Composite wheel rim preform and method of fabricating a composite wheel rim preform
11090975 · 2021-08-17
Assignee
Inventors
Cpc classification
B60B2310/242
PERFORMING OPERATIONS; TRANSPORTING
B60B21/023
PERFORMING OPERATIONS; TRANSPORTING
B29B11/16
PERFORMING OPERATIONS; TRANSPORTING
B32B37/16
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B3/26
PERFORMING OPERATIONS; TRANSPORTING
B32B38/0012
PERFORMING OPERATIONS; TRANSPORTING
B29C70/30
PERFORMING OPERATIONS; TRANSPORTING
B60B2310/241
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
B32B5/06
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B37/16
PERFORMING OPERATIONS; TRANSPORTING
B32B38/00
PERFORMING OPERATIONS; TRANSPORTING
B32B3/26
PERFORMING OPERATIONS; TRANSPORTING
B29B11/16
PERFORMING OPERATIONS; TRANSPORTING
B29C70/00
PERFORMING OPERATIONS; TRANSPORTING
B60B21/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A preform for fabricating a wheel rim and a method of making a preform is provided. The preform includes a main section and at least one secondary section, each section being formed from composite materials, such as triaxially braided composite material that includes fibers oriented in at least three directions. The main section forms at least part of a lateral section of the preform and the secondary section forms at least part of a radial portion of the preform, the radial portion of the preform being generally perpendicular to the lateral section of the preform. The preform is fabricated from a plurality of composite layers, at least some being custom composite layers having a plurality of axial fibers interwoven intermittently with substantially consistent first and second sets of biased fibers. In some embodiments, the preform is initially fabricated in an intermediate configuration prior to being moved to a final configuration.
Claims
1. A composite preform for a composite wheel rim, the preform comprising a plurality of composite layers, at least some of the composite layers being custom composite layers having a plurality of axial fibers having an axial orientation being interwoven intermittently with a first set of biased fibers having a first biased orientation offset from the axial orientation and a second set of biased fibers having a second biased orientation offset from the axial orientation and the first biased orientation and wherein at least one custom composite layer defining a low-density region, said low-density region being defined by at least one of an omitted axial fiber within said low-density region or an undersized axial fiber within said low-density region and wherein at least one custom composite layer defines a high-density region, said high density region being defined by an oversized fiber within said high density region.
2. The composite preform of claim 1, wherein said low-density region being defined by said omitted axial fiber.
3. The composite preform of claim 1, wherein said oversized fiber is an oversized axial fiber within said high-density region.
4. The composite preform of claim 1, wherein at least one of the axial fibers is fabricated from a metallic material.
5. The composite preform of claim 1, wherein the axial orientation is generally perpendicular to a central axis of the wheel rim such that the axial fibers generally follow a circumference of the wheel rim.
6. The composite preform of claim 1, wherein the axial orientation is generally parallel with a central axis of the wheel rim such that the axial fibers are generally in line with the central axis of the wheel rim.
7. The composite preform of claim 1, wherein the preform comprises: a main section in a generally lateral configuration; and a secondary section in a radial configuration, wherein the secondary section extends generally perpendicularly from the main section, wherein the main section and the secondary section are formed at least partially from a custom composite layer extending from the main section into the secondary section, and wherein the custom composite layer comprises at least one of a low-density region or a high-density region.
8. The composite preform of claim 1, wherein said high-density region includes additional fibers.
9. The composite preform of claim 1 wherein the axial orientation of at least one of the axial fibers is selected from the group consisting of axial fibers generally following a circumference of the wheel rim wherein the axial orientation is generally perpendicular to a central axis of the wheel rim, or axial fibers generally in line with the central axis of the wheel rim wherein the axial orientation is generally parallel with said central axis of the wheel rim.
10. The composite preform of claim 1 wherein said low-density region being defined by said undersized axial fiber within said low-density region.
11. The composite preform of claim 1 wherein said high oversized fiber is at least one of said plurality of axial fibers.
12. The composite preform of claim 8 wherein said additional fibers are axial fibers.
13. The composite preform of claim 1 wherein said low-density region is defined by an undersized axial fiber.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) A preferred embodiment of the invention, illustrative of the best mode in which the applicant has contemplated applying the principles, is set forth in the following description and is shown in the drawings and is particularly and distinctly pointed out and set forth in the appended claims.
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DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT
(12) As required, a detailed embodiment of the present invention is disclosed herein; however, it is to be understood that the disclosed embodiment is merely exemplary of the principles of the invention, which may be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed structure.
(13) The present invention comprises a composite wheel rim preform 10 and a method of fabricating the same. More specifically, the present invention comprises a wheel rim preform 10 that is fabricated at least partially from triaxial braided composite material in such a way so as to enable production of a triaxial braided composite wheel 100 that includes at least one radial flange.
