Compression molding of composite parts on hot mold surfaces with a short cycle time.
Abstract
A molding system is provided comprising a cold mold with a large thermal mass and contoured thin mold inserts (15,17) with a low thermal mass. A composite sheet blank (11) of glass fibers in a thermoplastic matrix resin is placed between the inserts, heated and then transported to the cold mold. The composite sheet is pressed in the cold mold between the mold inserts to flow form and then cool the part. The mold inserts keep the surfaces of the composite sheet hot during the forming process, thereby enabling the matrix resin to flow and form smooth surfaces.

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Projected expiry passed 20 February 2009, 17.6 years ago.
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15 claims: 3 independent, 12 dependent
- 1A method of compression molding reinforced thermoplastic composite sheets to obtain a smooth surface finish and short cycle time comprising the steps of:heating the composite sheet above the temperature at which the matrix material in the composite sheet becomes molten;heating a mold insert having the desired contour of the molded composite sheet;transporting the composite sheet on the mold insert to a cooled mold;placing the mold insert and composite sheet in the mold, the thermal mass of the insert being much less than the lower half of the mold;closing the mold, the composite sheet and insert having been heated sufficiently and the insert having sufficient thermal mass to allow the thermoplastic resin to flow and fill the mold insert;allowing the molded composite sheet to cool;and opening the mold and removing the molded composite sheet and the mold insert.
- 6A method of compression molding a reinforced thermoplastic sheet to obtain a smooth surface finish and short cycle time, comprising the steps of:placing the composite sheet between mold inserts having the desired contour of the molded composite sheet;heating the composite sheet and mold inserts above the temperature at which the matrix material in the composite sheet becomes molten;transporting the composite sheet between the mold inserts to a cooled mold;placing the mold inserts and composite sheet in the mold, the thermal mass of the inserts being much less than the upper and lower mold halves the inserts are situated between in the mold;closing the press, the composite sheet and inserts, having been heated sufficiently and the inserts having sufficient thermal mass to allow the thermoplastic resin to flow and fill the mold inserts;allowing the molded composite sheet to cool;and opening the press and removing the molded composite sheet and the mold inserts.
- 11A method of compression molding a reinforced thermoplastic composite sheet to obtain a smooth surface finish and short cycle time comprising the steps of:heating the composite sheet above the temperature at which the matrix material in the composite sheet becomes molten;heating a pair of mold inserts having the desired contour of the molded composite sheet;placing the composite sheet between the inserts;transporting the composite sheets between the pair of mold inserts to a cooled mold;placing the mold inserts and composite sheet in the mold, the thermal mass of the insert being much less than the upper and lower mold halves the inserts are situated between in the mold;closing the press, the composite sheet and inserts having been heated sufficiently and the inserts having sufficient thermal mass to allow the thermoplastic resin to flow and fill the mold inserts;allowing the molded composite sheet to cool;and opening the mold and removing the molded composite sheet and mold inserts.
Independent claims3
35 paragraphs, as filed
Cross Reference to Related Applications
0001This application is related to copending application entitled "Multilayer Composite Mold Structure for Molding on Hot Surfaces", Serial No. (RD-18,414), and "Compression Molding Using Insulating Films", Serial No. (RD-18,364) both assigned to the same assignee as the present invention.
Background of the Invention
0002The present invention is related to a method for compression molding plastics.
0003Compression molding of glass reinforced thermoplastic sheets is a promising method for producing relatively thin, wide and strong parts such as car hoods, doors and panels. One important prerequisite for the use of glass reinforced composite products in automobile applications is a Class A surface. While there is no universally accepted specification, the Class A surface is a glossy, smooth and polished surface which should be as smooth as that of current automobile exterior parts made from sheet metal.
0004Current molding processes of glass reinforced thermoplastic composite sheets begins with the heating composite blanks in an oven, typically in infrared or hot air convection ovens. The material is heated above its melting point or if an amorphous material at least substantially above its glass transition temperature. The hot blanks are then pressed between cool mold surfaces (surfaces lower than the melting point or the glass transition temperatures), which are typically 175°-250°F. A molding pressure of one half ton/sq. in. to two tons/sq. in. is applied to the mold during a typical cycle time of 45-60 seconds.
