METHOD OF MAKING A HYBRID BEAM AND HYBRID BEAM
20190329466 ยท 2019-10-31
Assignee
Inventors
Cpc classification
B29L2031/3002
PERFORMING OPERATIONS; TRANSPORTING
B29C2045/14868
PERFORMING OPERATIONS; TRANSPORTING
B60R19/03
PERFORMING OPERATIONS; TRANSPORTING
B29C45/14311
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
Reinforced composite structural members and methods of forming thereof. The method includes providing one or more reinforcements, one or more adhesives, a mold with a mold cavity and resin. The one or more reinforcements are coated with the one or more adhesives and then are placed within the mold cavity. Next the mold cavity is closed and a step of overmolding the one or more reinforcements by injecting molten resin into the mold cavity, then curing the molten resin to form the structural member. The one or more adhesives coated onto the one or more reinforcements facilitates the bonding of the resin of material to the one or more reinforcements.
Claims
1. A method of making a structural member comprising the steps of: providing one or more reinforcements, one or more adhesives, a mold with a mold cavity and resin; coating the one or more reinforcements with the one or more adhesives; placing the one or more reinforcements coated with one or more adhesives into the mold cavity; overmolding the one or more reinforcements by injecting molten resin into the mold cavity and then curing the molten resin to form the structural member; and pre-heating the one or more reinforcements coated with the one or more adhesives to activate the one or more adhesives prior to the step of overmolding or prior to the step of placing the one or more reinforcements into the mold cavity.
2. (canceled)
3. The method of claim 1 wherein the pre-heating of the one or more reinforcements is carried out at a temperature greater than about 150 C.
4. The method of claim 1 wherein the pre-heating of the one or more reinforcements is carried out at a temperature range between about 150 C. to about 180 C.
5. The method of claim 1 wherein the coating step further includes plasma spraying the adhesive onto the one or more reinforcements using a first spray having a cleaning solution and then a plasma spray containing a stream of plasma containing the one or more adhesives.
6. The method of claim 1 wherein the step of coating the one or more reinforcements with one or more adhesives occurs at ambient temperature.
7. The method of claim 6 further comprising the curing of the molten resin by heating the mold cavity, wherein the one or more adhesives are activated by heat in the mold cavity during the step of overmolding.
8. The method of claim 7 wherein the one or more adhesives are activated at a temperature range between about 90 C. to about 150 C.
9. The method of claim 7 wherein the one or more adhesives are activated at a temperature range between about 115 C. to about 125 C.
10. A method of making structural member comprising the steps of: providing one or more reinforcements made of steel wire; providing one or more adhesives being at least one selected from the group consisting essentially of a nylon adhesive and a polypropylene adhesive; providing a mold having a mold cavity; providing a resin material being at least one selected from the group consisting essentially of polypropylene a resin and a nylon resin; coating the one or more reinforcements with the one or more adhesives; placing the one or more reinforcements coated with one or more adhesives into the mold cavity; overmolding the one or more reinforcements by injecting molten resin into the mold cavity and then curing the molten resin.
11. The method of claim 10 further comprising the step of pre-heating the one or more reinforcements coated with the one or more adhesives to activate the one or more adhesives prior to the step of overmolding or prior to the step of placing the one or more reinforcements into the mold cavity.
12. The method of claim 11 wherein the pre-heating of the one or more reinforcement rods is carried out at a temperature greater than about 150 C.
13. The method of claim 14 wherein the pre-heating of the one or more reinforcement rods is carried out at a temperature range between about 150 C. to about 180 C.
14. The method of claim 10 wherein the step of coating the one or more reinforcements with one or more adhesives occurs at ambient temperature.
15. The method of claim 14 further comprising the curing of the molten resin by heating the mold cavity, wherein the one or more adhesives are activated by heat in the mold cavity during overmolding.
16. The method of claim 15 wherein the one or more adhesives are activated at a temperature range between about 90 C. to about 150 C.
17. The method of claim 15 wherein the one or more adhesives are activated at a temperature range between about 115 C. to about 125 C.
18. The method of claim 10 wherein the coating step further includes plasma spraying the adhesive onto the one or more reinforcements using a first spray of a cleaning solution and then a plasma spray containing a stream of plasma containing the one or more adhesives.
19. (canceled)
20. (canceled)
21. (canceled)
22. (canceled)
23. The method of claim 1 wherein the resin is one or more selected from the group consisting essentially of castable urethane resins, polypropylene, polyester, polyamide and nylon.
24. The method of claim 23 wherein the resin further includes a fiber filler than is carbon fibers, glass fibers or a combination thereof.
