FILM-BONDED INFUSION
20230076283 · 2023-03-09
Inventors
Cpc classification
B32B3/266
PERFORMING OPERATIONS; TRANSPORTING
B29C70/40
PERFORMING OPERATIONS; TRANSPORTING
B32B37/1009
PERFORMING OPERATIONS; TRANSPORTING
B32B3/30
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
B32B3/30
PERFORMING OPERATIONS; TRANSPORTING
B32B3/26
PERFORMING OPERATIONS; TRANSPORTING
B32B37/10
PERFORMING OPERATIONS; TRANSPORTING
Abstract
This disclosure includes sandwich composites comprising fiber-reinforced laminates. The disclosure further includes one or more film adhesives between a core and the fiber-reinforced laminates.
Claims
1-11. (canceled)
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] The foregoing and other objects, features, and advantages of the systems and methods described herein will be apparent from the following description of particular embodiments thereof, as illustrated in the accompanying figures, where like reference numbers refer to like structures. The figures are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the systems and methods described herein.
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DESCRIPTION
[0023] References to items in the singular should be understood to include items in the plural, and vice versa, unless explicitly stated otherwise or clear from the text. Grammatical conjunctions are intended to express any and all disjunctive and conjunctive combinations of conjoined clauses, sentences, words, and the like, unless otherwise stated or clear from the context. Recitation of ranges of values herein are not intended to be limiting, referring instead individually to any and all values falling within the range, unless otherwise indicated herein, and each separate value within such a range is incorporated into the specification as if it were individually recited herein. In the following description, it is understood that terms such as “first,” “second,” “top,” “bottom,” “side,” “front,” “back,” and the like are words of convenience and are not to be construed as limiting terms unless otherwise stated or clear from context.
[0024] As used herein, the terms “about,” “approximately,” “substantially,” or the like, when accompanying a numerical value, are to be construed as indicating a deviation as would be appreciated by one of ordinary skill in the art to operate satisfactorily for an intended purpose. Ranges of values and/or numeric values are provided herein as examples only, and do not constitute a limitation on the scope of the described embodiments. The use of any and all examples, or exemplary language (“e.g.,” “such as,” or “the like”) provided herein, is intended merely to better illuminate the embodiments and does not pose a limitation on the scope of the embodiments. The terms “e.g.,” and “for example” set off lists of one or more non-limiting examples, instances, or illustrations. No language in the specification should be construed as indicating any unclaimed element as essential to the practice of the embodiments.
[0025] As used herein, the term “and/or” means any one or more of the items in the list joined by “and/or”. As an example, “x and/or y” means any element of the three-element set {(x), (y), (x, y)}. In other words, “x and/or y” means “one or both of x and y”. As another example, “x, y, and/or z” means any element of the seven-element set {(x), (y), (z), (x, y), (x, z), (y, z), (x, y, z)}. In other words, “x, y, and/or z” means “one or more of x, y, and z.”
[0026] As used herein, the terms “exemplary” and “example” mean “serving as an example, instance or illustration.” The embodiments described herein are not limiting, but rather are exemplary only. It should be understood that the described embodiments are not necessarily to be construed as preferred or advantageous over other embodiments. Moreover, the terms “embodiments of the invention,” “embodiments,” or “invention” do not require that all embodiments of the invention include the discussed feature, advantage or mode of operation.
[0027] In connection with
[0028] The process may further include applying a second film adhesive, pre-impregnated, to a second surface of the core 112. The process may further include loading a second (dry) laminate stack adjacent the second film adhesive 114. A vacuum may then be applied to at least the second laminate stack 116. Initially, the laminate stack is preferably dry, not yet containing infusion resin. The process may further include infusing the second laminate with liquid resin under vacuum 118.
[0029] A curing process (e.g., like the ones described below) can then be used to cure the second infused resin in the second laminate stack 120. Preferably, this curing process will also simultaneously cure the second pre-impregnated film adhesive.
[0030] The resultant film-bonded infusion component 200 in
[0031] One advantage of preferred embodiments is that the film adhesive 204, 208 and the infusion resin can be selected such that they are able to cure simultaneously or approximately simultaneously. This is able to occur because the preferred curing times and temperatures for the film adhesive and the infusion resin overlap. Suitable film adhesives include VF400 low temperature pre-impregnated film adhesive (also referred to as epoxy adhesive film or epoxy film), sold by SDH Composites. Suitable infusion resins include, without limitation, epoxy 2110 from Endurance Technologies, and its associated hardeners (including, without limitation, the 9227 hardener).
[0032] The film adhesive 204, 208 selected is preferably in a solid state at room temperature. When the film adhesive 204, 208 is solid at room temperature, it is impermeable to the liquid resin that is used to infuse the laminate stacks 202, 210. As a result, when the liquid resin infuses the laminate stack 210 under vacuum, the liquid resin is not able to penetrate into the core 206. This prevents or reduces unnecessary resin in the end product, and lowers the density and weight of the resultant end product as compared to products and components made using existing resin infusion processes.
[0033] Film adhesives 204, 208 that may be used in connection herewith generally include any epoxy films that are solid at room temperature and become liquid upon heating at an increased temperature, and that preferably are capable of adhering to both a wet laminate stack 210 and the material of the core 206. Examples of such film adhesives include, without limitation, VF400 low temperature pre-impregnated film adhesive (also referred to as epoxy adhesive film or epoxy film), sold by SDH Composites. Infusion resins that may be used in connection herewith generally include resins that are capable of infusing a dry laminate stack and capable of adhering to an epoxy film. Examples of such infusion resins include, without limitation, without limitation, epoxy 2110 from Endurance Technologies.
