COMPOSITE STRUCTURES, FORMING APPARATUSES AND RELATED SYSTEMS AND METHODS
20180154592 ยท 2018-06-07
Inventors
- Vernon M. Benson (Morgan, UT, US)
- Jason K. Slack (Clinton, UT, US)
- Todd A. Rosevear (Taylorsville, UT, US)
- James L. Harvey (Salt Lake City, UT, US)
- Mark Roman (Salt Lake City, UT, US)
- Timothy S. Olschewski (Kearns, UT, US)
Cpc classification
B29C70/545
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24628
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
Y10T156/1002
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
B29K2307/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24995
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
B29C70/504
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/249948
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
Y02T50/40
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
Y10T428/24124
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
B29C70/541
PERFORMING OPERATIONS; TRANSPORTING
Y10T156/1031
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
B29L2031/003
PERFORMING OPERATIONS; TRANSPORTING
Y10T156/1028
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
B29C70/38
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Apparatuses for forming a composite structure are configured to provide a tension at least partially along at least one ply of material as the at least one ply of material is supplied from a material feed assembly to a tool.
Claims
1. An apparatus for forming a composite structure, comprising: a forming tool having a forming surface configured to receive thereon at least one ply of material to form the composite structure; and a material feed assembly configured to hold a supply of the at least one ply of material and to provide the at least one ply of material onto the forming tool, the apparatus being configured to apply a force to the at least one ply of material to develop a tension at least partially along a width of the at least one ply of material as the at least one ply of material is supplied from the material feed assembly to the forming tool.
2. The apparatus of claim 1, further comprising a forming mechanism configured to apply a force to at least a portion of the at least one ply of material to conform the at least a portion of the at least one ply of material to the forming surface of the forming tool.
3. The apparatus of claim 1, wherein the material feed assembly is configured to apply the force to the at least one ply of material to develop the tension at least partially along the width of the at least one ply of material.
4. The apparatus of claim 3, wherein the material feed assembly is configured to apply the force to the at least one ply of material by restricting movement of the supply of the at least one ply of material as the at least one ply of material is supplied to the forming tool.
5. The apparatus of claim 1, wherein the material feed assembly is configured to hold a spool of material, and wherein the apparatus is configured to position a centerline of the spool of material on the material feed assembly at the oblique angle relative to an axis of the forming tool.
6. The apparatus of claim 1, wherein the apparatus is configured to develop a tension gradient at least partially along the width of the at least one ply of material, the width extending in a direction transverse to a major length of the at least one ply of material and transverse to a thickness of the at least one ply of material.
7. The apparatus of claim 1, wherein the apparatus is configured to supply a maximum amount of the tension at a portion of the at least one ply of material that is to be supplied to a corresponding portion of the forming tool having a relatively larger radius of curvature than another portion of the forming tool.
8. The apparatus of claim 1, wherein the forming tool exhibits at least one of an at least partially curved shape or an at least partially arcuate shape.
9. The apparatus of claim 1, wherein the forming tool exhibits an at least partially annular shape.
10. The apparatus of claim 1, wherein the apparatus is configured to form a composite structure exhibiting: a first portion having a first radius of curvature; a second portion having a second radius of curvature, wherein the second radius of curvature is either greater than or lesser than the first radius of curvature; and a middle portion extending between the first portion and the second portion, wherein the middle portion gradually changes from the first radius of curvature to the second radius of curvature.
11. An apparatus for forming a composite structure, comprising: a forming tool having a forming surface configured to receive thereon at least one ply of material to form the composite structure; and a material feed assembly configured to hold a supply of the at least one ply of material and to provide the at least one ply of material onto the forming tool, the material feed assembly configured to apply a tension to the at least one ply of material at a location in the at least one ply of material between the material feed assembly and the forming tool.
12. The apparatus of claim 11, wherein the tension comprises a tension gradient extending along the width of the at least one ply of material from a first lateral side of the at least one ply of material to a second lateral side of the at least one ply of material.
13. The apparatus of claim 12, wherein the apparatus is configured to supply a maximum tension of the tension gradient at the first lateral side that is to be supplied to a portion of the forming tool having a relatively larger radius of curvature than another portion of the forming tool.
