Method of manufacturing a composite insert
12054311 ยท 2024-08-06
Assignee
Inventors
- Michael J. Flener (Plymouth, MI, US)
- Martin Hornung (Rochester Hills, MI, US)
- Josef Hudina (Ketsch, DE)
- Gregory A. Krueger (Chisago City, MN, US)
Cpc classification
B29L2031/3002
PERFORMING OPERATIONS; TRANSPORTING
B29C39/10
PERFORMING OPERATIONS; TRANSPORTING
B32B1/00
PERFORMING OPERATIONS; TRANSPORTING
B29C45/14
PERFORMING OPERATIONS; TRANSPORTING
B29C33/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/1372
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29L2031/30
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/1376
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29C33/38
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/1355
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29K2063/00
PERFORMING OPERATIONS; TRANSPORTING
B29C67/246
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/1362
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
B29C33/00
PERFORMING OPERATIONS; TRANSPORTING
B29C33/38
PERFORMING OPERATIONS; TRANSPORTING
B29C39/10
PERFORMING OPERATIONS; TRANSPORTING
B29C45/14
PERFORMING OPERATIONS; TRANSPORTING
B29C67/24
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method of manufacturing a composite insert includes forming a polymer mold from a polymer sheet which may have a glass transition temperature of 70 to 160? C., the polymer mold either includes a cavity or may form a cavity disposed between the polymer mold and the carrier. The method proceeds by depositing a liquid reactive composite insert composition, which may be a two-component composition including a first part comprised of an isocyanate-epoxy blend and a second part comprised of an alcohol-epoxy blend, into the cavity under low pressure conditions of 0-10 bar and low temperature conditions of 15-100? C. The composition is then allowed to become dimensionally stable either within the polymer mold or between the polymer mold and the carrier.
Claims
1. A pre-packaged composite part comprising: a) a polymer mold joined to a carrier such that a cavity for accepting a composite insert composition is defined between the polymer mold and the carrier; b) a dimensionally stable composite insert comprising a composite insert composition provided with a shape by the polymer mold and the carrier, wherein said composite insert is adhered to the carrier, such that the carrier and the composite insert constitute a composite part, and the composite insert is disposed within the cavity such that the polymer mold remains covering at least a portion of the composite insert thereby forming a pre-packaging, which acts as an external protective covering for the composite insert; wherein the carrier is comprised of one or more of carbon fiber, fiberglass, plastics, metal, ceramic, paperboard and anisotropic materials; and the composite insert further comprises solid material, different from and separately introduced into the cavity from the composite insert composition, and molded with the composite insert composition, said solid material being incorporated discontinuously in the dimensionally stable composite insert at one or more selected positions such that the solid material is present in only portions of said insert.
2. The pre-packaged composite part of claim 1, wherein b) the dimensionally stable composite insert comprises a molded composite insert composition and a solid reinforcing material, different from and not comprised in composite insert composition as dispensed into the cavity, and molded with the composite insert composition, said solid reinforcing material being placed in only selected cavity positions prior to the composite insert composition such that the solid reinforcing material is incorporated into selected portions of the composite insert at one or more selected positions which correspond to the selected cavity positions.
3. The pre-packaged composite part of claim 2 wherein the solid reinforcing material, different from the composite insert composition, comprises fibers.
4. The pre-packaged composite part of claim 2 wherein the molded composite insert composition comprises a two-component composite insert composition comprising a first component and a second component reactive with the first component.
5. The pre-packaged composite part of claim 4 wherein the first component comprises an isocyanate-epoxy blend and the second component comprises an alcohol-epoxy blend reacted to form a polyurethane network providing dimensional stability of the not fully cured composite insert; wherein the epoxy of the blends remains unreacted until baked to produce full cure of the composite insert by epoxy reactions after removal from the cavity.
6. The pre-packaged composite part of claim 1 selected from a pre-packaged structural reinforcing composite part or acoustic abating composite part wherein the dimensionally stable composite insert and carrier are shaped to fit in a structural component of a vehicle; the composite insert adhered to and optionally over-molded onto the carrier, said carrier comprised of one or more of carbon fiber, fiberglass, plastic, metal, and anisotropic materials.
7. The pre-packaged composite part of claim 6 wherein the carrier comprises the anisotropic materials selected from wood and fiber reinforced composites.
8. The pre-packaged composite part of claim 6 wherein the dimensionally stable composite insert is not fully cured and requires a second curing stage after the pre-packaged composite part is fitted in the vehicle structural component, optionally with removal of the polymer mold pre-packaging, comprising paint oven baking to achieve full cure of the composite insert and adhesion to the vehicle structural component.
9. The pre-packaged composite part of claim 6 wherein the structural component for a vehicle, which the dimensionally stable composite insert and carrier are shaped to fit, is selected from an A-pillar, an A-pillar reinforcement, a B-pillar, a B-pillar reinforcement, a C-pillar, a C-pillar reinforcement, a rocker, a rocker reinforcement, a roof-rail or a roof-rail reinforcement.
