure of the
As a result, it is surprising that there is a remarkable effect that the opening width of the prepreg is kept wide and splits do not occur between the fibers.
According to a preferred embodiment of the present invention, the uneven surface may have a structure in which 2 to 6, more preferably 2 to 4, projections are formed in a zigzag shape on the inner surface of the discharge portion. These protrusions are more preferably formed at regular intervals.
The impregnation die structure according to the present invention exhibits a very good effect while simply changing the conventional impregnation die structure.
That is, according to the present invention, when the impregnation die is applied, the resin can be impregnated into the fiber more easily by simply changing the internal surface structure of the discharge portion in which the resin is impregnated into the fiber, The fiber width reduction phenomenon of the prepreg can be prevented.
In the preparation of a prepreg using a known impregnation die having a known structure, the input fiber has a reduced opening width due to the pressure and viscosity of the resin to be injected, and a split occurs between the fibers and the fibers. Further, when the number of fibers is increased to expand the width of the single prepreg, it is difficult to maintain the sheet form of the prepreg.
According to the present invention, by using the existing impregnation die as it is and by newly constructing the internal structure of the pregreg discharge portion (Lip) of the impregnation die, the opening width of each fiber is increased while expanding the width through additional opening after resin impregnation It is possible to prevent split between fibers and to maintain the shape of the prepreg sheet.
Hereinafter, the present invention will be described by way of examples, but the present invention is not limited by the examples.
Comparative Example, Examples 1 to 3
4 (a) and 4 (d), the impregnation die having a basic structure having a shape as shown in Fig. 1 is used, For the case of four protrusions, prepreg sheets were produced under the same conditions by using three types of discharge port structures (Examples 1 to 3) having different height and protrusion shapes.
The preparation of such a prepreg is a fiber-reinforced thermoplastic composite material containing carbon fibers, and a polycarbonate resin is impregnated with a prepreg sheet (width: 300 mm) using an impregnation die (size: 540 mm in width, Or more).
As a result, in comparison between the case of using the impregnating die having the structure of FIG. 4A and the case of using the impregnating die of the structure of FIG. 4B to FIG. 4D, the prepregs of FIGS. 4B to 4D (Examples 1 to 3) All of the prepregs were produced without splitting, and the appearance was improved. In the case of FIG. 4A (comparative example), however, splitting occurred.
In order to compare the results, the comparison results of the photographs of the prepregs prepared according to the comparative example and the example 1 are shown in FIGS. 5A and 5B, respectively.
10 - Fiber inlet
20 - resin inlet
30 - Fiber Groove Groove
40, 400 - prepreg discharge portion
410 - Inner side of outlet
420 - protrusion
50, 500 - prepreg
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020160018060A KR20170096667A (en) | 2016-02-16 | 2016-02-16 | Impregnation die for preparing unidirectional prepreg of fiber-reinforced thermoplastic resin |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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KR1020160018060A KR20170096667A (en) | 2016-02-16 | 2016-02-16 | Impregnation die for preparing unidirectional prepreg of fiber-reinforced thermoplastic resin |
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KR20170096667A true KR20170096667A (en) | 2017-08-25 |
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KR1020160018060A KR20170096667A (en) | 2016-02-16 | 2016-02-16 | Impregnation die for preparing unidirectional prepreg of fiber-reinforced thermoplastic resin |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20190115146A (en) * | 2018-03-30 | 2019-10-11 | 주식회사 이지컴퍼지트 | Apparatus for manufacturing tow prepreg and method for the same |
KR20230071982A (en) | 2021-11-17 | 2023-05-24 | (주)엘엑스하우시스 | Width adjustment guide device, apparatus and method of manufacturing continuous fiber composite having the same |
-
2016
- 2016-02-16 KR KR1020160018060A patent/KR20170096667A/en unknown
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20190115146A (en) * | 2018-03-30 | 2019-10-11 | 주식회사 이지컴퍼지트 | Apparatus for manufacturing tow prepreg and method for the same |
KR20230071982A (en) | 2021-11-17 | 2023-05-24 | (주)엘엑스하우시스 | Width adjustment guide device, apparatus and method of manufacturing continuous fiber composite having the same |
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