[0034] For curing, after the laminate 202, 210 stacks are infused, the structure is placed in a heated chamber or oven. The film adhesive 204, 208 becomes liquid and bonds the laminate stack(s) 202, 210 to the core. It is presently understood that primarily chemical bonds (e.g., cross-linking) secure the epoxy film to the infused, laminate stacks and that primarily mechanical bonds secure the epoxy film to the core. The simultaneous curing process creates not only primary bonds but also secondary bonds between the second laminate and the second film adhesive.
[0035] The curing preferably takes place under vacuum, at an increased temperature. Preferred temperatures can range from about 120° F. to about 180° F., and more particularly from about 140° F. to about 160° F. In example processes, the curing time can preferably range from about 10 to about 20 hours, and more particularly about 15 to about 17 hours. In one embodiment, the curing temperature is set to 150° F. and the curing time is set for about 16 hours. In a preferred embodiment, the ramp up time from approximately room temperature to 150° F. may be, for example, between about 1 and about 3 hours, and is preferably about 2 hours.
[0036] The heating process preferably takes place after the infusion process is completed, but before the infusion resin is cured or before the infusion resin is fully cured.
[0037] The core may be generally flat or can be any three-dimensional shape desired.
[0038] Suitable materials for the core include, without limitation, foam (including without limitation polyurethane foam or Styrofoam), balsa wood, plywood, and plastics. In preferred embodiments, the core may be approximately 1 mm to 100 mm thick and may have non-uniform, varied thicknesses. Other thicknesses may be used as well, as one skilled in the art can appreciate in light of this disclosure.
[0039] Materials used in the laminate stacks include, without limitation, fibers made from carbon, Kevlar®, aramid, fiberglass, and/or basalt.
[0040] The methods and systems described herein could be generally described as a hybrid method of composite sandwich core construction. One preferred method combines the best attributes of the pre-preg process (e.g., lightweight and little or no wasted infusion resin) and the infusion process (minimal excess air or air bubbles) to achieve a pre-preg quality product (or better) at closer to resin infusion level production costs (or lower). Excess air within the infused laminate stack is known to weaken the components containing that air, which weaknesses may cause failure.
[0041] The processes described herein are believed to be usable with small scale and large scale parts.
[0042] In an alternative embodiment (illustrated in
[0043] Thus, under vacuum and at room temperature, even though the film adhesive 404, 408 is impermeable to the infusion resin, the breaks 416, 418 in the film adhesive, which are lined up with the grooves 414 and perforations 420 in the core 406, permit the infusion to have paths to the second laminate stack 410. Compared to existing resin infusion processes, this results in much less infusion resin being absorbed into the core 406. This is able to occur, in part, because the infusion resin is absorbed into the core 406 in only the vicinity of the grooves and/or perforations in the core. In contrast, using an existing resin infusion process, the liquid resin could be absorbed into the core 406 across the entire area of the core. In turn, the component may be lighter than if an existing resin infusion process were used.
[0044] A layer of compoflex 426 adjacent the first laminate stack 404 may also be used during the infusion process. The compoflex 426 facilitates the distribution of the infusion resin across the laminate stack 404. The compoflex 426 is preferably removed upon completion of the infusion process and prior to part service. Compoflex may be used in connection with either the one step or two step infusion process.
[0045] The resultant film-bonded infusion component 400 in
[0046] In an alternative embodiment, the infusion is preferably performed in one infusion step instead of two. The film adhesive may have perforations 420 and/or grooves 414, while the film adhesives 404, 408 has breaks 416, 418 that preferably align with the grooves 414 and/or perforations 420.
[0047] In connection with
[0048] In
[0049] The two step infusion process may be preferred in applications for mass production of components. One drawback of the two step infusion process is that one of the surfaces is typically rougher than the other. That is because one side has mold quality (adjacent laminate 210) and the other side typically does not (and is thus rougher than the mold quality surface.
[0050] The one step infusion process may produce two mold quality surfaces and will be more precise. It may therefore be preferred for specialized or unique production of components that require more precision on both outer surfaces.
[0051] In an alternative embodiment illustrated in
[0052] The film adhesive is vacuum bagged to the surface of the core to ensure the film adhesive properly follows the contour of the additional resin feed channels. The secondary resin channels 619 preferably are in fluid communication with the main channels 618 to make transfer of resin into the laminate easier. Preferably, when the film adhesive is pulled into the secondary feed channels 619, the resin flows from the main channels 618, below the film adhesive (through breaks), then uses the space beneath the secondary channels (and, at this point also below the film adhesive, which has been pulled into the secondary channels. As with earlier embodiments described, the depth and grid pattern of these smaller channels again may vary based upon reinforcement type and thickness.
[0053] While particular embodiments have been shown and described, it will be apparent to those skilled in the art that various changes and modifications in form and details may be made therein without departing from the spirit and scope of this disclosure and are intended to form a part of the inventions as defined by the following claims, which are to be interpreted in the broadest sense allowable by law. Further, the sequence of steps for the example methods described or illustrated herein are not to be construed as necessarily requiring their performance in the particular order described or illustrated unless specifically identified as requiring so or clearly identified through context. Moreover, the example methods may omit one or more steps described or illustrated, or may include additional steps in addition to those described or illustrated. Thus, one of ordinary skill in the art, using the disclosures provided herein, will appreciate that various steps of the example methods can be omitted, rearranged, combined, and/or adapted in various ways without departing from the spirit and scope of the inventions.