10. The pre-packaged composite part of claim 1 wherein the dimensionally stable composite insert is over-molded onto the carrier thereby eliminating manual processes for fixing the composite insert to the carrier.
11. The pre-packaged composite part of claim 1, wherein the polymer mold comprises polyethylene terephthalate or isotactic polypropylene.
12. The pre-packaged composite part of claim 1, wherein the polymer mold surrounds a portion of the carrier.
13. The pre-packaged composite part of claim 1 wherein the polymer mold is fastened to the carrier using attachments, optionally comprising a surface interference fit between the polymer mold and the carrier.
14. The pre-packaged composite part of claim 13, wherein the polymer mold comprises one or more flange surfaces which comprise interference surfaces for contacting corresponding carrier flange surfaces on the carrier.
15. The pre-packaged composite part of claim 14 wherein the attachments comprise fasteners, tabs, clips, pins, weld tabs, ridges on the flanges, detents on the flanges and combinations thereof.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Other advantages of the present invention will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
DETAILED DESCRIPTION OF THE INVENTION
(12) Referring to the Figures, wherein like numerals indicate corresponding parts throughout the several views, a method of manufacturing a composite insert, as well as a method of manufacturing a composite part including the composite insert and a carrier joined together, first includes a step of obtaining, forming or having formed (hereinafter referred to collectively as forming) a polymer mold 20 for use in manufacturing the composite insert. One example of a polymer mold 20 that may result from such a forming step is generally shown in
(13) The polymer mold 20 shown in
(14) Carriers suitable for use in the invention include by way of non-limiting example, carriers for use in a structural component of a vehicle, such as an A-pillar, A-pillar reinforcement, B-pillar, B-pillar reinforcement, C-pillar, C-pillar reinforcement, rocker, rocker reinforcement, roof-rail, roof-rail reinforcement or the like. In these examples, the carrier often is comprised of steel or aluminum and the performance properties of the composite insert include the contribution of improved structural and/or acoustic performance to the structural component. The method of manufacturing the composite insert is not limited to these automotive structural components or even the two mentioned materials of the carrier. Rather, the method can be used to manufacture composite inserts for use with carriers of a variety of shapes and designs, and which can also be comprised of a variety of other materials such as carbon fiber, fiberglass, plastics, other metals, ceramics, anisotropic materials such as wood or fiber reinforced composites, paperboard and the like.
(15) As shown in
(16) Desirably, the polymer mold 20 may be comprised of an organic polymer having a glass transition temperature, in increasing order of preference, of at least 40, 45, 50, 55, 60, 65, 70, 75, 80, 85? C. and independently not more than 250, 200, 150, 100, 95, 90? C. In one embodiment, the method includes forming a polymer mold having a cavity from polymer having a glass transition temperature between 70 and 100? C. Organic polymer is intended to include homopolymers and co-polymers, random, block and tailed. One embodiment of the polymer sheet 22 comprises a polyester film, such as Mylar?, however any other suitable polymer sheets can be used to form the polymer mold 20, such as polyethylene terephtalate (PET), isotactic polypropylene (PP) or the like. The polymer sheet 22 is desirably insoluble in and not reactive with the composite insert composition at dispensing temperature.
(17) As shown in
(18) As shown in
(19) As shown in
(20) Also, where a composite insert is only desired to adhere or attach to a portion of the carrier 26, the seal defines limits or boundaries of the composite insert. For example, a polymer mold 20 can surround a portion of the carrier 26 on which a composite insert is desired, and in ensuing dispensing or injection steps, a composite insert composition would only flow and form an insert body up to the seal. Accordingly, through use of the polymer mold 20 and the attachments 32, the method can provide for forming a composite insert on only a portion of the carrier 26.
(21) As mentioned previously, in one embodiment of the method, only a composite insert is manufactured and thus use of a carrier 26 is not required. Rather, in this embodiment, the polymer mold 20 may be formed to create an open cavity into which a composite insert composition is dispensed or injected at low pressures. Alternatively, the polymer mold 20 may be formed such that the cavity 30 is surrounded by the polymer mold 20 thereby defining a closed cavity. The cavity 30 may be formed by joining two opposing polymer molds 20 together, or the polymer mold 20 and thus the cavity 30 could be formed by a variety of other suitable methods such as vacuum forming, blow molding, thermoforming, clam shell molding and the like.