(14) Referring to
(15) In some embodiments, the outer 122 and inner 142 bead flanges are radially oriented flanges that extend radially outward at or near respective outer and inner edges of the wheel rim 100. In some such embodiments, a generally axially oriented outer return flange 125 extends axially outward from a distal edge of the outer bead flange 122 such that the outer return flange 125 extends away from the outer bead seat region 124. In other such embodiments, a generally axially oriented inner return flange 145 extends axially inward from a distal edge of the inner bead flange 142 such that the inner return flange 145 extends away from the inner bead seat region 144.
(16) In some embodiments, the outer bead seat region 124 extends axially inward from a proximal edge of the outer bead flange 122. In some such embodiments, the outer bead hump 126 forms an inner edge of the outer bead seat region 124. In other embodiments, the inner bead seat region 144 extends axially inward from a proximal edge of the inner bead flange 142. In some such embodiments, the inner bead hump 146 forms an outer edge of the inner bead seat region 144.
(17) In some embodiments, the outer portion 120, the lateral portion 130, and the inner portion 140 of the wheel rim are all formed at least partially from a plurality of continuous composite layers 41 extending from the lateral portion 130 into each of the outer 120 and inner 130 portions. In some such embodiments, at least some of the continuous composite layers 41 extend from a distal edge of the outer bead flange 122 into the lateral portion 130. In other such embodiments, at least some of the continuous composite layers 41 extend from a distal edge of the inner bead flange 142 into the lateral portion 130. In still other such embodiments, at least some of the continuous composite layers 41 extend from a distal edge of the outer bead flange 122, through the lateral portion 130, to a distal edge of the inner bead flange 142. In some embodiments, the wheel rim 100 includes one or more auxiliary flange 150. In some such embodiments, at least some of the continuous composite layers 41 extend from the lateral portion 130 into the auxiliary flange 150. In other such embodiments, the auxiliary flange 150 is oriented in a radial configuration such that it is generally perpendicular to the lateral section 130. In still other such embodiments, the auxiliary flange 150 is formed as part of the lateral section 130.
(18) Referring to
(19) Referring to
(20) Referring to
(21) Referring to
(22) Referring to
(23) Referring to
(24) In preferred embodiments, the main section 22 comprises a generally lateral configuration. In some embodiments, the main section 22 is a single section of the preform 10. In other embodiments, the main section 22 is broken into several pieces and/or sections. In some such embodiments, the main section 22 is broken by one or more crease and/or fold line. In other such embodiments, the main section 22 is broken by one or more secondary section. In various such embodiments, one or more layer of composite material 41 extends from the main section 22 into the secondary section. In some such embodiments, the piece of composite material 41 extends from one portion of the main section 22, through the secondary section, and into another portion of the main section 22.
(25) In some embodiments, at least some of the composite layers 41 are folded against each other such that the secondary section comprises first and second radial portions. In some such embodiments, the first and second radial portions of the secondary section are capable of forming first and second radial portions of an auxiliary flange 150 of the wheel rim 100, with the first radial portion being formed from a portion of the composite material 41 that extends towards a distal end 152 of the auxiliary flange 150 and the second radial portion being formed from a portion of the composite material 41 that extends away from the distal end 152 of the auxiliary flange 150. In some embodiments, at least some of the composite layers 41 are folded back over themselves again so as to extend between the first and second radial portions of the secondary section such that the auxiliary flange 150 further comprises a third radial portion and/or such that a distal end of the composite layers 41 is entrapped between the first and second radial portions of the auxiliary flange 150.
(26) In some embodiments, the secondary section is moveable from an angled configuration to a radial configuration. In some such embodiments, the secondary section is in the angled configuration when the preform 10 is in an intermediate configuration. In other such embodiments, the secondary section is in the radial configuration when the preform 10 is in a final configuration. In some embodiments, the secondary section is generally perpendicular to the main section 22 when the secondary section is in the radial configuration. In some embodiments, the secondary section is an end section 23, 24 that is capable of forming at least part of a bead flange 122, 142 of the wheel rim 100. In other embodiments, the secondary section is an auxiliary section 25 that is capable of forming at least part of an auxiliary flange 150 of the wheel rim 100.
(27) The present invention further includes a method for making a preform 10 for a composite wheel rim 100. In some such embodiments, the method includes utilizing a capstan braiding process to create the preform 10 in an intermediate configuration. Referring to
(28) Referring again to
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(30) Still referring to
(31) Still referring to
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(33) In preferred embodiments of the present invention, the method of fabricating a composite preform 10 includes forming the preform 10 in an intermediate configuration and moving it to a final configuration. In some embodiments, the preform 10 includes a main section 22 and at least one secondary section, the secondary section being moveable between an angled configuration and a radial configuration. In some such embodiments, the secondary section is in the angled configuration when the preform is in the intermediate configuration. In other such embodiments, the secondary section is in the radial configuration when the preform is in the final configuration. In still other such embodiments, the main section 22 has a generally lateral configuration. In yet other such embodiments, the secondary section is generally perpendicular to the main section when the secondary section is in the radial configuration.