0005When the composite blanks are heated, they expand (loft) due to the recoil forces within the fibers. The surface of the expanded blanks then cools during its transfer to the mold, resulting in "frozen" resins on the surface. Compression of this blank in the cool mold produces surfaces which are not completely filled with resins, although some hot molten material moves from the inner core to the surface. This creates unfilled areas in the form of exposed fibers and surface porosity or voids. Since the resin at the cold surface is frozen and does not flow, rough boundaries between charged and newly formed areas are also produced. These exposed fibers, porous areas and blank boundaries are the major manifestations of surface roughness, although other physical processes, such as differential thermal shrinkage between fibers and resins, can also result in surface roughness and/or waviness.
0006Recently it has been found that smooth surfaces can be obtained from neat resin in blow molding by using hot surface molding. The resin is supplied hot to the mold as a parison in blow molding or injected into the mold in injection molding. These techniques, which are based on temperature cycling of mold surfaces, increase the cycle time of the process. The increased cycle time is the major disadvantage of these techniques. In addition, composite sheets with continuous mat fibers cannot easily be injected or supplied as a parison. Heating of composite sheets causes the fibers to loft and extend outside the polymer resin matrix. Attempts to obtain smooth surfaces with composite sheets have involved trying to change the structure of the composite sheets so that the outside layers on the composite sheets have neat resin with barrier layers sometimes being provided to prevent the fibers situated in the middle layers from coming to the surface. These sheets could then be molded using conventional compression molding techniques.
0007It is an object of the present invention to provide a method of compression molding reinforced thermoplastic composite sheets which result in finished products with smooth surfaces, a minimum of exposed fiber, porosity, and blank boundaries.
0008It is a further object of the present invention to provide a method of compression molding reinforced and thermoplastic parts which results in short cycle times and therefore increased throughput for each press.
0009It is still a further object of the present invention to provide a method of compression molding reinforced thermoplastic composite sheets which reduces the required molding pressure and therefore reduces press size, which is particularly significant in large fabrication.
0010It is another object of the present invention to provide a method of compression molding reinforced thermoplastic which results in reduced thermal decomposition of the thermoplastic resins.
0011It is yet another object of the present invention to provide a method of compression molding reinforced thermoplastic sheets which preserve the original sheet structure after molding.
Summary of the Invention
0012In one aspect of the present invention a method of compression molding reinforced thermoplastic composite sheets to obtain smooth surface finishes and short cycle times is provided. The method comprises the steps of heating the composite sheet above the temperature which the matrix material in the composite sheet becomes molten and heating a mold insert having the desired contour of the molded composite sheet. The heated composite sheet is placed on the heated mold insert and transported on the mold insert to a cooled mold. The mold insert and composite sheet are placed in the mold with the thermal mass of the insert being much less than the bottom half of the mold upon which it is placed. The mold is then closed, the composite sheet and insert having been heated sufficiently and the insert having sufficient thermal mass to allow the thermoplastic resin to flow and fill the insert. The molded composite sheet is allowed to cool inside the mold. The mold is then opened with the molded composite sheet as well as the mold insert removed.