14. The apparatus of claim 11, wherein the apparatus is configured to position the material feed assembly at an angle offset to the forming tool in order to apply the tension to the at least one ply of material.
15. The apparatus of claim 11, wherein the apparatus is configured to form the composite structure having a first radius of curvature, a second radius of curvature, and an intermediate portion extending between the first radius of curvature and the second radius of curvature.
16. The apparatus of claim 11, wherein the material feed assembly is configured to apply the tension to the at least one ply of material by restricting movement of the at least one ply of material as the at least one ply of material travels from the material feed assembly to the forming tool.
17. The apparatus of claim 11, wherein the apparatus is configured to apply a majority of the tension to one lateral side portion of the at least one ply of material.
18. The apparatus of claim 17, wherein the apparatus is configured to minimize the tension on another lateral side portion of the at least one ply of material, the another lateral side portion opposing the one lateral side portion.
19. The apparatus of claim 11, wherein the apparatus is configured to produce the composite structure exhibiting at least one of an at least partially arcuate shape, an at least partially curved shape, or an at least partially annular shape.
20. A method of forming a composite structure in an at least partially automated process, the method comprising: developing a tension gradient along a width of at least one ply of material between a supply of the at least one ply of material in a material feed assembly and a tool configured to form the composite structure having an at least partially annular shape; and applying the at least one ply of material on a surface of the tool, wherein fibers in at least one ply of material are offset relative to a side of the at least one ply of material.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0019] The foregoing and other advantages of the disclosure will become apparent upon reading the following detailed description and upon reference to the drawings in which:
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DETAILED DESCRIPTION
[0042] Referring to
[0043] The carriage assembly 108 further includes a rolling member 116, also referred to herein as a roller, configured to be at least partially complementary with, and positioned over, the mandrel 106. The roller 116 may be removably coupled with the carriage assembly 108 such that other rollers may be interchanged therewith at various stages of forming the elongated member 102 or for forming elongated members with differing cross-sectional geometries. The roller 116 may be coupled to the carriage assembly 108 by way of a suitable bearing member 118 allowing the roller 116 to turn or roll when engaged with the base 104 and when the carriage assembly 108 is moving relative thereto. The roller 116 may be formed of, or coated with, for example, an elastomer material, such as, for example, polytetrafluoroethylene (PTFE), for purposes of conforming the roller 116 to the surface of, and more evenly distributing forces over, the laminate materials disposed over the mandrel 106 and which are being used to form the elongated member 102 as the roller 116 passes thereover.
[0044] The frame 110 of the carriage assembly 108 may desirably be configured such that the roller 116 is substantially vertically displaceable or adjustable relative to the base 104. For example, a portion of the frame 110, such as a cross-member 120, may be vertically displaceable relative to the main portion of the frame 110. The carriage assembly 108 is also configured to exert a generally downward force on the base 104 and, thus, the elongated member 102, by way of the roller 116. Various mechanisms may be used to exert such a force. For example, as illustrated in
[0045] The carriage assembly 108 may also include a heating apparatus 123 configured to heat a portion of the elongated member 102 prior to the roller 116 passing thereover. The heating apparatus or device 123 may include, for example, a resistive heater with an associated blower, an infrared heater, an ultrasonic heating device, a laser heating device, an electron beam heater or another appropriate heating device. In one embodiment, the heating device 123 may be configured and located to heat the mandrel 106, the roller 116 or both. In another embodiment, the heating device 123 may be configured and oriented to heat a portion of the elongated member 102 and, more particularly, a portion of one or more composite material sheets laid down on the mandrel 106 to form the resulting elongated member 102 as shall be discussed in greater detail below. Such a heating device 123 may be particularly useful in forming elongated members 102 from preimpregnated or prepreg materials. Such prepreg materials may include unidirectional tape or cloth material impregnated with a resin in a B-stage form (uncured). The application of heat to such prepreg materials may enable the material sheets to more readily conform to the shape of the mandrel 106 and, more importantly, helps to effect consolidation of the laminar structure, including multiple overlaying sheets of material, as such a structure is formed on the mandrel 106.