25. (canceled)
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0006] The invention will be described below with reference to exemplary embodiments illustrated in the drawing, wherein:
[0007]
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[0019]
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0020] Referring now to
[0021] The body 14, 14 has a top portion 48, 48 having a length L1 with at least two of the plurality of reinforcements 12, 12 extends along a portion of the length L1 of the top portion 48, 48. A bottom 50, 50 portion has a length L2 with at least two of the plurality reinforcements 12, 12 extends along a portion of the length L2 of the bottom portion 50, 50. A left side portion 52, 52 having a length L3 with at least two of the plurality reinforcements 12, 12 extends along a portion of the length L3 of the left side portion 52, 52, wherein the left side portion 52, 52 extends between the top portion 48, 48 and the bottom portion 50, 50. A right side portion 54, 54 having a length L4 with at least two of the plurality reinforcements 12, 12 extends along a portion of the length L4 of the right side portion 54, 54. The right side portion 54, 54 extends between the top portion 48, 48 and the bottom portion 50, 50. Since the body 14, 14 is made of a composite material it is further strengthened with a plurality of integrated external reinforcement ribs 56, 56 that are formed during the molding process.
[0022] The methodology of the present invention is used to create other structural members. Additional examples will be discussed, but not limited to the examples shown in
[0023] The structural member 10, 10 shown is a composite front end module for a motor vehicle. However, it is possible for the structural member to take many forms including, but not limited to, crush cans, transverse support members, lift gates, tailgates, bumpers, etc. or any other structural member that would benefit from the increased strength of the reinforcement rods.
[0024] The body of the structural member 14, 14 is made of resin material, which is preferably castable urethane, polypropylene, polyamide, polyester or nylon resins, which may or may not have filler material such as carbon fibers or glass fibers. The plurality of reinforcements 12, 12 which are depicted as reinforcement rods that are preferably made of steel, but can also be made of aluminum, iron, metal alloys, polymer, polymer with fiber reinforcements or virtually any material having a suitable tensile strength. While the reinforcements 12, 12 in this specification are shown and described as rods, it is within the scope of this invention for them to have other shapes or forms such as ribbons, plates, threads, mesh, chain link etc.
[0025] Referring to
[0026]
[0027] After the first step of coating the reinforcement rods 12, as depicted in
[0028] The type of adhesives contemplated being used in accordance with the present invention are generally nylon or polypropylene adhesives. However the specific adhesives can include other types of adhesives. In one aspect of the invention the adhesive used is THIXON 422 manufactured by Rohm and Haas Company, which is a one-component, solvent-based adhesive for bonding castable urethane to metal substrates, offering very good high temperature resistance. In another aspect of the invention the specific adhesive used is an adhesion promoter called VESTAMELT Hylink manufactured by Evonik Resource Efficiency Gmbh, which is a cross linkable copolyamide adhesion promoter (e.g. a compound that makes the resin of the body 14 stick to the individual rods 12) for metal-plastic hybrid components with outstanding resistance to heat and mechanical stress. While THIXON 422 and VESTAMELT Hylink are specifically mentioned it is within the scope of this invention for any suitable adhesive or adhesion promoter to be used provided whatever compound used, makes the resin of the body 14 stick to the individual rods 12.
[0029] In embodiments where the rods 12 are coated in an oven or preheated before molding, as shown in
[0030] In embodiments where the coating step is carried out at ambient temperatures and no preheating of the rods is necessary or in embodiments shown in
[0031] Referring back to
[0032] Referring now to
[0033] At a second step a second spray stream 36, which in one embodiment is a silane stream of plasma having an adhesive is sprayed from a second spray source 38 onto the reinforcements 12. The second spray source 38 is a plasma spray source. The type of adhesive used can be a plasma spray able adhesive similar to the adhesives mentioned above with reference to
[0034] The process is optionally carried out in an oven 40 having a heat source 42 that heats the reinforcements 12. However, it is contemplated that certain types of adhesive can be applied using the plasma spray technique with the reinforcements 12 being kept at ambient temperature. If the plasma spray method requires heat the oven 40 environment is between about 160 C. to about 180 C. or any temperature there between. However, depending on the type of adhesives it is possible that both of the above steps occur at ambient temperatures, with the adhesives having the same curing temperature ranges as described above with respect to
[0035] Structural members of this kind may be used, for example, as supporting structures in motor vehicles, examples include, but are not limited to crush cans, front end modules and transverse supporting members.
[0036]
[0037] The structural member 27 is shown generically and hereby represents any structural member produced according to the methods described herein, including the reinforced composite member 10, 10 (described above), vehicle bumper 18 (described below), transverse supporting member 100 (described below) or any other type of product made according to the teachings of the method of the invention. As shown there a plurality of reinforcements 13 overmolded within a resin 29 material that forms the body of the structural member 27. The reinforcements 13 are coated with a layer 31 of coating that is an adhesive coating applied in a manner described above with respect to
[0038] Referring now to
[0039] Referring now to
[0040] The description of the invention is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.