Brief Description of the Drawing
0013The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the concluding portion of the specification. The invention however, both as to organization and method of practice, together with further objects and advantages thereof, may be best understood by reference to the following description taken in conjunction with the accompanying figures in which: <ul id="ul0001" list-style="none"><li>Figure 1 is an isometric representation of the steps of compression molding reinforced thermoplastic composite sheets to obtain smooth surface finishes in accordance with the present invention;</li><li>Figure 2 is an isometric representation of another embodiment of the method of compression molding reinforced composite sheets in accordance with the present invention;</li><li>Figure 3 is a graph of the transient temperature profile of heated 1/8" mold inserts surrounding a heated composite blank in a compression mold immediately after mold closing;</li><li>Figure 4 is a graph showing a comparison of the calculated surface temperature decay of a composite material containing a crystalline polymer after mold closing, when molded in a cool mold press and when molded cold mold press with heated inserts;</li><li>Figure 5 is a graph showing a comparison of the calculated temperature decay comparison at the centerline of a composite material containing an amorphous polymer after mold closing, when molded in a cool mold press and when molded in a cold mold press with heated inserts;</li><li>Figure 6 is a graph of the required mold pressure per square inch for different amounts of blank elongation for a cool mold and a cold mold using heated inserts; and</li><li>Figures 7A-G are an isometric representation of another embodiment of the steps of compression molding reinforced thermoplastic in accordance with the present invention.</li></ul>
Detailed Description of the Invention
0014Referring now to the drawing and and particularly Figure 1 thereof. A composite sheet 11 comprising thermoplastic resin, including reinforcing layers, is shown being preheated to approximately the glass transition temperature of the resin in an oven 13. Oven 13 can comprise a convection oven as shown or an infrared oven. Preheating allows the sheet 11 to soften to conform to the contours of mold inserts 15 and 17 when it is placed between the two thin mold inserts. The composite sheet can comprise, for example, approximately 30-40% glass fiber mat and 70-60% polymer resin. The glass fiber mats can be fabricated from continuous strands sized with a sizing compatible with a matrix resin being used. Depending on the application, a variety of polymer matrices such as polycarbonate, polyesters, polypropylene, polyamide polyimides, polyphenylene oxide, polystyrene and blends of the above can be used. The mold inserts 15 and 17 with the sheet 11 in between are then further heated above the temperature at which the matrix material in the composite sheet becomes molten, preferably by conduction heating between plates 21 and 23 containing heating elements 25. The temperature of the sheet will exceed the glass transition temperature if an amorphous resin is being used or exceed the melting point if a crystalline resin is being used. The mold inserts 15 and 17 can be fabricated from a material which can withstand the compression forces at elevated temperatures at which the composite material melts without distorting and has a smooth surface for shaping the composite materials. Examples of such materials are metals, ceramics, high temperature plastics, plastic composites. Conduction heating of the mold inserts is preferred over convection or infrared heating because of the faster heat transfer. The inserts with the sheet in between are transported then to a press 22 and between the cold upper and lower mold halves of a cold press 27 and compressed. The mold halves can comprise tool steel or to reduce cost can comprise a softer less expensive material such as aluminum on plastic composites. Since the mold inserts are used in direct contact with the composite, the mold halves are not subjected to wear by the material to be molded. The mold halves with which the hot inserts come in contact are maintained at approximately 100°F by liquid cooling through passageways (not shown) in the mold halves, not shown. Initially, the resins in contact with the hot mold inserts remain molten and fill the insert mold surface under pressure. The composite part and mold inserts cool in the cooled mold halves. The composite product is released from the mold inserts and the mold inserts reused. If only one smooth surface is required, one mold insert may be sufficient. The optimum thickness of the mold insert is determined by the minimum mass required to provide hot surfaces, the cooling time desired and the mechanical strength needed to withstand the compression molding process.
0015Another embodiment of the present invention is shown in Figure 2. A composite sheet blank 31 and mold inserts 33 and 35 are heated separately. The blank may be heated in a infrared or convection oven above the temperature which the matrix material in the sheet becomes molten, which is above the melting point of the resin if a crystalline material is used or above the glass transition temperature if an amorphous material is used. A tunnel convection oven 37 is shown providing a steady supply of heated blanks. Heating the blanks allows the glass fibers to loft. The blank is then placed between preheated inserts which have been heated between plates 41 and 43 containing heating elements 45. The inserts and blank are transported to a cooled press 47 and compressed. The mold inserts 33 and 35 are shown with a varying wall thickness profile which simplifies the design of the molding system. It has been found that a simple shape can be used at the interface between the cold mold halves 48 and 49 and the mold inserts based on tests of mold inserts with different wall thicknesses. Varying thickness mold inserts resulted in good resin flow and filling of resins at the surface of the part molded. The composite was free of exposed fibers, porosity and blank boundaries. The surface of the molded part was a reproduction of that of the mold insert.
0016The surfaces of composite parts distributed fibers throughout the sheet produced by hot surface molding of composite sheets with a uniformly were analyzed using a mechanical profilometer (Feinpruef Model M4P). Table 1 shows the comparison of the average roughness and the peak-to-valley height of composite parts produced by hot surface molding and cold surface molding. Samples made by hot surface molding with fine fibers and coarse fibers had average roughness of 8.4 and 9.4 microinches and peak to valley height of 65 and 78 microinches. Compared to values of 30 on 47.5 microinches for average roughness and 400 and 450 microinches for peak-valley height on parts made by the cold surface molding, it is a significant improvement in surface roughness. The significant reduction in surface roughness is due to elimination of imperfections such as exposed fibers, porosity and voids at the surfaces.