[0046] It is noted that the application of heat could be used to cure the elongated member 102 upon formation thereof (sometimes termed as cure-on-the-fly). However, the present disclosure also contemplates the ability to form an elongated member 102, which is substantially uncured. In other words, the present disclosure includes forming elongated members that are not significantly cured beyond the B-stage of a conventional prepreg material (also sometimes referred to as forming green structures or members). The ability to form uncured components provides for substantial flexibility in forming and manufacturing a composite structure including the ability to cocure the elongated members with a corresponding composite skin as is often desirable.
[0047] A cooling device 124 may also be coupled to the carriage assembly 108 to cool the elongated member 102, the roller 116, or some other tool or component associated with the apparatus 100. The cooling device 124 may include, for example, a vortex cooler, a system for circulating a cooling fluid through an interior portion of the roller 116, a cryogenic cooler, or a multiple phase system utilizing a condenser and evaporator.
[0048] Referring now to
[0049] For example, in forming an elongated member 102, plies of material (e.g., prepreg material) may be positioned on the mandrel 106, and upon one another, in a laminar manner. The first roller 116A may then be coupled to the carriage assembly 108, configured to engage the mandrel 106 and rolled along the base 104 to form an intermediate structure 102A, or a structure exhibiting an intermediate cross-sectional geometry taken substantially transverse to the length thereof, such as shown in
[0050] In one embodiment, the formation of the elongated member 102 may be conducted on a ply-by-ply basis. In other words, formation of the elongated member 102 may be effected by shaping a first ply to the desired cross-sectional geometry (e.g., by applying the ply to the mandrel 106 and passing the rollers 116A-116D thereover), applying a second ply of material and shaping the second ply of material to the desired cross-sectional geometry and conformally with the first shaped ply. The act of shaping the second or any subsequent ply through use of the rollers 116A-116D also serves to consolidate the plies and debulk the elongated member 102. Thus, the shaping and debulking of the elongated structure occurs as a substantially continuous and interrelated process.
[0051] In another embodiment, multiple plies may be placed over the mandrel 106 and shaped to a desired cross-sectional geometry simultaneously while also being consolidated and debulked. Thus, for example, two or three plies of material may be placed on the mandrel 106 and shaped and consolidated by the rollers 116A-116D followed by placement of two or three more plies of material over the shaped plies and the subsequent shaping thereof by the rollers 116A-116D.
[0052] The use of multiple rollers 116A-116D in sequentially forming intermediate structures 102A-102C and, ultimately, the final structure 102D, enables manipulation of the material (e.g., the prepreg plies) while imposing a relatively reduced amount of stress thereto than if the elongated member was formed in a single operation or a single pass of an individual roller. Perhaps more importantly, the multiple layers of, for example, prepreg material used to form the elongated member 102 become substantially consolidated and debulked during the formation of the intermediate structures 102A-102C.
[0053] It is noted that more or fewer rollers may be used in forming the elongated members 102 depending, for example, on the type of material being used, the number of plies or layers of material being utilized to form the elongated member 102, the number of plies being shaped during a given operation, and/or the desired cross-sectional shape of the resulting elongated member 102. Similarly, the incremental change in roller size may be adjusted depending on similar parameters.
[0054] It is also noted that, in forming intermediate structures, the rollers 116A-116D are progressive in their respective geometries. In other words, the first roller 116A only partially engages the mandrel and material laid thereover in that the outer sections 125A only extend partially down the side walls 127 of the complementary mandrel 106. The second roller 116B, while still only partially engaging the mandrel 106, does so more than did the first roller 116A. Similarly, the third roller 116C is configured to more fully engage the mandrel 106 than does the second roller 116B. Finally, the fourth roller 116D is configured to substantially fully engage the mandrel 106 such that its outer sections 125D extend fully down the side walls 127 of the mandrel 106.
[0055] The embodiment shown and described with respect to
[0056] Referring now to
[0057] A roller 216, configured to complementarily engage one or more of the mandrels 206A-206C, may be removably coupled to the carriage assembly 208 and may be coupled to an actuator 217 such that the roller 216 may be moved in a substantially vertical direction as indicated by directional arrow 218. The roller 216 may also be configured to swivel or rotate about a substantially vertical axis as indicated by directional arrow 219. The rotation of the roller 216 about the substantially vertical axis may be accomplished, for example, by allowing the roller 216 to freely swivel such that it generally follows the mandrel (e.g., 206B) with which it is engaged, as the carriage assembly 208 moves in the direction of directional arrow 211. In another embodiment, an actuator 217 may be used to motivate the roller 216 about the substantially vertical axis as may be desired.