(34) In some embodiments, the secondary section is an auxiliary section 25. In some such embodiments, the auxiliary section 25 forms an open v-section when the auxiliary section 25 is in the angled configuration. In other such embodiments, moving the auxiliary section 25 to the radial configuration comprises closing at least part of the v-section. In some such embodiments, the auxiliary section 25 is configured so as to be capable of forming at least part of an auxiliary flange 150 of a wheel rim 100 when the auxiliary section 25 is in the radial configuration.
(35) In some embodiments, the secondary section is an end section 23, 24. In some such embodiments, the end section 23, 24 extends from an edge of the main section 22. In other such embodiments, the end section 23, 24 is configured so as to be capable of forming at least part of an outer 120 or inner 140 portion and/or at least part of one or more cap flap 520, 540. In some embodiments, one or more cap flap is formed by cutting one or more radial slit 500.
(36) In some embodiments, moving the end section 23, 24 from the angled configuration to the radial configuration comprises rotating a proximal portion of the end section 23, 24 so as to be generally perpendicular with the main section 22. In this way, the proximal portion of the end section 23, 24 is capable of forming at least part of a bead flange 122, 142. In other embodiments, moving the end section from the angled configuration to the radial configuration further comprises rotating a mid-portion and/or a distal portion of the end section 23, 24 so as to be generally perpendicular with the proximal portion of the end section 23, 24. In this way, the mid and/or distal portion of the end section 23, 24 is capable of forming at least part of a return flange 125, 145 of the wheel rim 100. In still other embodiments, a distal portion of the end section 23, 24 forms at least one cap flap 520, 540. In some such embodiments, the method further includes folding the cap flap 520, 540 over the mid and/or proximal portion of the end section 23, 24. In this way, the end section 23, 24 is capable of forming a capped bead flange 122, 142 and/or a capped return flange 125, 145.
(37) In some embodiments, the present invention further includes forming a preform from a plurality of composite layers. In some such embodiments, at least some of the composite layers are custom composite layers. In some embodiments, a custom composite layer comprises a plurality of axial fibers that are interwoven intermittently with first and second sets of biased fibers. In some such embodiments, the first and/or second set of biased fibers are substantially consistent throughout all or part of the custom composite layer.
(38) In some embodiments, custom composite layers include one or more low-density region. In this way, in some embodiments, the custom composite layer provides for better drapability and/or otherwise improves the method of forming the preform of the present invention. In some embodiments, such as shown in
(39) In some embodiments, custom composite layers include one or more high-density region. In this way, in some embodiments, the custom composite layer provides for increased strength and/or increase thickness as required and/or desired. In some embodiments, a high-density region is a region of the custom composite layer in which one or more axial fiber is larger, stronger, and/or otherwise less susceptible to flexing and/or deforming than are other axial fibers outside of the high-density region. In some such embodiments, the high-density region is defined by axial fibers placed closer together than they are in other regions of the custom composite layer. In some such embodiments, two or more axial fibers are placed together in a high-density region where a single fiber would normally be utilized outside of the high-density region.
(40) In the foregoing description, certain terms have been used for brevity, clearness and understanding; but no unnecessary limitations are to be implied therefrom beyond the requirements of the prior art, because such terms are used for descriptive purposes and are intended to be broadly construed. Moreover, the description and illustration of the inventions is by way of example, and the scope of the inventions is not limited to the exact details shown or described.
(41) Although the foregoing detailed description of the present invention has been described by reference to an exemplary embodiment, and the best mode contemplated for carrying out the present invention has been shown and described, it will be understood that certain changes, modification or variations may be made in embodying the above invention, and in the construction thereof, other than those specifically set forth herein, may be achieved by those skilled in the art without departing from the spirit and scope of the invention, and that such changes, modification or variations are to be considered as being within the overall scope of the present invention. Therefore, it is contemplated to cover the present invention and any and all changes, modifications, variations, or equivalents that fall with in the true spirit and scope of the underlying principles disclosed and claimed herein. Consequently, the scope of the present invention is intended to be limited only by the attached claims, all matter contained in the above description and shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.
(42) Having now described the features, discoveries and principles of the invention, the manner in which the invention is constructed and used, the characteristics of the construction, and advantageous, new and useful results obtained; the new and useful structures, devices, elements, arrangements, parts and combinations, are set forth in the appended claims.
(43) It is also to be understood that the following claims are intended to cover all of the generic and specific features of the invention herein described, and all statements of the scope of the invention which, as a matter of language, might be said to fall therebetween.