0017The shape of the contact area between the mold inserts and the cold mold halves is important because of the thermal shrinkage that occurs to the mold inserts when cooling. Since the shape of the portion of the mold insert contacting the mold halves does not have to conform exactly to the mold insert contours, a simple geometry which provides good contact between the cold mold halves and surface element can be used. <tables id="tabl0001" num="0001"><table frame="all"><title>TABLE 1</title><tgroup cols="3" colsep="1" rowsep="0"><colspec colnum="1" colname="col1" colwidth="52.50mm" /><colspec colnum="2" colname="col2" colwidth="52.50mm" /><colspec colnum="3" colname="col3" colwidth="52.50mm" /><thead valign="top"><row><entry namest="col1" nameend="col3" align="center">Comparison of Surface Roughness</entry></row><row><entry namest="col1" nameend="col1" align="left">Hot Surface Molding</entry><entry namest="col2" nameend="col2" align="center"><u style="single">Average Roughness (micro. in.)</u></entry><entry namest="col3" nameend="col3" align="center"><u style="single">Average Peak Valley Height (micro in.)</u></entry></row></thead><tbody valign="top"><row><entry namest="col1" nameend="col1" align="left">fine fiber composite</entry><entry namest="col2" nameend="col2" align="char" char=".">8.4</entry><entry namest="col3" nameend="col3" align="right">65</entry></row><row><entry namest="col1" nameend="col1" align="left">coarse fiber composite</entry><entry namest="col2" nameend="col2" align="char" char=".">9.4</entry><entry namest="col3" nameend="col3" align="right">78</entry></row></tbody></tgroup><tgroup cols="3" colsep="1" rowsep="0"><colspec colnum="1" colname="col1" colwidth="52.50mm" /><colspec colnum="2" colname="col2" colwidth="52.50mm" /><colspec colnum="3" colname="col3" colwidth="52.50mm" /><thead valign="top"><row><entry namest="col1" nameend="col1" align="left">Cold Surface Molding</entry><entry namest="col2" nameend="col2" /><entry namest="col3" nameend="col3" /></row></thead><tbody valign="top"><row><entry namest="col1" nameend="col1" align="left">fine fiber composite</entry><entry namest="col2" nameend="col2" align="char" char=".">30</entry><entry namest="col3" nameend="col3" align="right">400</entry></row><row rowsep="1"><entry namest="col1" nameend="col1" align="left">coarse fiber composite</entry><entry namest="col2" nameend="col2" align="char" char=".">47.5</entry><entry namest="col3" nameend="col3" align="right">450</entry></row></tbody></tgroup></table></tables>
0018A one dimensional transient heat transfer mathematical analysis was made on a multilayer system comprising five layers; mold/insert/composite/insert/mold. The heat transfer between the insert and the composite was assumed to take place by conduction. The temperature profile of a 1/8" composite sheet situated between two 1/8" metal mold inserts in contact with a cooled mold is shown in Figure 3. Dimensionless temperature was used in the calculations with dimensionless temperature defined by the ratio ((T-T<sub>c</sub>)/(T<sub>i</sub>-T<sub>c</sub>), where T, T<sub>i</sub> and T<sub>c</sub> stand for temperature as a function of time and location, initial temperature, and boundary temperature, respectively. A constant boundary condition was used where the mold inserts were assumed to be heated to 550°F (T<sub>i</sub>) and cooling fluid in the cooled mold, with which the mold inserts where in contact, provided a constant temperature of 100°F (T<sub>c</sub>) at a distance of 1/4 inch from the mold insert surface.
0019Thermal conductivities of composite sheets were measured for use in the calculations and the thermal conductivities of composites made with continuous fiber mats are much higher than both the neat resin and short fiber filled composites. The composites were assumed to have a 40% fiber mat content.