[0058] A drive mechanism 220 may be configured to move the roller 216 and its associated actuator 217 laterally with respect to the base 204 and the gantry 210 as indicated by directional arrow 222. The ability to control the movement of the carriage assembly 208 relative to the base 204 allows considerable flexibility in forming elongated members 202. For example, the same roller 216 may be used to selectively and independently engage each of the plurality of mandrels 206A-206C.
[0059] Additionally, the elongated members 202 may be formed as relatively complex shapes, not only with respect to their cross-sectional geometries, but also with respect to their geometries along a defined longitudinal axis. For example, the base 204 of the presently described apparatus 200 includes a first relatively flat section 224, a sloped section 226, and a second relatively flat section 228 with the sloped section 226 being connected to adjacent flat sections 224 and 228 by curved transition sections 230 and 232. The mandrels 206A-206C generally comply with the contour or geometry of the base 204. Thus, as the carriage assembly 208 travels longitudinally as indicated by directional arrow 211, the roller 216 must be vertically displaced as indicated by directional arrow 218 in order to remain engaged with a corresponding mandrel (e.g., 206B).
[0060] In other embodiments, the mandrels 206A-206C may deviate laterally relative to the longitudinal direction of the base 204 (i.e., in the direction indicated by directional arrow 222). Such complex geometries may be accommodated by the present disclosure through the various degrees of freedom offered by the arrangement shown. It is noted that, in one embodiment, the roller 216 may be coupled to a wrist 234, which allows the axis upon which the roller 216 rotates to be varied. Thus, the roller 216 may be able to remain in substantial contact with a mandrel (e.g., 206B) even if the mandrel 206B exhibits a twist or rotation relative about its longitudinal axis and, thereby, enable the formation of elongated members 202 exhibiting a similar twist relative to their respective longitudinal axes.
[0061] In forming elongated members 202 with the above described apparatus 200, the roller 216 may be operated in a manner similar to that described above with respect to
[0062] Referring now to
[0063] Such an automated dispensing device may include cut, clamp and start mechanisms such that individual plies may be dropped and added on-the-fly as desired, or required depending on the configuration of the elongated member 302 being formed. Additionally, an automated dispensing device may include a mechanism for maintaining tension on the ply of material as it is being dispensed on to a mandrel 306A-306D. Application of tension to the material ply may be desirable to keep any wrinkles from developing in the material as the elongated members 302 are being formed. In one exemplary embodiment, a force of approximately 2 to 15 pounds-force (lbf) (approximately 8.9 to 66.7 Newtons (N)) may be applied to material plies as they are disposed on the mandrels 306A-306D.
[0064] Each device 312A-312D may further include associated actuators or drive mechanisms in order to move the devices 312A-312D relative to the base 304 and to apply pressure via an associated roller to any material laid up on the mandrels 306A-306D. Each device 312A-312D may be programmed to form identical stiffeners or form different stiffeners depending on the individual configuration of the mandrels 306A-306D mounted on the base 304.
[0065] Referring to
[0066] For example, referring briefly to
[0067] Referring briefly to
[0068] In another embodiment, one or more edge ply cutting devices 341 may be utilized to trim the edge (or edges) of any ply 330A-330H (
[0069] Still referring to
[0070] Referring now to
[0071] The apparatus 400 includes a plurality of rollers 406 (individually identified as rollers 406A-406E) that are each configured to engage a specific portion of the mandrel 404 (or the material plies laying thereover) in order to form a desired cross-sectional geometry. For example, a first roller 406A may be configured to press the plies of material onto the top surface of the mandrel 404. One set of rollers 406B may be configured to form the plies of material about the exterior corners of the male mandrel 404. Another set of rollers 406C may be configured to press the plies of material against the sides of the mandrel 404. A further set of rollers 406D may be configured to press the plies of material into the interior corners of the mandrel 404, and a final set of rollers 406E may be configured to press the plies of material against the laterally extending portions of the mandrel 404. Thus, the plurality of rollers 406 works collectively to substantially continuously form an elongated member 402 of a desired cross-sectional geometry over the mandrel 404.