(22) Whether generating a composite insert or a composite part, the method proceeds by dispensing or injecting a composite insert composition into the cavity 30, preferably under lower pressure conditions of between 0-10 bar and low temperature conditions of between 15-100? C., desirably 25-80? C. In an embodiment of the method, the cavity 30 can be pre-treated with a pre-curing media such as cooled or heated air, water, or other temperature controlled environment conditions prior to dispensing or injection of a composite insert composition, however this step is not required to perform the subject invention. In a preferred embodiment, the composite insert composition is a liquid at ambient temperatures, desirably at temperatures of about 10, 15, 20, 25 or 30? C. and can be dispensed at ambient temperature. Some composite insert compositions may optionally be warmed to dispensing temperature conditions as described herein prior to being introduced into the cavity 30; however dispensing temperature is less than a full cure temperature of the composite insert composition.
(23) Generally, whether liquid or solid at room temperature, the composite insert composition can be dispensed in the absence of the high temperature and high pressure conditions associated with the prior art injection molding processes of a solid composite insert composition.
(24) In one preferred embodiment, the composite insert composition is a two-component liquid composition, and thus the method includes pre-mixing the two components using a static or dynamic mixing element , shown diagrammatically in
(25) The step of dispensing or injecting the composite insert composition may include creating an injection hole 34 in the polymer mold 20 to provide access to the cavity 30 and injecting or dispensing the composite insert composition through the injection hole 34 and into the cavity 30. Where optional die 40 is used, the composition may be introduced to injection hole 34 via die passage 42. As mentioned previously, during injection of a composite insert composition into a cavity 30, although the attachments 32 create a liquid tight seal between the polymer mold 20 and the carrier 26, air is allowed to escape from the cavity 30 via air evacuation sites as the composition is introduced. In the embodiment where a carrier 26 is not used, the step of injecting or dispensing the composite insert composition also includes creating at least one vent hole 35 in the polymer mold 20 for allowing air to escape out of the cavity 30, e.g. rise, as the composition is introduced, unless the polymer mold 20 is an open cavity mold as described herein. While the injection hole 34 can be located at any position along the polymer mold 20, it is desirably positioned at the bottom of the polymer mold 20. Correspondingly, the vent hole 35 is desirably positioned opposite the injection hole 34 to allow the air to effectively rise and escape from the cavity 30 of the polymer mold 20. In one embodiment, an active air evacuation step can also be used to remove air from the cavity, but this step is not required to perform the subject method.
(26) After injecting or dispensing the composition into the cavity 30, the injection hole 34, and optionally the vent hole 35 where used, in the polymer mold 20 may be sealed using suitable methods and devices to isolate the composite insert composition within the cavity 30 and thus limit the composition either within the polymer mold 20 or between the polymer mold 20 and the carrier 26. Suitable methods and devices to isolate the composite insert composition within the cavity 30 include, by way of non-limiting example, adhesive tape, sealant, plugs, welding. ultrasonic energy, adhesive compositions or the like. The method proceeds by allowing the composite insert composition to become dimensionally stable. In the embodiment where a composite part is manufactured, the composite insert composition adheres to the carrier 26 and creates a solid composite insert 36 disposed between the polymer mold 20 and the carrier 26, as shown in
(27) When the composite insert composition is injected under low temperature conditions as described herein, the step of allowing the composite insert composition to become dimensionally stable includes cooling the injected composition for a predetermined residence time of between 0 to 600 seconds, desirably the cooling time is at least 1, 5, 10, 20, 30, or 45 seconds and independently is not more than 600, 550, 500, 450, 400, 350 300, 240, 200, 180, 150, 120, 100, 90 or 60 seconds. When a two-component liquid composition is injected under low temperature conditions, the step of allowing the composite insert composition to become dimensionally stable includes allowing the first and second components to react, and optionally cooling the injected composition, for a predetermined residence time as described above. For example, in one embodiment using polyurethane chemistries, the isocyanate of the first component reacts with the alcohol of the second component to create a cross linked polyurethane network that produces a solid, dimensionally stable, composite insert. A short residence time after the injecting or dispensing step provides the composite insert composition with sufficient time to solidify and form a solid composite.
(28) The solid composite insert is dimensionally stable, but is not fully cured after manufacture. A second curing step, typically in a production step for a vehicle or other article of manufacture utilizing the composite insert or part, such as a paint or other bake cycle, causes full cure of the composite insert composition. Desirably, full cure may result from epoxy reactions and the like. The full cure results in a cured composite section adhered to any optional carrier as well as to surfaces of a vehicle or other article of manufacture utilizing the composite insert or part.
(29) After the composite insert 36 is manufactured, the polymer mold 20 can be removed, and optionally reused or recycled; or can remain on the composite insert 36, as shown in
(30) Obviously, many modifications and variations of the present invention are possible in light of the above teachings and may be practiced otherwise than as specifically described while within the scope of the appended claims. These antecedent recitations should be interpreted to cover any combination in which the inventive novelty exercises its utility. The use of the word said in the apparatus claims refers to an antecedent that is a positive recitation meant to be included in the coverage of the claims whereas the word the precedes a word not meant to be included in the coverage of the claims. In addition, the reference numerals in the claims are merely for convenience and are not to be read in any way as limiting.