0020If the resin used as a matrix in the composite material is polybutylene terephthalate available from a General Electric Co. as Valox® thermoplastic with a melting point of 450°F, its dimensionless temperature is 0.8. Referring to the Fig. 3 the melting temperature is maintained at the mold insert surface for 0.6 seconds. The temperature of the resin further away from the metal surface is maintained above the melting point longer than 0.6 seconds. If a high speed press fills the mold surface with resin during this time period, the surface will be free of voids. Using a maximum temperature of 250°F as the desired final sheet temperature during cooling before release from the mold, cooling can be accomplished within 20 seconds. If the resin in the composite material is bisphenol A based polycarbonate an amorphous material with a glass transition temperature of 284°F, available from the General Electric Company as Lexan® 141 thermoplastic, the glass transition temperature is equivalent to 0.4 on the dimensionless temperature scale. A high speed press could fill the mold surface with resin during the period of time that the metal surface is maintained above the glass transition temperature and the surface will be free of voids. If a maximum temperature of 250° is again used as the desired final temperature during cooling before release from the mold, cooling can then be accomplished within 20 seconds. This indicates that the use of a hot mold insert fabricated from 1/8 inch metal sheets makes it possible to mold composite sheets free of voids.
0021A comparison of the calculated temperature decay of the surface of a composite sheet including a crystalline polymer in both a cold mold press with hot inserts and a cool surface press without inserts is shown in Figure 4. The temperature used in the calculations are 550°F for the preheat temperature of the composite sheet and mold inserts, 225°F for the mold surface temperature in the cool surface molding, and 100°F for the mold temperature of the cold mold into which the mold inserts are placed. Initially, the temperature of the metal surface in contact with the composite sheet during hot surface molding with hot mold inserts is much higher than during cool surface molding allowing increased flow time of the polymer resin assuming a smooth surface without voids.
0022Referring now to Figure 5 a comparison of the calculated temperature decay of the centerline of a composite sheet including a crystalline polymer in both a cold mold press with hot inserts and a cool surface press without inserts is shown. The temperatures use in the calculations are the same as used in connection with Figure 4, 550°F for the preheat temperature of the composite sheet and mold inserts, 225° for the mold surface temperature in the cool surface molding and 100°F for the mold temperature of the cold mold into which the mold inserts are placed. Initially, the temperature of the centerline of the composite material in the hot inserts and in the cool mold are the same. As cooling continues, the temperature in the middle of the composite in the hot surface molding process cools more rapidly than in the cool surface mold, showing that it is possible to have a shorter cycle time with the hot mold insert than with conventional cool surface molding.
0023The use of a thicker insert, 1/4 inch for example, does not result in much of an increase in cooling time (17-20 seconds in this case) when a mold insert fabricated of high thermoconductivity material such as metal is used. Increasing the composite thickness to 1/4 inch however, increases the cooling time to almost a minute, while the time the composite surface temperature remains higher than its melting temperature stays the same.
0024The temperature selected for the cooled mold can be in the range of 50° to 300°F. The lower the temperature the quicker the cycle time. However, for smooth surfaces the resin must be molten during press closing limiting the temperature selected. The cool mold temperatures in the upper part of the range are used with resins having high glass transition temperatures while the temperatures in the lower portion of the range are used with resins having low glass transition temperatures.
0025Referring now to Figure 6, the reduced pressure requirement in compression molding for hot surface mold inserts in a cold mold and a conventional cool mold is shown. For all the ratios of area of a part after compression molding to area of a part before compression molding, it is seen that the compression molding can be accomplished at reduced pressure when the hot surface insert mold technique is used. The reduced pressure requirement results from the higher composite sheet temperature in the early molding stages and resulting slow initial cooling at the composite surface.
0026Referring now to Figures 7A-G another embodiment of the present invention is shown. A single mold insert 51 is used as a carrier to transport a hot composite sheet 53 to the press 55. The composite sheet is heated above the temperature at which the resin used a matrix material becomes molten in an infrared or convection oven. A convection tunnel oven 57 is shown in the Figure. The single mold insert 51 is preferably heated by conduction heating between plates 59 and 61 which are heated by electrical resistance heating 63, for example. The heated sheet is then situated on the heated mold insert and transported to the press where it is placed on the fixed bed 65 of the press 55. The press 55 is shown with a two part movable head 67a and 67b. The press fixed bed and upper mold half core are cooled by cooling passages 69 carrying cooling liquid. As the press closes, as shown in Figure 7C, the first part of the movable head 67a, located on either side of the upper mold half 67b, contacts the mold insert 51, clamping it in place against the fixed bed of the press. The second part of the movable head 67b containing the upper mold half presses the sheet 53 as seen in Figure 7D. When the press opens as shown in Figure 7E, the shaped composite part 71 is lifted with the upper mold half, ejector pins 73 shown in Figure 7F in the upper mold half release the shaped composite part 71 which is shown in Figure 7G with its smooth defect free surface facing down. The mold insert is removed and used again.