[0072] Referring briefly to
[0073] Referring briefly to
[0074] While the above described embodiments have largely been discussed using the example of individual prepreg materials being laid up on associated mandrels, it is noted that nonimpregnated fiber materials may be utilized with such materials being laid upon on an associated mandrel while substantially simultaneously infusing or impregnating the plies of material with an appropriate resin or binder. For example, referring now to
[0075] It is noted that the various illustrative embodiments of the disclosure described above herein have generally shown an exemplary cross-sectional geometry of a hat, or the formation of an elongated member as a hat channel. However, it is contemplated that the present disclosure may be used to form elongated members of other cross-sectional geometries. For example: at least one C-shaped channel may be formed as illustrated in
[0076] Referring now to
[0077] The base 704 may include a rotary table 716 configured to rotate about a defined axis 718 relative to the gantry 708 and carriage assembly 710. A motor 720 or other actuator may be operably configured to rotate the rotary table 716 relative to a supporting portion 722 of the base 704. As the rotary table 716 rotates, the carriage assembly 710, along with its associated components, may move relative to the gantry 708 (i.e., in the direction indicated by directional arrow 714) so as to track the position of the mandrels 706A-706D as each mandrel 706A-706D sequentially passes therebeneath. The carriage assembly 710 may be configured to actively track the position of a mandrel 706A-706D passing therebeneath, such as through the use of the controller 500 and an actuator coupled to the carriage assembly 710. In another embodiment, the carriage assembly 710 may be configured to passively track the position of a mandrel 706A-706D passing therebeneath, such as by the engagement of one or more components of a forming device 726 with the mandrels 706A-706D, as will become apparent through subsequent discussion of such a forming device 726.
[0078] It is noted that, while the exemplary embodiment described with respect to
[0079] It is also noted that the mandrels 706A-706D may not necessarily exhibit a constant radius of curvature throughout their respective lengths. It is also noted that each mandrel 706A-706D may exhibit a different length, radius of curvature or other geometric characteristic than any of the other mandrels.
[0080] A material dispensing device 724 and a forming device 726 are coupled with the carriage assembly 710. As the rotary table 716 rotates relative to the gantry 708, the material dispensing device 724 is configured to place one or more plies of material onto the mandrels 706A-706D. The forming devices 726 may include a plurality of rollers 728 coupled to actuators 730 and configured to shape the plies of material placed on the mandrels 706A-706D.
[0081] For example, referring to the schematic shown in
[0082] It is noted that the tack roller 750 (and subsequent rollers encountered by the material 740) is shown in a first elevational view with a second, rotated elevational view depicted immediately therebeneath to provide additional understanding of how the material 740 is being shaped by the interaction of various rollers with the material 740 and the underlying mandrel 706A.
[0083] The forming device 726 includes a plurality of rollers 728A-728D used to shape and debulk material 740 disposed over the mandrel 706A (or over previously shaped material plies disposed on the mandrel 706A). Thus, for example, a first roller 728A engages the mandrel 706A to generally conform the material 740 to the shape of the mandrel 706A. Second, a set of rollers 728B may be used to press the material against the side walls 754 of the mandrel 706A. If desired, this may be accomplished with multiple sets of rollers 728B working from an upper portion of the mandrel 706A to a bottom portion as depicted in the rotated elevational views of the rollers 728B. Another set of rollers 728C may be used to press the material 740 into interior lower corners 756 of the mandrel 706A. A squeegee 758 may be used to help pull wrinkles from the material 740 at one or more intermediate locations among the rollers 728A-728D. Finally a set of rollers 728D may be used to press and form flange members of the elongated member 702.
[0084] It is noted that the process of forming the elongated member 702 includes forming, shaping and debulking the material 740 from the inside out. In other words, the tack roller 750 applies pressure to the mandrel 706A and material 740 disposed thereon at the center, with subsequent rollers 728A-728D each sequentially applying pressure at a location further towards the outer edges of the material 740. Such a process has been determined to be efficient and effective in removing wrinkles and air gaps between laminar plies of material thereby producing a highly consolidated and debulked composite member.
[0085] A take-up roller 760 may be associated with the forming device 726 (or independently coupled with the carriage assembly 710) to collect carrier material 762 (also referred to as backing) which may be disposed on a surface of, for example, a prepreg material used to form the elongated member 702. The carrier material 762, which may include a suitable polymer material, not only keeps the prepreg material from adhering to itself when in rolled form (i.e., such as when on supply and tension roller 742) but also may remain on the material 740 while the material 740 is being shaped, formed and debulked so that the various rollers 750 and 728A-728D do not stick to the material 740 or collect and build-up resin of a surface thereof. Additionally, the presence of such carrier material 762 may serve to protect the material 740 used to form an elongated member 702 when the various rollers 728 press and rub against the material 740 during forming of the elongated member 702.
[0086] Referring now to
[0087] The scrub roller 728A may include two roller halves 800A and 800B coupled to a shaft 802. The shaft 802 may be coupled to the carriage assembly 710 and an actuator or other force applying mechanism (not shown in
[0088] Besides the ability to tailor the amount of force being applied to the side walls 754 of the mandrel 706A, the configuration of the scrub roller 728A also enables the production of elongated members 702 that exhibit varied cross-sectional geometries. For example, referring briefly to
[0089] As seen in
[0090] Referring now to
[0091] It is noted that the initial location of pressure or contact between the material 740 and the mandrel 706A effected by the scrub roller 728A may be determined by the shape, contour, and positioning of the scrub roller 728A relative to the mandrel 706A. For example, referring briefly back to
[0092] Referring now to
[0093] Each dispenser 724A-724C of the material dispensing device 724 may include a supply of material that exhibits different characteristics than the other supplies of material. For example, the first dispenser 724A may include a ply of material 740A that exhibits a 0 fiber orientation, the second dispenser 724B may include material 740B that exhibits a 45 fiber orientation, and the third dispenser 724C may include material 740C exhibiting a fiber angle different than that included in the first and second dispensers 724A and 724B. In another embodiment, the width or thickness of the material may vary from one dispenser to another. Another exemplary embodiment may include different types of grades of material in each dispenser 724A-724C. Such a configuration provides considerable flexibility and efficiency in the formation of elongated members 702 (
[0094] Referring briefly to
[0095] In other embodiments, the material dispensing device 724 may be configured to dispense filler materials such as, for example, filler adhesives or small filler members known by those of ordinary skill in the art as noodles. Such filler material may be utilized, for example, if an apparatus was configured to join two elongated structures formed as C-shapes in a back-to-hack arrangement in order to form an I-beam. As recognized by those of ordinary skill in the art, such a construction often leaves a small recess along the edge of the joint line between the two members, which is desirably filled with, for example, a noodle.
[0096] Similarly, the material dispensing device 724 may be configured to lay down other materials including, for example, tackifier materials or bagging materials. Tackifier materials may be disposed on individual plies of the material 740 to enhance tack between adjacent plies. Bagging materials may be disposed over a mandrel 706A prior to dispensing a ply of material 740 for subsequent release of an elongated member 702 from the mandrel 706A. Thus, in some instances, it may be desirable to apply a new layer of bagging material over the mandrel 706A prior to manufacturing a new elongated member 702.
[0097] Referring now to
[0098] To prevent wrinkling of the material 740 (
[0099] Considering the use of a woven prepreg material as the ply of material 740 being dispensed, application of tension to the material 740 as it is disposed on to the mandrel 706A and subsequently shaped by the forming device 726 causes the material 740 to stretch along the larger radius of curvature (e.g., R2 in
[0100] In other words, a tension gradient may be developed across the width of the material 740 as it is dispensed and formed on the mandrel 706A. For example, a tension gradient may be developed in the material 740 used to form the elongated member 702 such that tension is at a minimum (which may be nearly zero in some cases) at the lateral edge exhibiting the smaller radius of curvature (e.g., R1) while tension is at a maximum at the lateral edge of the material exhibiting the larger radius of curvature (e.g., R2). The gradient need not be strictly a linear gradient from one edge of the material 740 to the other. The weave of the material 740 may determine, in part, the amount of stretching that may be accommodated by the fabric and the magnitude of the force that needs to be applied to the fabric depending on the give of the material as determined by the particular weave of the fabric.