0027The use of the mold insert to transport the heated sheet blank from the oven to the press is another important feature of this invention. Since the heated sheet blank is very flexible, a carrier which supports it, is required, particularly when transporting a large blank. The insert can be used as a carrier for this purpose.
0028Mold inserts in contact with the composite blank reduce surface cooling of the blank during its transfer from the oven to mold. While composites can be heated to a higher initial temperature to compensate for cooling which occurs when mold inserts are not used, thermal decomposition of the resin in the composite sheet will increase due to the longer heating times, higher temperatures, and increased exposure to air. The use of mold inserts allows plastics with a narrow operating ranges to be more easily accommodated.
0029The foregoing has described a method of compression molding reinforced thermoplastic composite sheets which result in finished products with smooth surfaces and a minimum of exposed fiber, porosity and blank boundaries. Parts can be formed using the present invention that require short cycle times and reduced molding pressure.
0030While the invention has been particularly shown and described with reference to several preferred embodiments thereof, it will be understood by those skilled in the art that various changes in form and detail may be made without departing from the spirit and scope of the invention.
9 sheets
Sheet 1 Sheet 2 Sheet 3 Sheet 4 Sheet 5 Sheet 6 Sheet 7 Sheet 8 Sheet 9
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| Document | Relation | Office | Cited during |
|---|---|---|---|
| AU2008200588B2 | Cited by | Australia | Search report |
| EP0551692A1 | Cited by | European Patent Office (EPO) | Search report |
| US5260017A | Cited by | United States of America | Search report |
| EP4108431A1 | Cited by | European Patent Office (EPO) | Search report |
| EP3492233A4 | Cited by | European Patent Office (EPO) | Search report |
| US11014275B2 | Cited by | United States of America | Applicant |
| GR900100633A | Cited by | Greece | Search report |
| EP0493538A4 | Cited by | European Patent Office (EPO) | Search report |
| US5783132A | Cited by | United States of America | Search report |
| EP0493538A1 | Cited by | European Patent Office (EPO) | Search report |
| FR2779988A1 | Cited by | France | Search report |
| EP0687548A3 | Cited by | European Patent Office (EPO) | Search report |
| EP0687548A2 | Cited by | European Patent Office (EPO) | Search report |
| US4304751A | Cites | United States of America | Search report |
4 priority claims, no other members on record
Priority claims4
| Document | Office | Kind | Date |
|---|---|---|---|
| 176114 | United States of America | – | |
| 17611488 | United States of America | A | |
| US19880176114 | – | – | – |
| 176114 | – | – | – |
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Numbers
- Publication
- 0335098
- Publication, DOCDB
- 0335098
- Publication, EPODOC
- EP0335098
- Application
- 891029183
- Application, DOCDB
- 89102918
- Application, EPODOC
- EP19890102918
Titles6
- German
- Formpressen von Formteilen aus Verbundwerkstoff auf heissen Formoberflächen und mit kurzer-Zykluszeit
- English
- Compression molding of composite parts on hot mold surfaces with a short cycle time
- French
- Moulage par compression de pièces en matière composite sur des surfaces de moule chaudes en employant un temps de cycle court
- German
- Formpressen von Formteilen aus Verbundwerkstoff auf heissen Formoberflächen und mit kurzer-Zykluszeit.
- English
- Compression molding of composite parts on hot mold surfaces with a short cycle time.
- French
- Moulage par compression de pièces en matière composite sur des surfaces de moule chaudes en employant un temps de cycle court.
Classification
- CPC, 5
- B29C70/46
- B29C33/02
- B29C33/56
- B29C33/565
- B29C43/52
- IPC, 9
- B29C43 18
- B29B11 12
- B29C33 02
- B29C33 56
- B29C43 34
- B29C43 52
- B29C70 46
- B29K105 08
- B29K105 20
Designated states5
- Contracting states, 5
- Germany
- France
- United Kingdom
- Italy
- Netherlands (Kingdom of the)