[0101] In one exemplary embodiment, a force of approximately 30 to 40 lbf (approximately 133.4 to 177.9 N) may be applied to the material 740 to place the material 740 in appropriate tension. Of course, the amount of force applied to the material may depend on a number of factors including, for example, the type of material being used (including the weave of the fabric), the width of the material, the radius of curvature of the mandrel 706A, or a combination of such factors. In addition to the tension applied to the material 740, heat may be applied to the material to relax the material and help facilitate the stretching of the material 740 along, or adjacent to, the edge exhibiting the larger radius of curvature. However, the amount and intensity of heat applied to the material 740 may be selected and controlled so as to prevent premature curing of the material 740.
[0102] Referring now to
[0103] A material dispensing device 724 and a forming device 726 are coupled with the carriage assembly 710. As the rotary table 716 rotates about the defined axis 718 relative to the gantry 708, the material dispensing device 724 is configured to place one or more plies of material onto the mandrel 706. The forming device 726 may include a plurality of rollers 728 coupled to actuators 730 and configured to shape the plies of material placed on the mandrel 706. The mandrel 706 is coupled to the rotary table 716 in a spaced relationship thereto by a plurality of support structures 780. The material dispensing device 724 and the forming device 726 are positioned radially inwardly of the mandrel 706 and configured to engage and interact with the mandrel 706 as it rotates along with the rotary table 716. The configuration and orientation of the material dispensing device 724 and the forming device 726 may be referred to as being parallel to the rotary table 716, whereas the configuration and orientation of the material dispensing device 724 and forming device 726 shown in
[0104] Referring to
[0105] It is noted that the cross-sectional geometry of the elongated member 702 is rotated along a general radius of curvature 786 relative to that of the elongated member 702 shown in
[0106] Referring now to
[0107] The use of multiple adjacent and abutting plies of material reinforced by laminar bridge plies provides additional flexibility in forming a curved elongated member 702. For example, if the radius of curvature of the elongated member 702 is such that use of a single ply of material to form the entire cross-sectional geometry would not be feasible, either because wrinkles would still develop or because the amount of tension required to avoid wrinkles would be detrimental to the strength characteristics of the material, separate plies of narrower width may be used. In other words, the tension required to stretch a material ply that is wide enough to extend between the first radius of curvature R1 and the second radius of curvature R2 is greater than that required to stretch a material ply that is wide enough to extend between, for example, the second radius of curvature R2 and a third radius of curvature R3. Thus, using multiple laterally adjacent plies of material enables the construction of elongated members 702 exhibiting wider cross-sectional geometries while reducing the tension applied to, and the stretching experienced by, the material plies.
[0108] It is noted that other variations of the present disclosure are also contemplated. For example, while the exemplary embodiments have been described to include a mandrel and a plurality of complementary rollers, two sets of complementary rollersan upper set, and a lower setmay be used to form the elongated members. Thus, for example, a plurality of fibers may be passed through an upper female set of rollers and a lower male set of rollers to obtain a desired cross-sectional geometry. However, it is noted that the use of a mandrel, such as in the above-described exemplary embodiments, may provide more precise placement of the plies and control of fiber orientation. Additionally, while various embodiments have been described in terms of utilizing carriage assemblies and gantries, it is further contemplated that robotic arms may be utilized in positioning the rollers and applying appropriate force or pressure to materials disposed over a mandrel. Such a robot may be configured such that the associated roller or rollers are positionable about multiple axes.
[0109] Additionally, various materials may be used in forming the elongated structural members. For example, composite tape, fabric, dry fabric or various combinations thereof may be used. Furthermore, filler materials may be introduced into the elongated structural member as deemed appropriate. Such filler materials may include, for example, foam, metallic or other nonplastic materials.
[0110] While the disclosure may be susceptible to various modifications and alternative forms, specific embodiments have been shown, by way of example, in the drawings and have been described in detail herein. However, it should be understood that the disclosure is not intended to be limited to the particular forms disclosed. Rather, the disclosure includes all modifications, equivalents, and alternatives falling within the scope of the disclosure as defined by the following appended claims and their legal equivalents.